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AbstractAluminum metal matrix composite brake rotors with a selective ceramic function reinforcement gradient (FRG) have been developed for automotive applications. This paper will highlight the design, manufacturing, and testing of the rotors. Weight saving of an aluminum composite rotor in comparison to an industry standard cast iron rotor is 50-60%. With this material change comes design considerations to manage rotor temperature, rotor surface integrity, and friction. Manufacturing methods to meet these design constraints were needed to develop a viable high performance aluminum composite rotor. High pressure squeeze casting with soluble coring techniques were developed to incorporate the selective FRG MMC rotors. Dynamometer testing was performed, concentrating on brake friction and temperature to evaluate the macro and micro interfaces in the rotors. The rotors’ testing results indicate that a functional reinforced aluminum metal matrix composite rotor is viable option for front and rear brake applications in the automotive and commercial trucking market.IntroductionThe automotive industry has had an emphasis on light weighting, due to factors like NHTSA standards [1] and consumer pressure. Brake rotors are a component that may not see the same emphasis as others, due to the passenger safety requirement of a braking system or cost differential.Metal matrix composites (MMC) are made of nonmetal materials dispersed in a metal matrix. Aluminum MMC’s have and are being used in components like pistons, cylinders, and brake disks. Aluminum MMC’s can be stir-cast to give increased strength, stiffness, thermal resistance and stability over aluminum.REL Inc. and others [2] have directed efforts towards development of an aluminum MMC automotive rotor. A one piece internally vented rotor was the goal of REL’s efforts. This would allow for a lightweight rotor that would have the ability to reduce its temperature faster than a standard rotor. This is crucial for an aluminum MMC rotor to operate under heavy braking conditions. Standard iron rotors have the ability to operate at higher temperatures than an aluminum MMC rotor due to material differences. To compensate, a venting structure is needed to increase airflow and reduce running temperature.Rotor DevelopmentREL’s aluminum MMC material has a high ceramic content. A 50% ceramic volume fraction MMC is achievable. This MMC material has a coefficient of thermal expansion of about half of aluminum. The MMC’s thermal diffusivity is also about half of aluminum’s.In the path to developing an aluminum MMC one piece internally vented automotive rotor, there were three stages of development before the final prototype. This stages are as follows: Single blademotorcycle rotor, solid one piece rotor, and three piece vented rotor. Figure 1. REL aluminum MMC motorcycle rotor and carrierDevelopment of Aluminum Composite Automotive Brake Rotors2016-01-1937Published 09/18/2016 Taylor Erva, Adam Loukus, and Luke LuskinREL, Inc.CITATION: Erva, T., Loukus, A., and Luskin, L., "Development of Aluminum Composite Automotive Brake Rotors," SAE Technical Paper 2016-01-1937, 2016, doi:10.4271/2016-01-1937.Copyright © 2016 SAE InternationalThe single blade motorcycle rotors are for use by road motorcycles. They are generally thin (≈6mm) and have no center section. The entire blade is composed of aluminum MMC with a function gradient. The rotors are being sold as OE replacements for select street motorcycles.The solid one piece automotive rotor is a single blade rotor with a center hub section that has mounting for an automobile. The rotor is selectively reinforced, with the aluminum MMC section being the friction ring of the rotor. The rotor has external vanes, to help regulatetemperature. The hub and venting section are made of aluminum alloy.Figure 2. REL solid one-piece aluminum MMC automotive rotorThree piece vented automotive rotor is similar to the design of the one piece internally vented automotive rotor. It consists of a center hub section and two rotor blade halves. Each rotor blade half holds half of the internal venting structure. The halves are bolted together and then to the hub. The rotor blade halves and venting sections arealuminum MMC. The hub is made of aluminum alloy.Figure 3. REL vented three-piece aluminum MMC automotive rotorOne Piece Vented Automotive RotorThe automotive rotor has these features: Aluminum with selectively reinforced aluminum MMC sections, one-piece construction, andinternal venting.Figure 4. REL vented one-piece aluminum MMC automotive rotorThe rotor is made up of aluminum alloy and aluminum metal matrix composite material. The ceramic reinforced sections of the rotor are the two braking surfaces. The rotor hub and venting sections are made up of aluminum alloy. The MMC braking surfaces have a function reinforcement gradient (FRG). The ceramic density isradially variable, with an increase in volume fraction from the interior to the perimeter of the preform. This radial change in ceramic volume fraction compensates for the increase in energy and stress on the outer section of the rotor during braking.A computational simulation was done to determine the thermal mechanical performance of a rotor during a stop. Results from the simulation show a difference in stress from the outer edge of the rotor to the inner edge. The pattern of higher stress on the outer edge of the rotor to lower stress on the inner edge of the rotor is followed in a simulation with 0% ceramic content and simulation with 100%ceramic content.Figure 5. Stress simulation with 0% ceramic contentFigure 6. Stress simulation with 100% ceramic contentFigure 7. Stress simulation: rotor edge comparisonTensile testing of aluminum MMC samples was done. Samples of specific ceramic volume fractions were tensile tested and Poisson’s ratio was determined from the results. A trend of decreasing Poisson’s ratio as ceramic volume fraction increases can be observed from the results. With this trend, a gradient of ceramic in the metal matrix composite section of the rotor is used to maintain a rotors integrity during a braking cycle. Higher stress regions have higher ceramic content than lower stress regions of the MMC braking surface.Table 1. Poisson’s ratio of MMCAluminum alloy has a melting temperature of about 550°C lower than iron. However, aluminum MMC has a higher thermalconductivity than iron. These material constraints influenced the design of the rotor. The venting structure in the rotor provides a way for the rotor to regulate its temperature. The curved vanes produce a centrifugal air pump in the rotor when rotated. This airflow created by the pump transfers heat from the rotor to the air. The heated air is then pushed out of the vent. The thermal conductivity of aluminum MMC is higher than iron, so while heat from braking is absorbed faster by an aluminum MMC rotor, heat is dissipated at a faster rate.Venting is crucial to the operation of this rotor.Figure 8. Sectioned internally vented one-piece rotorManufacturingTo manufacture a brake rotor with a high ceramic content and a function reinforcement gradient, high pressure squeeze casting is necessary. The ceramic volume fraction in the in REL rotors cannot be easily achieved by stir cast MMC. To attain the content andgradient of ceramic material, a preform of ceramic material is used. This preform gets infiltrated by aluminum in a high pressure squeeze casting. The infiltration allows the aluminum to form the matrix around the ceramic material.The method of infiltrating ceramic preforms with aluminum gives the ability to have a FRG. The infiltrated preforms are tailored to improve rotor performance. The move away from a stir-cast aluminum MMC method to a preform infiltration method, gives the ability to selectively reinforce the rotor.The aluminum MMC used in the automotive rotor is difficult to machine. Sections of the rotor, venting structure and rotor hub, are not reinforced with ceramic. These sections are not used for braking and do not require improved properties. The majority of the machining required in the non-MMC areas of the rotor.The internal venting in the one piece rotor is not machined andrequires a core. Using high pressure squeeze casting required a high strength core. A salt core had to be developed to withstand thecompressive force required, not be infiltrated, and not lose integrity with temperatures required for casting. The salt core is one piece and holds the negative pattern of the venting structure.The assembly used for casting consists of two ceramic preforms, with a salt core in the middle. The casting assembly is placed in the die and squeeze cast. The aluminum will infiltrate the preforms to create composite material, and be voided by the salt core, creating theventing structure. All other aluminum in the casting will removed orused for rotor hub.Figure 9. REL vented one-piece rotor manufacturing setupTestingThere were three types of testing done with the aluminum MMC rotors. Friction testing was done to determine the ability of a brake rotor to stop with a given set of brake pads. Integrity testing was done to observe the ability of the rotors to withstand braking before failure. Temperature testing was used to evaluate a rotors ability to manage heat added through braking. All tests were done on a brakedynamometer. Thermocouples placed in rotors and pads are used for temperature collection.Friction TestingDifferent brake pads were tested to determine the friction coefficient, brake pad wear and rotor wear when used on aluminum MMC rotors. Non-asbestos organic (NAO) brake pads are preferred for aluminum MMC rotors. Metallic and semi-metallic brake pads are not ideal for the hardness of the composite rotors. All tests shown were completed using the same compound of braking material. It is a NAO brake pad selected for its compatibility with aluminum MMCs.An aluminum MMC rotor was friction tested against a similar cast iron rotor. Both rotors were braked with the same composition of organic material and in the same caliper. The test followed the FMVSS 122 Standard, S7.1 to S7.5. After a brake warming andburnish, the effectiveness tests consisted of six stops from 48.3 km/h (30 mph) and six stops from 96.6 km/h (60 mph) initiated at 65.5°C (150°F) brake temperature. The test concludes with four 128.7 km/h (80 mph) stops and four 160.9 km/h (100 mph) stops in succession. From the test, a brake coefficient of friction for each stop iscalculated. [3]Figure 10. Cast Iron vs Aluminum MMC Friction ResultsThe cast iron and aluminum MMC rotors exhibited similar friction behavior in the test. Through the 30 mph and 60 mph stops, the coefficient of friction for both rotors varied between 0.40 and 0.44. On the 80 mph and 100 mph stops, the MMC rotor saw a steady decrease in its friction coefficient, while the cast iron rotor had a similar decrease but resisted fade better on the final stops.Integrity TestingWith a selectively reinforced rotor, there are two or more different material expansion rates in the rotor as there are two differentmaterials. When subjected to braking, the heat added to the rotor is not constant, linear, or uniform throughout the rotor. Testing on the rotor was done to determine a brake rotors behavior during a heat cycle. Organic brake pads were used. Results of the testing are determined visually. Cracking, separation, degrading, and gougingare all evaluated and compared to other rotors.Figure 11. Integrity testing separation resultsIntegrity testing done consisted of repeated braking without any external cooling. The rotor was stopped from 80 km/h (equivalent speed) at high braking pressure (4500 kPa target) until significant gouging occurred.The results of the integrity testing indicate that the selectivelyreinforced rotor will not fail under temperature change. There was no visible layer separation or significant warping. Gouging occurred at high rotor temperature (≥540°C), exceeding the degradation temperature of the brake pads used.Temperature TestingEvaluating the effectiveness of the venting structure in the rotors was done through temperature testing. The rate of cooling of a vented automotive aluminum MMC rotor was compared against a similar rotor with the venting blocked. Venting was blocked using an epoxy putty. Minimal amounts of epoxy was used, to maintain thesimilarities between the rotors. The test consisted of adding heat to arotor, through a braking cycle, then spinning the rotor at a constant speed (300 rpm). Temperatures are then monitored as the rotor cools down. No external air source was added.Table 2. Vented vs Non-vented cooldown resultsThe comparative results of the cooling of the vented and non-vented rotors showed that the vented rotor will cool faster than a non-vented rotor. This verifies development from solid rotor, to internally vented rotor.In the same manner as the previous test, a vented cast iron rotor was compared to the aluminum MMC vented automotive rotor. Therotation speed was 330 rpm with a cooling wind with of 48.3 km/h.Figure 12. Cast Iron vs Aluminum rotor cooldown resultsThe results of the second temperature test shows the difference in the cooling rates between cast iron and aluminum MMC. The aluminum MMC cooled to 100°C in about half of the time that the cast iron rotor did. This difference in cooling rates allows an aluminum MMCrotor to cool faster than a traditional brake rotor.Figure 13. Aluminum MMC rotor dynamometer testingA third temperature test was run on a dynamometer with two 280mm rotors. One rotor in the test was a prototype aluminum MMC rotor, while the second rotor, like the previous test, was a vented cast iron rotor of similar geometry. The test consisted of ten stops from 80 km/hr equivalent speed and braking with a target maximum brake line pressure of 3500 kPa. There was approximately 20 seconds between each stop. There was an external inline convective airflow produced by an industrial blower that matched the speed of the rotor,simulating the operation of a vehicle. The dynamometer flywheel hada moment of inertia of 78.25 kg*m^2.Figure 14. Aluminum MMC vs cast iron operating temperature testResults from the third temperature test show the operatingtemperatures of a vented aluminum MMC rotor against a comparable cast iron rotor in an aggressive braking test. The MMC rotordisplayed a higher temperature gain per stop than the iron rotor, but also had a greater temperature loss between stops. The cast iron rotor had higher final temperature after the test, but displayed slightlyquicker braking, finishing the test in less time than the MMC rotor.Figure 15. Iron rotor dynamometer testingProductionREL mass produces aluminum MMC motorcycle rotors following the process of squeeze casting aluminum into a ceramic, post cast machining, and heat treatment. The production of a single piecevented aluminum MMC rotor requires an extra component (salt core), two ceramic preforms, and an extra post process (salt removal). Although there are differences the production method of the single blade MMC motorcycle and the process needed for the vented MMC rotor, the method is adaptable to produce the vented MMC rotor.Production costs for a single piece vented aluminum MMC automotive rotor are higher than that of an equivalent cast iron rotor. This is due to a more extensive manufacturing process as well as more expensive materials. When compared to lightweight carbon ceramic rotors, aluminum MMC rotors are significantly cheaper. Market OpportunityNo cost effective one-piece lightweight brake rotor is currently available in the automotive market. Lightweight multi-piece composite rotors are in the high-end auto market. Development is needed to make these components more robust, accepted and cost effective. Though there is widespread demand for this sort of innovation, the expensive composite brake rotors and other lightweight automobile components are only available to the high end and niche applications.The developed lightweight automotive rotor will improve fuel efficiency by allowing for less vehicle weight, lowering the un-sprung weight for better handling and allow for even greater vehicle weight reduction elsewhere by enabling additional complementary weight saving improvements.The commercial potential of the development of a selectively reinforced aluminum composite automobile brake rotor provides a needed solution for the automobile industry. Vehicles that can be targeted for commercialization include lightweight and electric vehicles. Small lightweight vehicle are less demanding of braking systems than full size vehicles. Electric vehicles may have regenerative braking systems that will reduce the amount of braking that is done in the mechanical braking system. In both types of vehicles, electric and lightweight, there is a reduced amount of braking needed compared to a standard vehicle. With limited braking needed, lightweight and electric vehicles are an initial commercialization target for selectively reinforced aluminum composite automobile brake rotors. Beyond this initial target, vehicles from the small car to medium duty truck and military industry can also be targeted for adoption of aluminum MMC rotors. Aluminum MMC Brake DrumsBrake drums made of aluminum metal matrix composite have been developed by Century Inc. The lightweight braking solution can remove 40% of the weight of a similar cast iron brake drum. The brake drums were selectively reinforced and used ceramic preforms and squeeze casting as the method of manufacture. Vehicle and dynamometer testing showed the MMC brake drum either matched or exceeded cast iron drum performance on a 4536 kg axle load. The level of success demonstrated by this brake drum makes it a feasible for the commercial truck and military market. [2] ConclusionAluminum metal matrix composite brake rotors with a selective ceramic function reinforcement gradient have been developed to supplement the demand for light weighting in the auto industry. The development moved from proven single blade motorcycle rotor, to a solid one piece automotive rotor, an internally vented three piece automotive rotor, and finally a one piece internally vented automotive rotor. The intention of development was to produce a lightweight rotor that can be substituted for a standard cast iron rotor. The one piece internally vented rotor has a ceramic function reinforcement gradient, which tailors the MMC rotor sections to a braking cycle, as well as internal venting that will remove heat in the rotor.Rotor development also include development of manufacturing strategies to complement the rotor demands. To be selectively reinforced with a ceramic FRG, the casting method of ceramic preforms and high pressure die casting had to be optimized. Incorporation of an internal venting structure required the development of a large, high strength salt casting core. Dynamometer testing of the aluminum MMC rotor consisted of friction, integrity, and temperature testing. Friction results show that an aluminum MMC rotor and cast iron rotor have similar friction capabilities when using an organic brake pad. Integrity testing results prove that a selectively reinforced rotor can operate without failure at normal braking temperatures. Temperature testing verified the effectiveness of a venting structure as well as the faster cooling rate of an aluminum MMC rotor over a cast iron rotor. The testing results indicate that a functional reinforced aluminum metal matrix composite rotor is viable option for front and rear brake applications in the automotive market.Noise and rusting of rotors was observed during comparison testing of between cast iron and aluminum MMC rotors. The MMC rotors made considerably less noise than the cast iron rotors. While the iron rotors would squeak during braking, the MMC rotors would make a much softer light grinding sound. During storage of rotors, the iron rotors would build an oxidation layer that would be removed before braking. The aluminum MMC rotors did not have a need for oxidation to be removed.This development has been able to prove out the performance and manufacturing of a single piece vented aluminum automotive MMC rotor. Optimization of the rotor and it production process are still necessary for improvement of the product before market introduction. On-vehicle testing is the next step toward pushing development. References1. National Highway Traffic Safety Administration, “CAFÉ - FuelEconomy,” /fuel-economy, accessed Mar.2016.2. Kero, M. and Halonen, A., "Development and Testing ofLightweight Aluminum Composite Brake for Medium to Heavy Duty Vehicles," SAE Technical Paper 2010-01-1705, 2010,doi:10.4271/2010-01-1705.3. National Highway Traffic Safety Administration, Department ofTransportation., “Traffic Safety Administration Laboratory Test Procedure for FMVSS 122,” TP-122-02 August 1, 2006 Contact InformationAdam Loukusadam@Taylor Ervataylor@Luke Luskinluke@REL, Inc.57640 North Eleventh StreetCalumet, MI 49913Phone: 1-906-337-3018rel@Fax: (906) 337-2930AcknowledgementsThe authors would like to thank the Ohio State University for theirwork, support, and results in material testing and computersimulation.Additionally, the authors would like to thank the National ScienceFoundation for their funding of this development effort.The Engineering Meetings Board has approved this paper for publication. It has successfully completed SAE’s peer review process under the supervision of the session organizer. The process requires a minimum of three (3) reviews by industry experts.All rights reserved. No part of this publication may be reproduced, stored in a retrieval system, or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE International.Positions and opinions advanced in this paper are those of the author(s) and not necessarily those of SAE International. The author is solely responsible for the content of the paper.ISSN 0148-7191/2016-01-1937。
Electronic letter
doi:10.1136/jmg.38.9.e282001;38;28- J. Med. Genet.Bourgeron Lluis Quintana-Murci, Agnes Rötig, Arnold Munnich, Pierre Rustin and Thomasdeleted mtDNA Mitochondrial DNA inheritance in patients with/cgi/content/full/38/9/e28Updated information and services can be found at:These include:References /cgi/content/full/38/9/e28#otherarticles 1 online articles that cite this article can be accessed at:/cgi/content/full/38/9/e28#BIBL This article cites 25 articles, 9 of which can be accessed free at: Rapid responses/cgi/eletter-submit/38/9/e28You can respond to this article at:service Email alertingtop right corner of the articleReceive free email alerts when new articles cite this article - sign up in the box at the Topic collections(3977 articles)GeneticsArticles on similar topics can be found in the following collectionsNotes/cgi/reprintform To order reprints of this article go to:/subscriptions/ go to: Journal of Medical Genetics To subscribe toElectronic letterMitochondrial DNA inheritance in patients withdeleted mtDNALluis Quintana-Murci,Agnes Rötig,Arnold Munnich,Pierre Rustin,Thomas BourgeronE DITOR—Mitochondrial diseases encompass a large group of clinical disorders resulting from numerous genotypes,with variable age of onset and all possible modes of heredity,which have been extensively studied over the past decade.1–3So far,more than50point mutations and a significant number of complex rear-rangements,including deletions and duplica-tions,have been identified in mitochondrial DNA(mtDNA)of patients with oxidative phosphorylation diseases(MITOMAP4).In most cases,there is a cell to cell variable load of mutant to wild type(wt)mtDNA,a condition called heteroplasmy.The severity of the result-ing mitochondrial defects depends not only on the nature of the mutation but also on the pro-portion of mutant to wild type mtDNA.The origin and mechanism of the accumula-tion of mutant mtDNA(up to99%in some tissues)in patients with mitochondrial diseases are still a matter of debate.5Di V erent hypoth-eses have been proposed.First,the mutant mtDNA may already be present in the mother’s oocytes.Then,by simple genetic drift,mutant mtDNA couldfinally represent a high pro-portion of the total mtDNA in a specific organ or tissue.It has already been shown that a small amount of founder mtDNA can populate the organism and that the number of segregating units(n)could be as low as a single mitochon-drion.67This proposal of a genetic bottleneck has been supported by the observation of significant levels of rearranged mtDNA in the oocytes of a patient with Kearns-Sayre syn-drome8and by studies of mtDNA hetero-plasmy in mice.7Another explanation could be that the mutational event occurs later during embryogenesis.Accordingly,the accumulation of mutant molecules could reflect a prolifera-tive advantage for the mutant mtDNA over the wild type during replication or segregation. This hypothesis comes from studies of mutant mtDNA segregation in vitro.9–11A new alternative hypothesis is based on the particular pattern of inheritance of mtDNA. This is assumed to be strictly maternally inher-ited with no apparent paternal contribution to the mtDNA pool of the o V spring.It is known that paternal mitochondria entering the egg are rapidly eliminated by active processes during thefirst stages of mammalian embryogen-esis.1213However,the presence of paternal mtDNA has been detected at the blastocyst stage in some abnormal human embryos.14Furthermore,in contrast to the orthodox view of clonal maternal inheritance,several recent articles have shown that recombination eventscan occur in human mtDNA,casting doubtson the strict maternal inheritance ofmtDNA.15–17However,while attracting a lot ofattention,these results remain contentious.18–22Based on these observations,it could behypothesised that the presence of mutantmtDNA in the zygote could result from a par-tial degradation of paternal mtDNA after ferti-lisation.T o address this question,we haveascertained the parental origin of the deletedmtDNA( -mtDNA)in a group of patientswith Pearson syndrome,villous atrophy,and/orencephalomyopathy.23–27All patients had a pro-portion of -mtDNA higher than80%of thetotal mtDNA pool in the tissue studied,exceptfor one case where the proportion of -mtDNA was30%.Wefirst looked for the presence of -mtDNA in the blood cells of themothers by PCR amplification of the relevantfragments,using primersflanking the deletion.The -mtDNA was absent in all testedsamples.In the case of a paternal origin of the -mtDNA,we expected tofind a paternal hap-lotype in the patients.The mitochondrial con-trol region(CR)haplotypes were therefore defined in six families where DNA samples from both parents of the a V ected child were available.Variation in the CR sequence was determined by direct sequencing of a total of 401bp(from nucleotide position(np)16000 to np16400)encompassing the CR hypervari-able segment I(HVS-I),as described previ-ously.28Sequence variants were ascertained by alignment and comparison with the Cam-bridge Reference Sequence(CRS).The mtDNA CR haplotypes in the six fami-lies analysed are reported in table1togetherwith the proportion of -v wt-mtDNA.Out ofthe six families analysed,two(families2and4)turned out to be uninformative since all mem-bers shared the same mtDNA lineage.Amongthe four informative cases(families1,3,5,and6),all patients showed only the maternalmtDNA lineage.Thus,all mtDNA moleculespresent in the a V ected children were transmit-ted following strict maternal inheritance,rulingout the possibility of a paternal origin of the -mtDNA molecules found in the o V spring. Our results also show that mtDNA deletions occur on di V erent mtDNA backgrounds,for example,the common deletion(4977bp)wasJMG2001;38:e28(/cgi/content/full/38/9/e28)1of3 Unitéd’ImmunogénétiqueHumaine,INSERME021,Institut Pasteur,25-28rue Dr Roux,75724Paris Cedex15,FranceL Quintana-MurciT BourgeronUnitéINSERM U393,Hôpital NeckerEnfants-Malades,149rue de Sèvres,75743Paris Cedex15,FranceA RötigA MunnichP RustinCorrespondence to:DrBourgeron,thomasb@pasteur.frfound in families1and6on two di V erent mtDNA genetic backgrounds.Although sam-ple size was rather small and deletion break-points heterogeneous,these observations sug-gest an absence of correlation between a particular mtDNA background and higher occurrence of mtDNA deletion.Strict maternal transmission could be an advantage for preventing the spread of deleteri-ous mitochondrial genomes from the sperma-tozoa.29Nevertheless,assisted reproductive techniques,such as intracytoplasmic sperm injection(ICSI),using immature spermatozoa during fertilisation,could increase the risk of a leakage of paternal mtDNA in the zygote.30 Moreover,in two independent studies,no paternal mtDNA could be detected in the blood of children born after ICSI.3132In contrast,paternal mtDNA was still detectable in polyploid embryos generated by standard in vitro fertilisation or ICSI.14Moreover,both recipient and donor female mtDNA was present in thefirst babies born after egg cytoplasmic donation.33In conclusion,we report the absence of paternally transmitted mtDNA in children with mitochondrial deletions.While we only studied sporadic cases of mitochondrial dis-ease,this should be extended to familial cases with more than one a V ected child harbouring multiple or single -mtDNA.Characterising the origin of the mutant mtDNA molecules could help in understanding the genetic complexity of mitochondrial diseases and improve genetic counselling and prenatal diagnosis in families with mtDNA hetero-plasmy.1Larsson NG,Clayton DA.Molecular genetic aspects of human mitochondrial disorders.Annu Rev Genet 1995;29:151-78.2Wallace DC.Mitochondrial diseases in man and mouse.Science1999;283:1482-8.3Munnich A,Rötig A,Chretien D,Saudubray JM,Cormier V,Rustin P.Clinical presentations and laboratory investiga-tions in respiratory chain deficiency.Eur J Pediatr 1996;155:262-74.4MITOMAP.A human mitochondrial genome database.Center for Molecular Medicine,Emory University,Atlanta, USA./mitomap.html(2000).5Chinnery PF,Thorburn DR,Samuels DC,White SL,Dahl HM,Turnbull DM,Lightowlers RN,Howell N.The inheritance of mitochondrial DNA heteroplasmy:random drift,selection or both?Trends Genet2000;16:500-5.6Jenuth JP,Peterson AC,Fu K,Shoubridge EA.Random genetic drift in the female germline explains the rapid seg-regation of mammalian mitochondrial DNA.Nat Genet 1996;14:146-51.7Shoubridge EA.Mitochondrial DNA segregation in the developing embryo.Hum Reprod2000;15:229-34.8Marchington DR,Macaulay V,Hartshorne GM,Barlow D, Poulton J.Evidence from human oocytes for a genetic bot-tleneck in an mtDNA disease.Am J Hum Genet 1998;63:769-75.9Y oneda M,Chomyn A,Martinuzzi A,Hurko O,Attardi G.Marked replicative advantage of human mtDNA carrying a point mutation that causes the MELAS encephalomyopa-thy.Proc Natl Acad Sci USA1992;89:11164-8.10Bourgeron T,Chretien D,Rotig A,Munnich A,Rustin P.Fate and expression of the deleted mitochondrial DNA dif-fer between human heteroplasmic skinfibroblast and Epstein-Barr virus-transformed lymphocyte cultures.J Biol Chem1993;268:19369-76.11Moraes CT.What regulates mitochondrial DNA copy number in animal cells?Trends Genet2001;17:199-205.12Kaneda H,Hayashi JI,T akahama S,T aya C,Lindahl KF, Y onekawa H.Elimination of paternal mitochondrial DNA in intraspecific crosses during early mouse embryogenesis.Proc Natl Acad Sci USA1995;92:4542-6.13Sutovsky P,Moreno RD,Ramalho-Santos J,Dominko T, Simerly C,Schatten G.Ubiquitin tag for sperm mitochon-dria.Nature1999;402:371-2.14St John J,Sakkas D,Dimitriadi K,Barnes A,Maclin V, Ramey J,Barratt C,De Jonge C.Failure of elimination of paternal mitochondrial DNA in abnormal ncet 2000;355:200.15Ankel-Simons F,Cummins JM.Misconceptions about mitochondria and mammalian fertilization:implications for theories on human evolution.Proc Natl Acad Sci USA 1996;93:13859-63.16Awadalla P,Eyre-Walker A,Smith JM.Linkage disequilib-rium and recombination in hominid mitochondrial DNA.Science1999;286:2524-5.17Strauss E.Human genetics.mtDNA shows signs of paternal influence.Science1999;286:2436.18Macaulay V,Richards M,Sykes B.Mitochondrial DNA recombination-no need to panic.Proc R Soc Lond B Biol Sci1999;266:2037-9.19Parsons TJ,Irwin JA.Questioning evidence for recombina-tion in human mitochondrial DNA.Science2000;288:1931. 20Kumar S,Hedrick P,Dowling T,Stoneking M.Questioning evidence for recombination in human mitochondrial DNA.Science2000;288:1931.21Kivisild T,Villems R.Questioning evidence for recombina-tion in human mitochondrial DNA.Science2000;288:1931. 22Jorde LB,Bamshad M.Questioning evidence for recombina-tion in human mitochondrial DNA.Science2000;288:1931. 23Rotig A,Cormier V,Blanche S,Bonnefont JP,Ledeist F, Romero N,Schmitz J,Rustin P,Fischer A,Saudubray JM, Munnich A.Pearson’s marrow-pancreas syndrome.A mul-tisystem mitochondrial disorder in infancy.J Clin Invest 1990;86:1601-8.24Cormier-Daire V,Bonnefont JP,Rustin P,Maurage C,Ogler H,Schmitz J,Ricour C,Saudubray JM,Munnich A,Rotig A.Mitochondrial DNA rearrangements with onset as chronic diarrhea with villous atrophy.J Pediatr1994;124:63-70.25Cormier V,Rotig A,Geny C,Cesaro P,Dufier JL,MunnichA.mtDNA heteroplasmy in Leber hereditary opticneuroretinopathy.Am J Hum Genet1991;48:813-14.T able1HVS-I haplotypes in the six families analysed.Relevant information on%of deleted mtDNA,extent of the deleted region,and clinical presentation is also givenFamily Clinical presentation Tissue DeletedmtDNA Deletion extent HVS-I haplotypeP1Pearson syndrome Lymphocytes90%8484–13460239G256311M1239G256311F1069097G104A126261 P2Villous atrophy+Muscle90%10665–14856CRSM2encephalomyopathy CRSF2CRSP3Villous atrophy+Lymphocytes30%10744–14124291M3encephalomyopathy291F3224270P4Progressive Lymphocytes90%(Multiple deletions)7845–15761,7931–15761,7619–15032,9844–16064,9966–15801126193278M4encephalomyopathy126193278F4298311P5Pearson syndrome Bone marrow80%5793–12767069126145222261M5069126145222261F5069126145222261P6Pearson syndrome Lymphocytes85%8484–13460224311362M6224311362F61922243112of3Electronic letter26Cormier V,Rotig A,Quartino AR,Forni GL,Cerone R, Maier M,Saudubray JM,Munnich A.Widespread multi-tissue deletions of the mitochondrial genome in the Pearson marrow-pancreas syndrome.J Pediatr1990;117: 599-602.27Rotig A,Bourgeron T,Chretien D,Rustin P,Munnich A.Spectrum of mitochondrial DNA rearrangements in the Pearson marrow-pancreas syndrome.Hum Mol Genet 1995;4:1327-30.28Vigilant L,Stoneking M,Harpending H,Hawkes K,Wilson AC.African populations and the evolution of human mito-chondrial DNA.Science1991;253:1503-7.29Allen JF.Separate sexes and the mitochondrial theory of aging.J Theor Biol1996;180:135-40.30Bourgeron T.Mitochondrial function and male infertility.Results Probl Cell Di V er2000;28:187-210.31Houshmand M,Holme E,Hanson C,Wennerholm UB, Hamberger L.Is paternal mitochondrial DNA transferred to the o V spring following intracytoplasmic sperm injection?J Assist Reprod Genet1997;14:223-7.32Danan C,Sternberg D,Van Steirteghem A,Cazeneuve C, Duquesnoy P,Besmond C,Goossens M,Lissens W,Amse-lem S.Evaluation of parental mitochondrial inheritance in neonates born after intracytoplasmic sperm injection.Am J Hum Genet1999;65:463-73.33Barritt JA,Brenner CA,Willadsen S,Cohen J.Spontaneous and artificial changes in human ooplasmic mitochondria.Hum Reprod2000;15:207-17.Electronic letter3of3。
AMS2759_2F
__________________________________________________________________________________________________________________________________________ SAE Technical Standards Board Rules provide that: “This report is published by SAE to advance the state of technical and engineering sciences. The use of this report is entirely voluntary, and its applicability and suitability for any particular use, including any patent infringement arising therefrom, is the sole responsibility of the user.”SAE reviews each technical report at least every five years at which time it may be revised, reaffirmed, stabilized, or cancelled. SAE invites your written comments and suggestions.Copyright © 2014 SAE InternationalAll rights reserved. No part of this publication may be reproduced, stored in a retrieval system or transmitted, in any form or by any means, electronic, mechanical, photocopying, recording, or otherwise, without the prior written permission of SAE. TO PLACE A DOCUMENT ORDER: Tel: 877-606-7323 (inside USA and Canada) Tel: +1 724-776-4970 (outside USA) Fax: 724-776-0790Email: CustomerService@ SAE WEB ADDRESS:h ttp://SAE values your input. To provide feedbackon this Technical Report, please visit/technical/standards/AMS2759/2FAEROSPACE MATERIAL SPECIFICATIONAMS2759/2REV. FIssued 1984-10 Revised 2010-05 Reaffirmed 2014-04Superseding AMS2759/2EHeat Treatment of Low-Alloy Steel PartsMinimum Tensile Strength 220 ksi (1517 MPa) and HigherRATIONALEAMS2759/2F has been reaffirmed to comply with the SAE five-year review policy.1. SCOPEThis specification, in conjunction with the general requirements for steel heat treatment covered in AMS2759, establishes the requirements for heat treatment of low-alloy steel parts to minimum ultimate tensile strengths of 220 ksi (1517 MPa) and higher. Parts are defined in AMS2759. 2. APPLICABLE DOCUMENTSThe issue of the following documents in effect on the date of the purchase order forms a part of this specification to the extent specified herein. The supplier may work to a subsequent revision of a document unless a specific document issue is specified. When the referenced document has been cancelled and no superseding document has been specified, the last published issue of that document shall apply. 2.1 SAE PublicationsAvailable from SAE International, 400 Commonwealth Drive, Warrendale, PA 15096-0001, Tel: 877-606-7323 (inside USA and Canada) or 724-776-4970 (outside USA), .AMS2418 Plating, Copper AMS2424 Plating, Nickel, Low-Stressed Deposit AMS2759 Heat Treatment of Steel Parts, General RequirementsARP1820 Chord Method of Evaluating Surface Microstructural Characteristics 2.2 ASTM PublicationsAvailable from ASTM International, 100 Barr Harbor Drive, P.O. Box C700, West Conshohocken, PA 19428-2959, Tel: 610-832-9585, .ASTM E 384 Microindentation Hardness of MaterialsDownloaded from SAE International by Daryl Jaeger, Wednesday, July 02, 20143. TECHNICAL REQUIREMENTS3.1 Heat TreatmentShall conform to AMS2759 and requirements specified herein.3.2 EquipmentShall conform to AMS2759. Furnace temperature uniformity requirements for annealing, subcritical annealing, normalizing, hardening, straightening, stress relieving, and baking shall be ±25 °F (±14 °C), and for tempering or aging shall be ±10 °F (±6 °C).3.3 Heating EnvironmentParts shall be controlled by type (See 3.3.1), and heat treated in the class of atmosphere (See 3.3.2), permitted in Table 1 for that type when heating above 1250 °F (677 °C). When heating parts at 1250 °F (677 °C) or below, Class A, B, or C atmosphere may be used (See 8.2).TABLE 1 - ATMOSPHERESPart Classification (1)Class A Class B Class CType 1 Permittted Permitted Permitted(3)Type 2 Permitted PROHIBITED (2) PermittedType 3 Permitted Permitted PROHIBITEDType 4 Permitted Permitted (3)(4) PROHIBITEDNOTES:(1) See 3.5.1.2.(2) Permitted provided the atmosphere is controlled to produce no carburization or nitridingas described in 3.5.1.(3) Prohibited if a specific requirement to control the surface carbon on all surfaces isspecified.(4) Not recommended for Aermet 100.3.3.1 Types of PartsThe heat treating processor shall determine the part type.Type 1: Parts with 0.020 inch (0.51 mm) or more to be machined off all surfaces after heat treatment and parts with as-forged, as-cast, or hot-finished mill surfaces at time of heat treatment with all surfaces to be machined off.Unless informed that all surfaces will have at least 0.020 inch (0.51 mm) machined off, the heat treating processor shall assume all surfaces will not and shall control the part as Type 2, 3, or 4, as applicable.Type 2: Forgings, castings, sheet, strip, plate, bar, rod, tubing, and extrusions with hot-finished surfaces at time of heat treatment and which will remain on the finished part.Type 3: Parts with finished machined surfaces or surfaces with less than 0.020 inch (0.51 mm) to be machined off any surface after heat treatment and parts with protective coating on all surfaces.Type 4: Parts that are partially machined with both unmachined (e.g., as-forged, as-cast, or hot- finished mill surfaces) and finished/near-finished surfaces (e.g., finished machined surfaces, or machined surfaces with less than0.020 inch (0.51 mm) to be machined off after heat treatment).3.3.1.1 If part type cannot be determined, the part shall be processed as Type 3.3.3.2 Classes of AtmospheresClass A: Argon, hydrogen, helium, nitrogen, nitrogen-hydrogen blends, vacuum, or neutral salt. Nitrogen from dissociated ammonia is not permitted.Class B: Endothermic, exothermic, or carbon-containing nitrogen-base (See 8.2).Class C: Air or products of combustion.3.3.3 AtmospheresAtmosphere furnaces shall be controlled to ensure that surfaces of heat treated parts are within the limits specified in 3.5.1. Salt baths shall be tested in accordance with AMS2759.Coatings3.3.4 ProtectiveA supplemental coating or plating is permitted, when approved by the cognizant engineering organization. Fine grain copper plating in accordance with AMS2418 or nickel plating in accordance with AMS2424 may be used without approval but the surface contamination specimens in 3.6.1 shall not be plated (See 8.3).3.4 Procedure3.4.1 PreheatingPreheating until furnace stabilization in the 900 to 1200 °F (482 to 649 °C) range is recommended before heating parts above 1300 °F (704 °C) if the parts have previously been heat treated to a hardness greater than 35 HRC, have abrupt changes of section thickness, have sharp reentrant angles, have finished machined surfaces, have been welded, have been cold formed or straightened, have holes, or have sharp or only slightly-rounded notches or corners.3.4.2 SoakingHeating shall be controlled, as described in AMS2759, such that either the heating medium or the part temperature, as applicable, is maintained at the set temperature in Table 2 or 3 for the soak time specified herein. Soaking shall commence when all control, indicating, and recording thermocouples reach the specified set temperature or, if load thermocouples as defined in AMS2759 are used, when the part temperature reaches the minimum of the furnace uniformity tolerance at the set temperature.3.4.2.1 Parts coated with copper plate or similar reflective coatings that tend to reflect radiant heat shall have their soaktime increased by at least 50%, unless load thermocouples are used.3.4.3 AnnealingShall be accomplished by heating to the temperature specified in Table 2, soaking for the time specified in Table 4, and cooling to below the temperature specified in Table 2 at the rate shown in Table 2 followed by air cooling to ambient temperature. Isothermal annealing treatments may be used providing equivalent hardness and microstructure are obtained. Isothermal annealing shall be accomplished by heating to the annealing temperature specified in Table 2, soaking for the time specified in Table 4, cooling to a temperature below the critical, holding for sufficient time to complete transformation, and air cooling to ambient temperature.Annealing3.4.4 SubcriticalShall be accomplished prior to hardening by heating in the range 1150 to 1250 °F (621 to 677 °C), soaking for the time specified in Table 4, and cooling to ambient temperature. Steel parts of the 9Ni - 4Co types shall be subcritical annealed as specified in Table 2.3.4.5 Pre-Hardening Stress RelievingShall be accomplished prior to hardening by heating in the range 1000 to 1250 °F (538 to 677 °C), soaking for not less than the time specified in Table 4, and cooling to ambient temperature.3.4.6 NormalizingShall be accomplished by heating to the temperature specified in Table 2, soaking for the time specified in Table 4, and cooling in air or atmosphere to ambient temperature. Circulating air or atmosphere is recommended for thicknesses greater than 3 inches (76.2 mm). Normalizing may be followed by tempering or subcritical annealing.3.4.7 Hardening (Austenitizing and Quenching)All parts, except those made from H-11, 52100, or M-50 steels, shall be in one of the following conditions prior to austenitizing: normalized, normalized and tempered, normalized and overaged, or hardened. If such parts have been normalized only, without tempering or overaging, they shall be preheated within the range of 850 to 1250 °F (454 to 677 °C) before exposure to the austenitizing temperature (See Table 2 Note 2). Welded parts and brazed parts with a brazing temperature above the normalizing temperature shall be normalized before hardening. Welded parts should be preheated in accordance with 3.4.1. Hardening shall be accomplished by heating to the austenitizing temperature specified in Table 2, soaking for the time specified in Table 4, and quenching as specified in Table 2. The parts shall be cooled to or below the quenchant temperature before tempering.3.4.8 Tempering or AgingShall be accomplished by heating quenched parts to the temperature required to produce the specified properties. Parts should be tempered within 2 hours of quenching (See 3.4.8.1). Tempering for specific tensile strengths for each alloy is shown in Table 3. Soaking time shall be not less than 2 hours plus 1 hour additional for each inch (25 mm) of thickness or fraction thereof greater than 1 inch (25 mm). Thickness is defined in AMS2759. When load thermocouples are used, the soaking time shall be not less than 2 hours. Multiple tempering is permitted. When multiple tempering is used, parts shall be cooled to ambient temperature between tempering treatments.3.4.8.1 Prior to final tempering parts may be snap tempered for 2 hours at a temperature, usually 400 °F (204 °C), thatis lower than the final tempering temperature (See 8.5.1).3.4.9 StraighteningWhen approved by the cognizant engineering organization, straightening shall be accomplished at either ambient temperature, during tempering, or by heating to not higher than 50 °F (28 °C) below the tempering temperature. Ambient temperature straightening or hot or warm straightening after tempering shall be followed by stress relieving. It is permissible to retemper at a temperature not higher than the last tempering temperature after straightening during tempering.3.4.10 Post-Tempering Stress RelievingWhen required by the cognizant engineering organization, parts shall, after operations which follow hardening and tempering, be stress relieved by heating the parts to 50 °F (28 °C) below the tempering temperature and soaking for not less than 1 hour plus 1 hour additional for each inch (25 mm) of thickness or fraction thereof greater than 1 inch (25 mm). When load thermocouples are used, the soaking time shall be not less than 1 hour. Stress relief is prohibited on parts that have been peened or thread- or fillet-rolled after hardening and tempering.3.5 PropertiesParts shall conform to the hardness specified by the cognizant engineering organization or to the hardness converted from the required tensile strength in accordance with AMS2759.3.5.1 SurfaceContaminationSalt baths and the protective atmosphere in furnaces for heating parts above 1250 °F (677 °C), when less than 0.020 inch (0.51 mm) of metal is to be removed from any surface, shall be controlled to prevent carburization or nitriding and to prevent complete decarburization (See 3.5.1.1). Partial decarburization shall not exceed 0.006 inch (0.15 mm) and a severity of 5 points HRC converted from Knoop. Depth and severity are described in ARP1820. Intergranular attack shall not exceed 0.0007 inch (0.018 mm). Rejection criterion for total depth of decarburization shall be the microhardness reading that has more than a 20-point Knoop, or equivalent, decrease in hardness from the core hardness. Rejection criterion for severity of decarburization is the difference between the HRC hardness (converted from Knoop) at 0.0003 inch (0.008 mm) and that of the core. Rejection criterion for carburization and nitriding shall be that the microhardness shall not exceed the core hardness by 20 points Knoop or more, or equivalent, at a depth of 0.0003 inch (0.008 mm). Tests shall be in accordance with 3.6.1. The requirements of this paragraph also apply to the cumulative effects of operations such as normalizing followed by austenitizing or austenitizing followed by reaustenitizing (See 3.5.1.4). For reheat treatments, the original specimen or a portion thereof shall accompany the parts and be tested after the reheat treatment.3.5.1.1 Unless specifically informed that at least 0.020 inch (0.51 mm) will be removed from all surfaces of parts, theheat treating processor shall heat treat the parts as if less than 0.020 inch (0.51 mm) will be removed from some surfaces and, therefore, shall heat treat using controlled atmosphere which will produce parts conforming to surface contamination requirements.3.5.1.2 Parts that will be machined after heat treatment, but which will have less than 0.020 inch (0.51 mm) of metalremoved from any machined surface may be reclassified as Type 1, as described in 3.3.1, and need not meet the requirements of 3.5.1 as heat treated, when it is demonstrated by tests (See 3.6.1.1) on each load that all surface contamination exceeding the requirements of 3.5.1 is removable from all machined surfaces, taking into account distortion after heat treatment.3.5.1.3 Furnaces used exclusively to heat treat parts that will have all contamination removed shall not require testing.3.5.1.4 The heat treating processor shall be responsible for determining whether cumulative heat treating operations atthat facility, as described in 3.5.1, have caused excessive surface contamination.3.6 Test MethodsShall be in accordance with AMS2759 and as follows:Contamination3.6.1 SurfaceTesting shall be performed by the microhardness method in accordance with ASTM E 384, supplemented, if necessary, by ARP1820. Test specimens shall be of the same alloy as the parts. Unless otherwise specified, test specimens shall be in the as-quenched condition except that secondary hardening steels, such as H-11, shall be tempered. In addition, the presence of total depth of decarburization, carburization, and nitriding shall be determined by etching with the appropriate etchant and examining at approximately 250X magnification. The depth of intergranular attack shall be determined on an unetched specimen at approximately 250X magnification (See 8.4).3.6.1.1 Testing for reclassification in 3.5.1.2 may be by any microhardness method if more than 0.002 inch (0.05 mm)is subsequently machined off all machined surfaces.4. QUALITY ASSURANCE PROVISIONSThe responsibility for inspection, classification of tests, sampling, approval, entries, records, and reports shall be in accordance with AMS2759 and as specified in 4.1 and 4.2. 4.1Classification of TestsThe classification of acceptance, periodic, and preproduction tests shall be as specified in AMS2759 and as specified in 4.1.1 and 4.1.2.4.1.1 Acceptance TestsIn addition to the tests specified in AMS2759, tests for surface contamination (3.5.1) shall be performed on each lot. Alternatively, if carbon potential is controlled automatically and either indicated or recorded, frequency of surface contamination tests may be in accordance with the sampling plan of 4.2. 4.1.2 Preproduction TestsIn addition to the tests specified in AMS2759, tests for surface contamination (3.5.1) shall be performed prior to any production heat treating on each furnace, each kind of atmosphere to be used in each furnace, and for each Class B atmosphere at two carbon potentials, up to 0.40% and over 0.40%. 4.2Alternative Sampling Plan4.2.1 An alternative test plan to meet the requirements of 4.1.1 is permitted for heat treatment processes verified bystatistical process control (SPC) to be stable and capable. 4.2.1.1 A process is considered stable when statistical evaluation of the product and process parameters show that allmeasured values fall within established control limits. 4.2.1.2 A process is considered capable when, after achieving and maintaining stability, all parts running to the processhave a minimum C pk of 1.33 with a confidence level of 90%. NOTE: C pk is defined as the smaller of either C pl or C pu as determined by Equation 1 or Equation 2:σ−=3LSLX C pl (Eq. 1) σ−=3XUSL C pu (Eq. 2) where:X = process averageLSL = lower specification limit* USL = upper specification limit**Specification limits are based on target values established by the supplierσ = estimated standard deviation4.2.2 The alternative test plan shall contain the following:4.2.2.1 Statistical analysis of the heat treatment process parameters and the product test results of properties forcontrol and capability (See 3.5).4.2.2.2 Documentation of the critical process parameters and of the product test results of properties on a control plan(See 3.5). A change in these process parameters of product test results will require review to determine if the process capability requires reverification.4.2.2.3 Periodic auditing of the heat treatment process parameters and the product test results of properties to verifycontinued control and capability (See 3.5).4.2.2.4 Monthly, or whenever needed by either the cognizant engineering authority or process constraints,decarburization shall be examined in accordance with 3.5.1.5. PREPARATION FOR DELIVERYIn accordance with AMS2759.6. ACKNOWLEDGMENTIn accordance with AMS2759.7. REJECTIONSIn accordance with AMS2759.8. NOTESIn accordance with AMS2759 and the following:8.1 A change bar (l) located in the left margin is for the convenience of the user in locating areas where technicalrevisions, not editorial changes, have been made to the previous issue of this document. An (R) symbol to the left of the document title indicates a complete revision of the document, including technical revisions. Change bars and (R) are not used in original publications, nor in documents that contain editorial changes only.8.2 Heating below 1400 °F (760 °C) with Class B atmospheres containing 5% or more of hydrogen (H2), carbonmonoxide (CO), or methane (CH4), may result in explosion and fire.8.3 When supplemental plating or coating, such as copper plate, is used, all atmosphere controls and surfacecontamination tests are still required.8.4 Use of a chromic-caustic etch to reveal intergranular attack/oxidation has been discontinued because (1) it is anenvironmental hazard (2) it is unnecessary for measurement of maximum depth of crevices, and (3) light etching zones extending beyond the crevices have been misinterpreted as manifestations of intergranular oxidation.8.5 Terms used in AMS are clarified in ARP1917 and as follows:8.5.1 Snap tempering is an immediate low temperature treatment to relieve stresses and prevent cracking prior to thenext operation. It is most often used prior to a refrigeration cycle. Final tempering to the specified requirements is performed after snap tempering.8.5.2 Marquenching(Martempering)Quenching an austenitized alloy in a salt or hot oil bath at a temperature in the upper part of, or slightly above, the martensite range and holding until temperature uniformity throughout the part is obtained, usually followed by air cooling through the martensite range to ambient temperature.8.6 Dimensions and properties in inch/pound units and the Fahrenheit temperatures are primary; dimensions andproperties in SI units and the Celsius temperatures are shown as the approximate equivalents of the primary units and are presented only for information.PREPARED BY AMS COMMITTEE “E” AND AMECTABLE 2A - ANNEALING, NORMALIZING, AND AUSTENITIZING TEMPERATURES AND QUENCHANTS,INCH/POUND UNITSMaterial DesignationAnnealing (1)Temperature, °FNormalizingTemperature, °FAustenitizing (2)Temperature, °FHardeningQuenchant4330V, 4330M (2) 4335, 4335M (2) 4340 (2)Hy-Tuf (2)300M (2)4340 Mod (2)H-11 (3)98BV40 (2)D6AC (2)521009Ni-4Co-0.30C (2) (5) M-50AF1410 (2) (5) AerMet ® 100 (2)157515501550140015501550160015501550( 6)( 8)--1650 (12)--165016501650172517001700--1600172516501700( 9)1650 (12)1650 (13)160016001500 (16)160016001600185015501625 (4)1550 (7)15502025 (10)15251625oil, polymeroil, polymeroil, polymeroil, polymeroil, polymeroil, polymerair, oil, polymeroil, polymeroil, polymeroil, polymer (5) (15)oil, polymer (5)salt (11)oil, polymer (5)air, oil, polymer (14)NOTES:1. Cool at a rate not to exceed 200 °F per hour to below 1000 °F, except cool 4330V, 4335V, and 4340 to below800 °F, and 300M to below 600 °F.2. All parts, except those made from H-11, 52100, or M-50 steels, shall be in one of the following conditions prior toaustenitizing: normalized, normalized and tempered, normalized and overaged, or hardened. If such parts have been normalized only, without tempering or overaging, they shall be preheated within the range of 850 to 1250 °F before exposure to the austenitizing temperature.3. H-11 parts shall be in the annealed condition prior to the initial austenitizing treatment.4. 1700 °F permitted for D6AC parts, when approved by the cognizant engineering organization.5. Immediately after quenching refrigerate parts made from 52100, 9Ni-4Co-0.30C, and AF1410 at -90 °F or lower,hold 1 hour minimum, and air warm to room temperature. For parts made from 52100 with high propensity to crack during refrigeration, a snap temper before refrigeration is recommended (See 8.5.1).6. Anneal parts made from 52100 at 1430 °F for 20 minutes, cool to 1370 °F at a rate not faster than 20 °F per hour,cool to 1320 °F at a rate not to exceed 10 °F per hour, cool to 1250 °F at a rate not faster than 20 °F per hour, and air cool to ambient temperature.7. 1500 °F permissible for parts made from 52100 requiring distortion control. Parts shall be hardened from thespherodize annealed condition or the normalized condition.8. 9Ni-4Co-0.30C parts shall be duplex subcritical annealed by heating at 1250 °F for 4 hours ± 1/4, air cooling toambient temperature, reheating at 1150 °F for 4 hours ± 1/4, and air cooling to ambient temperature or shall be annealed by heating at 1150 °F for not less than 23 hours minimum and air cooling to ambient temperature.9. Normalizing of M-50 parts should be avoided due to grain growth.10. M-50 parts shall be preheated to 1550 °F prior to austenitizing.11. For M-50 use 1125 °F followed by air cool to ambient temperature or air cool directly to ambient temperature.12. For AF1410, to facilitate machining, normalize and then heat to 1250 °F for not less than 6 hours and air cool.13. For Aermet ® 100, to facilitate machining, normalize and then heat to 1250 °F for not less than 16 hours and aircool.14. For AerMet ® 100, quench in oil (160 °F or lower), polymer, gas quench, or air cool below 400 °F within 2 hours.Within 8 hours of quenching, cool parts to -100 °F or lower, hold 1 hour per inch of thickness or fraction thereof, and warm in any convenient manner to room temperature.15. F or 52100 a salt marquench may be used if specified by the cognizant engineering organization (See 8.5.2).16. Parts made from 4340 may be austenitized at a set temperature of 1525 °F.Aermet® 100 is a registered trade name of Carpenter Technology.TABLE 2B - ANNEALING, NORMALIZING, AND AUSTENITIZING TEMPERATURES AND QUENCHANTS, SI UNITSMaterial DesignationAnnealing (1)Temperature, °CNormalizingTemperature, °CAustenitizing (2)Temperature, °CHardeningQuenchant4330V, 4330M (2) 4335, 4335M (2) 4340 (2)Hy-Tuf (2)300M (2)4340 Mod (2)H-11 (3)98BV40 (2)D6AC (2)521009Ni-4Co-0.30C (2) (5) M-50AF1410 (2) (5) Aermet ® 100 (2)857843843760843843871843843(6)(8)--899 (12)--899899899941927927--871941899927(9)899 (12)899 (13)871871815 (16)8718718711010843885 (4)843 (7)8431107 (10)829885oil, polymeroil, polymeroil, polymeroil, polymeroil, polymeroil, polymerair, oil, polymeroil, polymeroil, polymeroil, polymer ( 5) (15)oil, polymer (5)salt (11)oil, polymer (5)air, oil, polymer (14)NOTES:1. Cool at a rate not to exceed 111 °C per hour to below 538 °C, except cool 4330V, 4335V, and 4340 to below427 °C, and 300M to below 316 °C.2. All parts, except those made from H-11, 52100, or M-50 steels, shall be in one of the following conditions prior toaustenitizing: normalized, normalized and tempered, normalized and overaged, or hardened. If such parts have been normalized only, without tempering or overaging, they shall be preheated within the range of 454 to 677 °C before exposure to the austenitizing temperature.3. H-11 parts shall be in the annealed condition prior to the initial austenitizing treatment.4. 927 °C permitted for D6AC parts, when approved by the cognizant engineering organization.5. Immediately after quenching refrigerate parts made from 52100, 9Ni-4Co-0.30C, and AF1410 at -68 °C or lower,hold 1 hour minimum, and air warm to room temperature. For parts made from 52100 with high propensity to crack during refrigeration, snap temper before refrigeration is recommended (See 8.5.1).6. Anneal parts made from 52100 at 777 °C for 20 minutes, cool to 743 °C at a rate not faster than 11 °C per hour,cool to 716 °C at a rate not to exceed 6 °C per hour, cool to 677 °C at a rate not faster than 11 °C per hour, and air cool to ambient temperature.7. 816 °C permissible for parts made from 52100 requiring distortion control. Parts shall be hardened from thespherodize annealed condition or the normalized condition.8. 9Ni-4Co-0.30C parts shall be duplex subcritical annealed by heating at 677 °C for 4 hours ± 1/4, air cooling toambient temperature, reheating at 621 °C for 4 hours ± 1/4, and air cooling to ambient temperature or shall be annealed by heating at 621 °C for 23 hours minimum and air cooling to ambient temperature.9. Normalizing of M-50 parts should be avoided due to grain growth.10. M-50 parts shall be preheated to 843 °C prior to austenitizing.11. For M-50 use 607 °C followed by air cool to ambient temperature or air cool directly to ambient temperature.12. For AF1410, to facilitate machining, normalize and then heat to 677 °C for not less than 6 hours and air cool.13. For Aermet ® 100, to facilitate machining, normalize and then heat to 677 °C for not less than 16 hours and aircool.14. For AerMet ® 100, quench in oil (71 °C or lower), polymer, gas quench, or air cool below 204 °C within 2 hours.Within 8 hours of quenching, cool parts to -73 °C or lower, hold 1 hour per 25 mm of thickness or fraction thereof, and warm in any convenient manner to room temperature.15. For 52100 a salt marquench may be used if specified by the cognizant engineering organization (See 8.5.2).16. Parts made from 4340 may be austenitized at a set temperature of 829 °C.Aermet® 100 is a registered trade name of Carpenter Technology.。
2019新外研版高中英语必修二 Unit 2 单元知识滚动练
单元知识滚动练Unit 1 复习强化Ⅰ.单词拼写1.She has suffered(遭受)from headache,so she won’t go to school.2.What is your opinion(看法) about family planning this year?3.On arriving in Beijing,you must come and see me at your convenience(方便).4.They have been married(结婚) to each other for twenty years.5.In your new job you will perform a variety of functions.6.To tell the truth,I don’t know how he handled the job.7.Different ethnic groups have different cultures and customs.8.She was recommended for the post by the colleague.Ⅱ.单句语法填空9.The scientist is researching the information downloaded(download) from the Internet. 10.From now on I won’t go to play football at night.11.The original(origin) plan is much better than this one.12.I have been looking forward to having a chance to pay(pay) a visit to Huangshan.13.I was impressed by the way(that) she deal with this accident.14.What he said just now reminded me of that American professor.15.She picked up the telephone and dialed his number.16.We’re just trying to reach a point where both sides will sit down together and talk.Unit 2巩固落实Ⅲ.单词拼写17.The man lost his way in the desert and starved(挨饿) to death.18.The amount of money we have is limited(有限的) due to buying a computer.19.Only athletes who have reached the agreed standard for their event will be admitted(承认) as competitors.20.Now that you have been an adult(成人),you must learn to stand on your own feet. 21.Two thirds of the world’s population regularly eat rice.22.When on stage,try not to turn your back to the audience.23.The government calls on the citizens to lead a green life.24.Winning the match was the reward for the effort that the team had made.Ⅳ.单句语法填空25.In fact,there are many unexplained,puzzling and even amazing phenomena(phenomenon).26.As he works in a remote area,he visits his parents only on occasion.27.He gave her an admiring look in the competition(compete).28.She has been honoured(honour) with Star of the Week for her excellent work.29.It is my parents that/who often help me get out of trouble.30.Try to use the expressions above to indicate(indicate) that you are listening carefully to your partner.31.The scenery in my hometown is beautiful beyond expression.32.Your existence(exist) seems to have meaning,for someone needs you and loves you.Ⅴ.完成句子33.What he has said is not without reason.他说的话并非没有道理。
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or little about its physical environment at the start. In the process of planning, it must acquire more knowledge about the environment via successive sensing actions, and then use this knowledge of the environment to further plan its sensing actions. This iterative process is repeated until the given task is accomplished (Yu and Gupta 1999). A variety of sensors have been used in the past, mostly with mobile robots, with some exceptions as in Lumelsky and Cheung (1993). The class of robotic systems we are concerned with is broad and involves a distance or range sensor mounted on a robot mechanism with non-trivial geometry and kinematics.2 This class includes robots ranging from a simple polygonal mobile robot to complex articulated manipulators, mobilemanipulators (Holmberg and Khatib 2000; Wosch et al. 2002), humanoid robots (Hirai et al. 1998), and it includes a broad class of range sensors (also called “eye” sensors) such as range scanners (laser-based or ultrasound-based) that give distance with respect to a single vantage point (or the sensor coordinate frame). One example of such general robot–sensor systems is an eye-in-hand system – a manipulator arm (called robot from here on), equipped with an eye type sensor as shown in Figure 1. The robot is required to plan and execute collision-free motions in a unknown to it. Such a system provides significantly greater maneuverability for the sensor in exploring and mapping cluttered and constrained environments. Another example is that of humanoid robots with eye sensor(s) located on the head (Hirai et al. 1998). While such general robot–sensor systems raise some interesting fundamental and theoretical issues for sensor-based planning (see Gupta and Yong 2001), this paper follows the “high-level” framework proposed in Yu and Gupta (2000),
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Journal of Information ScienceDOI: 10.1177/01655515060623262006; 32; 131Journal of Information Science Dirk Lewandowski, Henry Wahlig and Gunnar Meyer-BautorThe freshness of web search engine databases /cgi/content/abstract/32/2/131The online version of this article can be found at:Published by:On behalf of:Chartered Institute of Library and Information Professionalscan be found at:Journal of Information Science Additional services and information for /cgi/alerts Email Alerts: /subscriptions Subscriptions: /journalsReprints.nav Reprints:/journalsPermissions.nav Permissions:/cgi/content/refs/32/2/131SAGE Journals Online and HighWire Press platforms):(this article cites 9 articles hosted on the CitationsThe freshness of web search engine databasesDirk Lewandowski, Henry Wahlig and Gunnar Meyer-BautorDepartment of Information Science,Heinrich-Heine-University Düsseldorf, GermanyReceived 19 July 2005Revised 5 September 2005Abstract.This study measures the frequenc y with whic h searc h engines update their indices. Therefore, 38 websites that are updated on a daily basis were analysed within a time-span of six weeks. The analysed searc h engines were Google, Yahoo and MSN. We find that Google performs best overall with the most pages updated on a daily basis, but only MSN is able to update all pages within a time-span of less than 20 days. Both other engines have outliers that are older. In terms of indexing patterns, we find different approaches at the different engines. While MSN shows c lear update patterns, Google shows some outliers and the update process of the Yahoo index seems to be quite chaotic. Implications are that the quality of different search engine indices varies and more than one engine should be used when searching for current content.Keywords:search engines; online information retrieval; world wide web; index quality; index fresh-ness 1.IntroductionThe numerous research papers dealing with the quality of web search engines can be divided into two groups. The first deals with the quality of search engines’results, the second with the quality of the search engines’ databases.The quality of search results is usually measured with retrieval tests, e.g. [1–8]. I n more recent studies one finds that the retrieval effectiveness of the big search engines converges, but the overall precision is not that good.n addition, some research focuses on the index quality. There are some studies dealing with the size of the search engines’ databases [9, 10] which reveal that the search engines only index a small portion of the web. Unfortunately, these papers are quite out of date, and further research should be carried out on this topic.The depth of indexing is discussed in some older studies (cf. [4]) but there are no current results. Bias in web crawling and therefore in the indices of search engines is discussed in some recent studies [12–14]. An important part of index quality lies in the fresh-ness of the databases. Users looking for current infor-mation will find it only if the search engine’s index is up to date. There are several search functions to evade the problem of outdated indices, such as special news search engines [15] or blog search engines.Our aim is to study the freshness of the databases of popular web search engines. Users usually rely on their favourite search engine to provide them with the best results and give little thought to whether the desired information is in the index at all. On the basis of our findings we would like to give a recommendation as to which search engine should preferably be used when searching for current information. First, we discuss the results from past studies dealing with date issues. Then we present our study of the freshness ofCorrespondence to: Dirk Lewandowski, Heinrich-Heine University Düsseldorf, Department of I nformation Science, Universitätsstraße 1, 40225 Düsseldorf, Germany. E-mail:dirk.lewandowski@uni-duesseldorf.deWeb search engine databasessearch engine databases, which will be discussed in detail.2.Related studies2.1.Notess 2001–2003Notess [16] uses six queries to analyse the freshness of eight different search engines (MSN, HotBot, Google, AlltheWeb, AltaVista, Gigablast, Teoma, and Wisenut). Unfortunately the author gives no detailed information on how the queries were selected. For each query all URLs in the result list which meet the following criteria are analysed:•First, they need to be updated daily.•Second, they need the reported update information in their text.The age of every web page is noted. Results show the age of the newest page found, the age of the oldest page found and a rough average per search engine. I n the most recent test [16], the big search engines MSN, HotBot, Google, AlltheWeb, and AltaVista all have some pages in their databases that are current or one day old. The databases of the smaller engines Gigablast, Teoma, and Wisenut contain pages that are quite a lot older, at least 40 days.When looking for the oldest pages, results differ a lot more and range from 51 days (MSN and HotBot) to 599 days (AlltheWeb). This shows that a regular update cycle of 30 days, as usually assumed for all the engines, is not used. All tested search engines have older pages in their databases.For all search engines, a rough average of freshness is calculated, which ranges from four weeks to seven months. The bigger ones reach an average of about one month except AltaVista whose index, with an average of about three months, is older.Notess’study has several shortcomings,which mainly lie in the insufficient disclosure of the methods. Neither how the queries are selected,nor how the rough averages were calculated,is described.Since only a small number of queries were used,only10to46 matches per search engine were analysed.This amount is simply too small to get more than just exploratory results.Another shortcoming is that the author does not explain how he determined the date when the different search engines indexed a page.For some engines the cache could be used,but not all of them offer this kind of function.Notess’research is discussed here simply because it has been–at least to our knowledge–the only attempt similar to our approach so far.The methods used in the Notess study were used in several similar investigations from 2001 [17] and 2002 [18–20]. Results show that search engines are perform-ing better in indexing current pages, but they do not seem to be able to improve their intervals for a complete update. All the engines have outdated pages in their index.2.2.Lewandowski 2004In a study testing the ability of search engines to deter-mine the correct date of web documents, Lewandowski [21] finds that the major search engines all have problems with this. He uses 50 randomly selected queries from the German search engine Fireball, which are sent to the major search engines Google, Yahoo and Teoma. These engines were selected because of their index sizes and their popularity at the time of the investigation. All searches were done twice: once without any restrictions, and once with a date restric-tion for the last six months. For each query, 20 results were examined for date information. The study reveals that about 30–33 percent of the pages have explicit update information in their content. This information was used to compare the non-restricted with the date-restricted queries.The number of documents from the top 20 list that were updated within the last six months was counted. The proportion of these documents, out of all the documents, was defined as the up-to-dateness rate. The corresponding sets of documents retrieved by the simple search, as well as by the date-restricted search, were calculated. The up-to-dateness rates for the simple search are 37 percent for Teoma, 49 percent for Google, and 41 percent for Yahoo. For the date-restricted search, the rates are 37 percent for Teoma (which means no improvement),60percent for Google, and 54 percent for Yahoo. Taking this into consideration even Google, which proved to be the best search engine in this test, fails in 40 percent of all docu-ments. All in all the study shows that all the tested search engines have massive problems in determining the actual update of the found documents. However this data could be very useful for indexing and even for the ranking process (cf. [22]).The study recommends using information from several sources to identify the actual date of a document. The following factors should be combined: server date, date of the first time the document was indexed, metadata (if available), and update infor-mation provided in the contents of the page [21].D.LEWANDOWSKI ET AL.2.3.Ntoulas, Cho and Olston 2004The problems described in Lewandowski [21] could result, at least in part, from the inability of search engines to differentiate between an actual update of the documents’ contents and the mere change of design elements or minor alterations such as the current date and time which is shown on some web pages.Ntoulas, Cho and Olston [23] distinguish between two measurements to determine an update of a web document. On the one hand there is the frequency of change, which search engines currently use to deter-mine an update. On the other hand there is the degree of change, which is not used by the search engines suf-ficiently. The study finds that, since there are often only minor changes in the content, the use of the frequency of change is not a good indicator to determine the degree of change. Of course there may be exceptions to this, such as pages providing weather information, but for general text-based information pages, this seems to be true.Furthermore the study can prove that a large amount of web pages are changing on a regular basis. Estimat-ing the results of the study for the whole web, the authors find that there are about 320 million new pages every week. About 20 percent of the web pages of today will disappear within a year. About 50 percent of all content will be changed within the same period. The link structure will change even faster: about 80 percent of all links will have changed or be new within a year.The results show how important it is for the search engines to keep their databases up to date.2.4.Machill, Lewandowski, and Karzauninkat 2005In a ‘reaction test’ [15], this study investigates how fast the several engines index news content. The test was designed to analyse the speed of search engines at inte-grating events of topical interest into their news indices. Nine search engines were tested one hour,three hours and five hours after an event appeared in the Reuters news ticker.Just one query was used,‘Hubschrauber Absturz im I rak’ (helicopter crash in Iraq).Results show that Google as well as AltaVista and Yahoo provided the best reaction time of less than an hour. All other search engines with the exception of T-Online (a German portal) were able to provide first articles after three hours. Yahoo, AltaVista and Google were in the lead with regard to the number of hits as well as to the impact of the results.A strong limitation of the test is the use of just onequery. Apart from that it is obvious that a good reaction time is needed to keep the news indices current. I t would be very difficult to integrate the news results into the regular index of crawled web pages. Search engines therefore separate the two databases.Additional news indices would not be needed if the engines were able to integrate the current news into their regular databases.3.Objectives of this studyThe previous chapter proved that the testing of the freshness of search engine databases is still new in information science. As we have seen there are just a few studies published and they all focus mainly on other aspects of the broad topic of date information.The representative daily measuring of a search engine’s index up-to-dateness, as planned in this research, has never been run in such a test environment before.Keeping that in mind, we are aware that our study has to carry out basic research especially in terms of its method. We attach particular importance to the exper-imental setup and description of the workflow, which tries to find the best way to test the up-to-dateness of the web page indices. Our hope is that our method can play the role of a model for further similar studies on the same topic.In terms of content, this paper concentrates on more general questions and compiles some basic facts about the update process of the search engine indices. With our tests we would like to find out the frequency with which the search robots update their indices. Are there any specific intervals for every single web page or – to put it more generally – are there any clear intervals at all? So far, assumptions have been made that the search engines update their whole index within a period of 30days. These assumptions were proved false by Notess [16] but this general theory has to be double checked in our research because of possible improvements since Notess’ studies.Certainly, the comparison of the three competitors is an important focus of our research. Which similarities and differences can be stated between the search engines and what do they tell us about the quality of the index? Can Google confirm its role as the perceived technology leader in search engine technology in terms of its up-to-dateness as well?As already mentioned, our work will define some basic statements and raise more specific questions for later research. This means that we can answer the question if the search engines update their indicesWeb search engine databasesproperly, but not why this works better or worse with some pages or engines. These questions have to be answered in later research, which will concentrate on certain phenomena. For these points, our general data basis is simply not detailed enough.4.Method4.1.Selection of the pagesOurfirst goal was tofind40German websites which are updated on a daily basis. The number of 40 websites was chosen since it seemed to provide the best relation between reliable results on the one hand and acceptable work effort for testers on the other. From this basic set, we had to omit two pages in the course of our study for technical reasons.The first restriction was that all websites had to show the date of their last update within their content. This restriction had to be made since not all of the search engines publish information on when the cache version was taken. While Google and MSN display the date above the record taken from the cache, Yahoo does not. To clarify the date of that page we had no other option than to get the date from the web page itself. To collect this information, we simply needed an automatic date generator, which displays the actual date somewhere in the content. Many news portals, for example, show the actual date and time on top of every page. Another study [21] had already proved that the search engines cannot distinguish between minor changes (e.g. change of date) and changes that affect the content. We were mainly interested in the content of the page and we wanted to get a representative image of daily updated websites for our research. Therefore we formed four groups with nine or ten websites in order to reflect the actual situation on the web: 18 news portals (groups 1 and 2), 10 science-oriented pages (group 3) and 10 special interest websites (group 4); although we were conscious of the fact that there is some overlap between the groups.The following paragraphs present these groups. Details on the sites can be found in the appendix.4.1.1.National news portals.The first group (like the second one) consists of nine clearly news-oriented websites. The difference between these two groups is that this first group concentrates on news portals with a supra-regional character and mainly on national and international news. The websites satisfy common infor-mation needs of visitors from completely different backgrounds and exceed the portals of the second group in importance and traffic.4.1.2.News portals with a regional c harac ter.This second group with nine websites also focuses on news-oriented but more regional websites. The news services offered there may include national news, but mainly concentrate on regional or local information.4.1.3.Science-oriented websites.The third group consists of science-oriented websites. The main focus of these pages is to transfer specific academic news or background information. The main audience is not the public in general, but people who are interested in this topic. Traffic and importance depend decisively on the single topic.4.1.4.Spe ial interest websites.The fourth group contains 10 special interest websites. The topics range from specific ones on certain leisure time activities such as camping to more general topics, such as for example online flirting. The traffic and audiences on these websites also vary depending on the topic.4.2.Selection of the search enginesAfter choosing the websites for our research we had to decide which search engines should be examined. I n order to fulfil these conditions, we first had to get an overview of the current situation on the German search engine market.When analysing the dependence of the different companies we found out that only google.de, yahoo.de and msn.de run their own indices. All other big players in Germany such as T-Online or AOL get their results from one of these companies.Empirical studies of user behaviour towards German search engines are rare and mostly quite old. The latest publication on that topic from Machill and Welp [6] dates back to the year 2003. We therefore observed current international studies, which are frequently updated on . Nielsen Net Ratings [24] is one of them. I t measures the search behaviour of more than a million representative users worldwide on a monthly basis. The results convey a clear message: Google, Yahoo and MSN together share more than 80 percent of the complete market. In March 2005, Google got a share of 47 percent, Yahoo 20.9 percent and MSN 13.6 percent. All other competitors were in a negligible position.Our hypothesis was that this worldwide trend is also valid for Germany. In order to test this assumption, weD.LEWANDOWSKI ET AL.used a special empirical instrument on the web:WebHits (www.webhits.de), the leading German company offering web counters for private and com-mercial homepages. One of the services they offer is to determine which search engine brought the user to the websites, using a WebHits counter. The variety of the customers using WebHits is very large and includes small private websites but also heavily frequented commercial pages. Generally, the updated statistical output is based on approximately 50,000 queries per day. The results show an even clearer, but finally com-parable result: 80 percent use the search engine Google,whereas MSN and Yahoo share the second position with about 5 percent each.These clear findings confirmed our hypothesis and encouraged us to run the study with the three big inde-pendent search engines on the German market:google.de, yahoo.de and msn.de.4.3.Workflow: how to measure freshness?Our research tried to find out whether these theoretical statements can be sustained in reality. In order to get an answer, we had to find out how fast our 38 daily updated pages are updated in the Google, MSN and Yahoo indices. We will call this value the ‘freshness rate’.The measuring of the index up-to-dateness seemed to be not that easy, since the age of the index versions is not directly displayed by the search engines. Although the result list is based on the internal index, the user is led to the real website on the web when he or she clicks on one of the items. To avoid that forwarding, we developed the following workflow, which determines the ‘freshness rate’, which is defined as the time lag between the internal cache version and the real version of a web page:(1)The complete URL has to be entered in the querybox of the search engine.(2)In the displayed record, the link ‘Cache-Version’(Google), ‘im Cache’ (Yahoo) or ‘zwischengespe-icherte Seite’ (‘Cached page’, MSN) had to be followed. This link refers not to the real web page,but to the current version of the same page in the internal index.(3)The displayed page shows the cache version andsome further information in a text above. MSN and Google include the date and time when the cache version was taken, whereas Yahoo does not show any date or time at all. That forced us, as already mentioned, just to select websites with a date record in the content itself. However, wefinally got exact dates for every cached web page.We first thought about using the http header of the cached pages to determine the actual date, but this did not work since the header always shows the current date.(4)In order to finally get the freshness rate, the datesof the cache versions must be set in relation to the actual date of that day. A cache version from 8March, for example, has a freshness of two (days)on 10 March. The freshness rate of a search engine’s database is the average freshness of all pages examined.The described workflow led to a complete statistical output of 4788 specific freshness rates (38 web pages ϫ3 search engines ϫ42 days).4.4.The outward settingBeside these theoretical questions, we also had to define some further practical settings at the beginning of the test. The first one concerned the length of our research: we finally decided to run our tests for exactly six weeks or 42 days. This time seemed adequate to lead to reliable results on the one hand, with manage-able proportions on the other. The study was eventu-ally carried out from 15 February to 28 March 2005.Moreover, we opted to repeat our tests on a daily basis – no other frequency would have guaranteed us consistent results. An important factor in this context was to lay down a fixed time at which the tests had to be repeated daily. Otherwise disparities in the results would certainly have emerged, since a cache version not updated at 8 a.m. may already have been renewed by 8 p.m. the same day. This result would have led to two different freshness rates.We settled on 6 p.m., which was not meant as a strict rule but more as a reference value. The time period for our test was finally extended from 5 p.m. to 8 p.m. This was no problem since our pre-tests clearly showed that all search engines tend to update their caches once a day – mostly at night (Central European Time).4.5.Pre-testAn extensive pre-test was run for five weeks beginning on 18 December and ending on 19 January. In this test we examined the same search engines, Google, Yahoo and MSN, but limited the number of pages to the five websites web.de, sportschau.de, idw-online.de, rp-online.de, and uni-duesseldorf.de.The methods of the pre-test later determined the workflow of the main test. It was primarily carried outWeb search engine databasesby a group of four students, two of whom took part in the main test as well.The main purpose of the pre-test was to get a first impression as to whether it was worthwhile carrying out a more comprehensive study with a larger number of websites. Additionally, the daily tests were intended to provide first-hand experience on the practicability of the workflow.The results of the pre-test produced a divided picture. Google and MSN reached constant freshness rates of about 1.0 and 2.3 days on average, whereas Yahoo caused several problems. On some days, the cache was completely unreachable, on other days the results varied extraordinarily. We were astonished by the continuing phenomenon that Yahoo showed on one day one-day-old cache versions and on the next day versions that were nine or ten days old. We concluded that at the very least Yahoo could not guarantee constant updates of its index. This phenomenon of sudden ‘refreshment gaps’ also occurred at MSN, although not to the same extent. These curious results encouraged us to examine this subject on a broader scale in an additional main test.Furthermore the pre-test proved that the four-steps workflow was the right instrument. Therefore it was applied to the main test as well. Technical problems were only caused by other factors, since especially Yahoo removed the display of the cache for some sites during the test.4.6.Main testThe main test started on14February and was,as already mentioned,conducted for38websites,3 search engines and42days.This meant that thefinal analysis would be based on4674single records(38ϫ3ϫ42).Unfortunately this number of records was reduced because of some insurmountable technical problems we had already recognized during our pre-test: from time to time, the search engines (especially Yahoo but never Google) removed the display of the cache from their website overnight. For some sites like reuters.de, this phenomenon occurred nearly daily. One day the cache was displayed, the next it was not. This inacces-sibility of the cache version reduced our total statisti-cal output to 4572 records.Another problem led to a further reduction since one of the sites changed its layout during the tests. The portal www.liebesalarm.de removed the date display from its website on 10 March, so we could not assess the age of the cached version at Yahoo anymore. This limited our statistical output to a final number of 4556 records.No further technical or other problems occurred during the test.5.ResultsThe presentation of our results contains three parts. The first one will point out some general aspects which are valid for the complete research. We will then focus on the four groups, which were selected according to their topic and popularity (see section 4.1. ff.). We will attempt to prove the assumption that the update fre-quency has something to do with the content of the website. Finally, part three will concentrate on the indexing patterns of the three search engines and observe the technique with which the search robots update their indices.5.1.Overall resultsFirst of all we wanted to find out which search engine provides the best results. When searching the web every search engine usually yields a large quantity of results. But how do we know that we got the latest information on our topic? Perhaps one page was updated just yesterday with some really new aspects. An ideal search engine would update its index on a daily basis. I n our first analysis we want to examine how close each search engine gets to that ideal.I n our research we got an overall data set of 1558 results for every search engine. In this evaluation, we measure how many of these records are not older than one or even zero days. We were not able to differenti-ate between these two values because we queried the search engines only once a day. If there was a search engine that updated pages at a certain time of the day we would have preferred it to the others. Therefore, we assume that a page that was indexed yesterday or even today is up to date in the cache.As shown in Figure 1, Google returns most of its results with the value 1 (including 0). The total number of 1291 records shows that 82.86 percent of the Google results were not older than one day. These results are much better than those of the competitors and are an obvious sign of the premium quality of the Google index.MSN follows with 748 (48.01%). Yahoo contains 652(41.85%) one- or zero-days old pages in its index. Obviously,the percentage of current websites cannot be the only indicator to measure the overall。
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Clinical Rehabilitation Evaluation of cervical range of motion and isometric neck muscle strength: reliability and validityThomas Tai Wing Chiu and Sing Kai Lo Clin Rehabil 2002; 16; 851 DOI: 10.1191/0269215502cr550oa The online version of this article can be found at: /cgi/content/abstract/16/8/851Published by:Additional services and information for Clinical Rehabilitation can be found at: Email Alerts: /cgi/alerts Subscriptions: /subscriptions Reprints: /journalsReprints.nav Permissions: /journalsPermissions.nav Citations (this article cites 20 articles hosted on the SAGE Journals Online and HighWire Press platforms): /cgi/content/refs/16/8/851Downloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.Clinical Rehabilitation 2002; 1 6: 851–858Evaluation of cervical range of motion and isometric neck muscle strength: reliability and validityThomas Tai Wing Chiu and Sing Kai Lo Department of Rehabilitation Sciences, The Hong Kong Polytechnic University, Hung Hom Kowloon, Hong Kong Received 4th April 2001; returned for revisions 5th June 2001; revised manuscript accepted 2nd July 2001.Objective: To examine the test–retest reliability and construct validity of cervical active range of motion and isometric neck muscle strength as measured by the Multi Cervical Rehabilitation Unit (Hanoun Medical Inc., Ontario). Design: A cross-sectional study. Setting: Institutional practice. Subjects: Twenty-one patients with neck pain and 25 healthy volunteers. Methods: After a trial-run session, active range of motion (AROM) was measured in the subsequent two sessions, with 2–3 days in between. During each session, three measurements were taken for each direction ( exion, extension, lateral exions and rotations). The measurement of isometric strength was after a 15-minute break following completion of the measurement of AROM. Three measurements were made for each of the six directions ( exion, extension, lateral exions, protraction and retraction). The software of the Multi Cervical Rehabilitation Unit automatically recorded and calculated the maximum AROM and isometric strength. Results: There was a good to high level of reliability in the measurement of AROM for both groups of subjects, with intraclass correlation coef cients (ICCs) ranging from 0.81 to 0.96. Results also demonstrated very good to excellent reliability in isometric strength measurement (ICCs ranged from 0.92 to 0.99). Moreover, there was a signi cant difference in isometric neck muscle strength (p = 0.001) and in AROM (p = 0.034) between the two groups. Conclusions: The Multi Cervical Rehabilitation Unit was found to be reliable and valid for testing the cervical active range of motion and isometric neck muscle strength for both normal and patient subjects.Address for correspondence: Thomas TW Chiu, Department of Rehabilitation Sciences, The Hong Kong Polytechnic University, Hung Hom Kowloon, Hong Kong. e-mail: rstchiu@.hk © Arnold 2002Downloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.10.1191/0269215502cr550oa852TTW Chiu and SK Lo the use of neck active range of motion (AROM) measurements for impairment ratings, measuring AROM is still a very common assessment method used by clinicians. However, Cole 13 reported that clinical measurement of cervical spine motion has very low accuracy, due to the lack of bony landmarks on the head and the thickness of soft tissues overlying segments of cervical spine. One of the most commonly used methods, as suggested by Moll and Wright, 14 is visual estimation, but this method has been criticized as not reliable.15 Other measuring methods include electrogoniometers, radiographs and computerized tomography. The latter two involve radiation and are not advisable for repeated measures. Further, these instruments lack good control over the plane of movement, which may result in inaccurate measurement. After a comprehensive review of the literature from 1966 to 1998 using meta-analysis, Chen 8 concluded that radiography is not reliable for global cervical range of movement measurements, and there is no ‘gold standard’ in measuring neck AROM. There is a need to develop a reliable clinical measurement of neck AROM. Hence, we initiated this study to examine the test–retest reliability and construct validity of the AROM and isometric muscle strength testing in the neck with a Multi Cervical Rehabilitation Unit (MCRU). Methods Subjects As we planned to carry out a contrast-group comparison, we adopted this approach for sample size calculations. Using a software package,16 it was estimated that a total of approximately 44 subjects, i.e. 22 subjects in each of the patient and control groups, would be required. The following parameters were used as inputs to the program: (1) 0.05 alpha; (2) 0.9 power; (3) two-sided alternative; (4) an effect size of 0.5 – this was chosen because an effect size of 0.5–0.7 was considered moderate by Cohen.17 Twenty-one subjects (12 females and 9 males) aged between 19 and 46 years (mean 27.0, SD 9.5) with a diagnosis of mechanical neck pain by the same doctor in a university health centreIntroduction Neck pain is a very common spinal symptom. In a nationwide survey conducted in Sweden, the prevalence of persistent neck pain was found to be 30%.1 Hasvold and colleagues2 reported a prevalence of 26% in Finland. In a household survey conducted in Hong Kong, 800 men and women over 30 years old were interviewed. The one-year prevalence of neck pain was 15% in men and 17% in women.3 Moreover, Kamwendo4 and Maeda5 suggested that the prevalence of neck pain is high among sedentary workers and the number is increasing. In a recent populationbased cross-sectional mailed survey in Saskatchewan, Cote 6 reported that the age-standardized lifetime prevalence of neck pain was 66.7% and the point prevalence was 22.2%. It is costly in terms of treatment, individual suffering, and time lost due to work absentee.7 Despite its high incidence, studies of neck pain are sparse. Objective assessment of neck pain in the clinical eld includes measurement of the range of movement, palpation and X-ray ndings, which are inadequate to re ect the signs and symptoms of neck pain.8 There is a need for the development of a reliable objective clinical assessment which can be used to relate to patients’ signs and symptoms. Barton and Hayes9 compared the neck muscle strength, ef ciency and relaxation times in normal people and subjects with neck pain. They found that all force values were signi cantly lower in individuals with neck pain. A number of studies10–12 have demonstrated that neck isometric strength measurement is a useful and practical method to show objectively a functional improvement in response to rehabilitation. However, the above studies only reported the isometric strength of exion and extension. There is little research that investigates the isometric strength of other directions: lateral exions, protraction and retraction. Weakness in these directions may go undetected. Clinically, the actual functioning of the neck muscles has not been studied. A major reason for the paucity of study is the lack of reliable equipment to accurately and safely quantify cervical muscle strength in different directions. Although controversy still exists concerningDownloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.Cervical range of motion and neck muscle strength were randomly selected from a list available in the rehabilitation clinic of the same university. Twenty- ve healthy volunteers (10 females and 15 males) aged between 20 and 39 years (mean 22.1, SD 3.9) without neck pain during the past year were recruited by advertisement on a notice board within the university. Informed consent was obtained from all subjects. Documented consent was obtained from each subject and the project was approved by the University’s Review Board for Health Sciences Research involving Human Subjects. Multi Cervical Rehabilitation Unit The unit is a newly developed apparatus for measuring the active range of motion of the neck and the isometric strength of neck muscles (Figure 1). AROM measurements can be taken in the direction of exion, extension, lateral exions and rotations. Isometric muscle strength can be measured in the directions exion, extension, lateral exions, protraction and retraction, and even in combined directions. The unit is equipped with an armchair that rotates 90° for measurement of lateral exions, with adjustable seat height, lumbar support and armrests, and a shoulder restraint system to secure the subject within the seat in order to isolate the cervical spine during testing. It also contains a unique head assembly system (movable inner and outer head brace) designed to cause the subject’s head to move safely in different planes. The inner brace is used when positioning subjects for the various tests during exion, extension and lateral exion movements. The outer brace is used during rotation movements and to control overall movement of the head assembly. Within the inner head brace, a load cell can be inserted to measure isometric strength (Figure 2a). The load cell is connected to the computer so that information is collected automatically. A exion and an extension pad can be inserted into the inner brace in order to ‘hold’ the subject’s head comfortably during measurement of active range of motion (Figure 2b). A potentiometer is also tted into the inner head brace for automatic measurement of range of motion. The MCRU has a built-in calibration function. The load cell was calibrated by applying no force rst, and then by applying standard weights853between 10 and 50 lb (4.5–22.7 kg). The potentiometer was calibrated by rst setting the outer brace at 0° rotation and then to 90° rotation to the left. The inner brace was then set at 70° exion for calibration of movement in the sagittal plane. Range of movement measurement The subjects underwent AROM measurement in three sessions (S1, S2, S3), with 2–3 days between each session. Three measurements were made for each direction ( exion, extension, lateral exions and rotations) at each session. The rst session was used as a trial run, to allow the subjects to become familiar with the procedures. During theFigure 1 Multi Cervical Rehabilitation Unit (Hanoun Medical Inc., Ontario).Downloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.854TTW Chiu and SK LoFigure 2 Accessories of the MCRU: (a) load cell tted within inner head brace; (b) head assembly system with exion and extension pad tted within inner head brace.measurement, the subject sat comfortably upright in the adjustable chair, and the trunk was secured with the shoulder restraint system, to isolate cervical from thoracic motion. The seat height was adjusted so that the lower portion of the exion pad met the upper portion of the subject’s eyebrow. The armrests were adjusted so that the subject’s elbows were at 90° with the forearm, parallel to the ground. The subject’s cervical spine was aligned with the side bar of the outer brace to attain a neutral head position by adjusting the exion or extension pads inserted onto the inner brace, which were then fastened in place to ‘hold’ the subject’s head comfortably. The seat height and the position of the exion and the extension pads were documented for repeated testings. After that, the subject was instructed to do three consecutive free active movements (in different directions for testing exion, extension, lateral exions and rotations, randomly) as far as they could, and to return to neutral each time, with 10 seconds’ rest in between each movement and 2 minutes’ rest between different directions. All the ranges of movement were automatically measured by the potentiometer tted into the head assembly system, which was connected to the MRCU with the Objective Documentation and Evaluation System (ODES™ system) through a direct system interface. The ODES system automatically recorded (sampling rate 20/second) and calculated the average and the maximum degrees of motion among the three trials.Isometric strength measurement Measurement of isometric strength was carried out after a 15-minute break following completion of the measurement of range of movement. Again, three measurements were taken for each of the six directions randomly ( exion, extension, lateral exions, protraction and retraction) at each session. During the measurement, the subject again sat in the adjustable chair with his/her trunk secured by the shoulder restraint system. Both the seat height and the position of the armrest were recorded to ensure a standardized position for repeated testings. The inner head brace was secured comfortably around the head of the subject. A load cell tted into the brace was used to measure the isometric force applied by the subject for the six directions. The subject was instructed to do three consecutive steady contractions (in different directions for testing different muscle groups) as hard as possible, with 10 seconds’ rest between each contraction and 2 minutes’ rest between different directions to avoid fatigue within a session. The load cell was connected to the MRC unit with an objective documentation and evaluation system through a direct system interface. The system’s software automatically recorded (sampling rate 20/second) and calculated the average and peak isometric strength (PIS) for six different directions among the three trials. Data management The rst session was used as a trial run so that the subjects could become familiar with the pro-Downloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.Cervical range of motion and neck muscle strength cedure and the machine. Data collected from the second and third sessions were used for analysis. Reliability was assessed using the two-way nested ANOVA random model, as described in Safrit, 18 and the corresponding intraclass correlation coefcient (ICC). This model was considered most appropriate in our study because three measurements (trials) were taken within each of the two sessions, so that statistically, ‘trials were nested within sessions which were nested within subjects’. In this model, both trial-to-trial and session-to-session variations were identi ed as error variance, while the third source of variation, between subjects, was considered true variance. This ICC was chosen because both inter- and intra-session variability can be assessed simultaneously. The inter- and intra-session reliability will need to be analysed separately only when this ICC value is low. In addition, analysis of variance (ANOVA) was used to conduct a contrastgroup comparison of mean muscle strength and AROM between the patient and normal groups, as a means to assess construct validity. The Sharpened Bonferroni method 19 was applied to adjust for the alpha level when multiple testings were performed. Results Intraclass correlation coef cients (ICCs) and 95% con dence intervals for all the AROM tests (six directions) for the patient and the normal855groups are presented in Table 1. Results demonstrated that there is a good to high level of test–retest consistency and reliability (as de ned in Blesh20) in the measurement of range of movement for both the normal and the symptomatic group. The ICC values ranged from 0.81 to 0.96. Further analysis using ANOVA demonstrated that there was difference in some of the AROM parameters between the normal and symptomatic groups. The signi cance was mainly attributed to the difference in the direction of extension (F = 11.89; df = 1,44; p = 0.001) and to some extent to the direction of the right lateral exion (F = 3.80; df = 1,44; p = 0.058) and exion (F = 3.44; df = 1,44; p = 0.070). Intraclass correlation coef cients and 95% con dence intervals for maximal isometric strength measurements (six directions) for the patient and normal groups are presented in Table 2. Results demonstrate that very good to excellent test–retest consistency was obtained in isometric strength measurement for both the normal and symptomatic groups, as the ICCs ranged from 0.92 to 0.99. Again, further analysis using ANOVA demonstrated that there was signi cant difference in isometric neck muscle strength between the normal group and the symptomatic group. The differences in all six directions were signi cant even after adjusting for individual alpha level using the Sharpened Bonferroni method.Table 1 VariableIntraclass correlation coef cients (ICCs) and mean value for AROM test in six different directions Normal (95% CI) (N = 25) 0.81 (0.59, 0.93) 0.94 (0.70, 0.99) 0.93 (0.88, 0.95) 0.96 (0.93, 0.97) 0.85 (0.71, 0.92) 0.82 (0.65, 0.92) Mean ± SD (degrees) 68.0 ± 6.19 68.3 ± 7.33 49.8 ± 7.47 52.6 ± 7.60 78.0 ± 6.41 77.2 ± 7.63 Patient (95% CI) (N = 21) 0.96 (0.89, 0.98) 0.95 (0.88, 0.98) 0.91 (0.85, 0.95) 0.82 (0.66, 0.92) 0.87 (0.76, 0.95) 0.90 (0.82, 0.95) Mean ± SD (degrees) 64.0 ± 8.62 60.1 ± 8.84 45.8 ± 6.15 50.3 ± 6.25 74.8 ± 7.67 72.8 ± 10.5 p-valueFlexion Extension Right lateral exion Left lateral exion Right rotation Left rotation0.070 0.001a 0.058 0.271 0.137 0.10795% CI, 95% con dence interval. a p-value for comparing AROM between normal and patient groups was still signi cant after the Sharpened Bonferroni adjustment.Downloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.856TTW Chiu and SK LoTable 2 Intraclass correlation coef cients (ICCs), and mean value for maximal isometric strength measurement in six different directions Variable Normal (95% CI) (N = 25) 0.98 (0.91, 0.99) 0.98 (0.95, 0.99) 0.95 (0.89, 0.98) 0.97 (0.95, 0.98) 0.95 (0.90, 0.97) 0.94 (0.84, 0.98) Mean ± SD (N) 74.5 ± 19.6 93.3 ± 34.0 65.7 ± 19.2 66.9 ± 16.4 74.8 ± 17.6 78.9 ± 21.5 Patient (95% CI) (N = 21) 0.99 (0.97, 1.0) 0.95 (0.90, 0.99) 0.92 (0.74, 0.97) 0.94 (0.89, 0.97) 0.99 (0.97, 1.0) 0.97 (0.95, 0.99) Mean ± SD (N) 56.7 ± 24.5 67.4 ± 27.3 52.4 ± 21.2 50.6 ± 22.9 52.9 ± 26.1 51.7 ± 21.5 p-valueaFlexion Extension Right lateral exion Left lateral exion Protraction Retraction0.009 0.007 0.030 0.007 0.002 0.00095% CI, 95% con dence interval. a All the p-values for comparing maximal isometric strength between normal and patient groups remained signi cant after the Sharpened Bonferroni adjustment.Discussion In determining the level of reliability, we have adapted a previously reported scheme20 for de ning the degrees of reliability based on ICC values: 0.90–0.99, high reliability; 0.80–0.89, good reliability; 0.70–0.79, fair; and 0.69 and below, poor reliability. Results of the current study show that our method of measuring the AROM of the neck in both normal and symptomatic subjects has good to high reliability in all directions of movement. Youdas21 studied the reliability of a ‘cervical-range-of-motion’ instrument for measurement of AROM in 26 healthy subjects. Results of his study demonstrated that test–retest reliability was fair for neck exion (ICC = 0.76, compared with 0.81 in our study); high for neck extension (ICC = 0.94; same in our study); andClinical messages The Multi Cervical Rehabilitation Unit is sensitive enough to detect differences in active range of motion and strength, between normal subjects and symptomatic patients. There was signi cant difference in isometric neck muscle strength and cervical active range of motion between the normal and symptomatic groups.good for left lateral exion (ICC = 0.86; 0.96 in our study), right lateral exion (ICC = 0.85; 0.93 in our study), left rotation (ICC = 0.84; 0.82 in our study), and right rotation (ICC = 0.80; 0.85 in our study). Kuhlman22 measured the AROM in 31 healthy subjects (16 men and 15 women aged 20–30) using a gravity goniometer. Kuhlman22 reported similar range of motion in all directions as compared with our current study, except that a larger range in rotation was demonstrated in his study. However, our results in rotation measurement (right rotation = 78°, left rotation = 77°) are similar to those reported by Penning and Wilmink.23 It is generally accepted that cervical AROM is decreased in patients with neck pain.8,9 The current study also demonstrates that there is signi cant difference in AROM between nonsymptomatic subjects and patients with neck pain, at least for extension and to some degree exion and right lateral exion. There is increasing clinical evidence that supports the ef cacy of muscular strengthening in neck rehabilitation programmes.10,24 Therefore, there is a need for a reliable measurement of cervical strength for the evaluation of exercise training protocols. The results of the present study demonstrate high test–retest reliability in cervical isometric strength measurement in both the patient and normal groups. In a recent study, Jordan and co-workers10 studied the reliability of measuring the isometric strength of the neck muscles in 12 healthy subjects with a strain-gauge dynamometer (Neck Exercise Unit, Follo, Nor-Downloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.Cervical range of motion and neck muscle strength way). The result for maximal isometric strength in exion was ICC = 0.76 (compared with 0.98 in our study), and that for isometric strength in extension was ICC = 0.92 (compared with 0.98 in our study). Results of the present study also demonstrated better reliability than previous studies using other measuring devices, in the directions of exion and extension11,25 and in the directions of lateral exions.26 No previous study had reported the reliability of measuring the isometric strength in the directions of protraction and retraction, so no comparison could be made. However, our results showed that the MCRU was highly reliable on isometric strength measurement in protraction and retraction. The isometric muscle strength of exion and extension (74.5 N and 93.3 N) in normal subjects as reported in our study are similar to those reported by Jordan et al.27 for a similar age group and gender. For isometric muscle strength in the direction of lateral exions, the previous study by Vernon et al.26 demonstrated a higher result (right lateral exion = 79.3 N and left lateral exion = 85.1 N) than our current ndings (65.7 N and 66.9 N), probably because they measured 40 young adult males (average age 25). Further study is needed to establish a baseline reference of isometric neck muscle strength in different directions for different age groups and gender. A number of studies9,25,27 have reported that the patient populations had signi cantly less muscle strength than the control populations. Our ndings con rmed that the isometric neck muscle strength of nonsymptomatic subjects is signi cantly stronger than that of patients with neck pain. In comparison with previous studies,11,21,25 the current study has made the following improvements. All the measurement data were automatically documented through the computer software system Objective Documentation and Evaluation System (ODESTM). This helped to minimize the possibility of transcription and calculation errors. The measurement procedures were standardized, and computer-generated verbal instructions were given during measurement. Moreover, the trunk was secured rmly with the shoulder restraint system, to isolate cervical from thoracic motion, in order to minimize procedural error.8 Two groups of people were recruited857(patient and the healthy groups) so that the results of this study have better generalizability. As there is no ‘gold standard’ in the measurement of AROM8 and isometric neck muscle strength, it is not possible for the current study to establish validity by direct comparison. This might be the limitation of this study. In order to overcome this, we adopted the method of contrast group comparison to compare mean isometric muscle strength and AROM between the patient and normal groups, as a method of assessing validity. Another limitation of the study is that the MCRU is not able to measure AROM in the direction of protraction and retraction. Moreover, isometric muscle strength in the direction of rotations is not measurable with this machine. The results of the ANOVA demonstrate that there is signi cant difference in AROM between the normal and the symptomatic groups, but the difference between the two groups is largely attributable to the direction of extension and to a certain degree by the right lateral exion and exion. More in-depth study in the difference of AROM between normal and symptomatic groups is warranted. Due to the limited number of subjects who participated in this study, and the possibility of selection bias in the recruitment of normal subjects, the AROM and isometric muscle strength results cannot be regarded as a baseline reference for the particular group. Further study with a larger sample size involving different age groups is recommended. Conclusion Results demonstrate that there is a high degree of test–retest reliability in testing active range of motion and isometric neck muscle strength for both normal subjects and those with neck pain by using the Multi Cervical Rehabilitation Unit. To be clinically useful, an instrument should be able to distinguish normal subjects from patients with pathological conditions, who are truly impaired. The current study has demonstrated signi cant difference in the AROM and isometric neck muscle strength for patients and normal subjects. With increasing demand being placed on evidence-based practice, a valid, reliable outcome-Downloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.858TTW Chiu and SK Lo12 Ylinen J, Ruuska J. Clinical use of neck isometric strength measurement in rehabilitation. Arch Phys Med Rehabil 1994; 75: 465–69. 13 Cole TM. Measurement of musculoskeletal function: goniometry. In: Kottke FJ, Stillwell GK, Lehmann JF eds. Krusens’s handbook of physical medicine and rehabilitation, third edition. Philadelphia: Saunders, 1982. 14 Moll JMH, Wright V. Measurement of joint motion. Clin Rheum Dis 1976; 2: 3–26. 15 Youdas JW, Carey JR, Garrett TR. Reliability of measurements of cervical spine range of motion – comparison of three methods. Phys Ther 1991; 71: 98–106. 16 Hintze JL. Power Analysis and Sample Size for Windows. PASS, NCSS, Kaysville, Utah, USA, 1996. 17 Cohen J. Statistical power analysis for the behavioural sciences. New York: Academic Press, 1977. 18 Safrit MJ, ed. Reliability theory. Physical education and recreation. American Alliance for Health, 1976: 32–35. 19 Hochberg Y, Benjamini Y. More powerful procedure for multiple signi cance testing. Stat Med 1990; 9: 811–18. 20 Blesh TE. Measurement in physical education, second edition. New York: The Ronald Press Co, 1974. 21 Youdas JW, Garrett TR, Suman VJ, Bogard CL, Hallman HO, Carey JR. Normal range of motion of the cervical spine: an initial goniometric study. Phys Ther 1992; 72: 770–80. 22 Kuhlman KA. Cervical range of motion in the elderly. Arch Phys Med Rehabil 1993; 74: 1071–79. 23 Penning L, Wilmink JT. Rotation of the cervical spine. A CT study in normal subjects. Spine 1987; 12: 732–38. 24 Highland TR, Dreisinger TE, Laura LV, Russell GS. Changes in isometric strength and range of motion of the isolated cervical spine after eight weeks of clinical rehabilitation. Spine 1992; 17(6 suppl): S77–82. 25 Silverman JL, Rodriquez AA, Agre JC. Quantitative cervical exor strength in healthy subjects and in subjects with mechanical neck pain. Arch Phys Med Rehabil 1991; 72: 679–81. 26 Vernon HT, Aker P, Aramenko M, Battershill D, Alepin A, Penner T. Evaluation of neck muscle strength with a modi ed sphygmomanometer dynamometer: reliability and validity. J Manipulative Physiol Ther 1992; 15: 343–49. 27 Jordan A, Mehlsen J, Bülow PM, Østergaard K, Danneskiold-Samsøe B. Maximal isometric strength of the cervical musculature in 100 healthy volunteers. Spine 1999; 24: 1343–48.measuring tool will contribute to better service and evaluation. Acknowledgements The project was supported by the Area of Strategic Development Fund of the Hong Kong Polytechnic University and the Health Services Research Fund of the Hong Kong Hospital Authority. References1 Andersson HI, Ejlertsson G, Leden I, Rosenberg C. Chronic pain in a geographically de ned general population: studies of differences in age, gender, social class, and pain localization. Clin J Pain 1993; 9: 174–82. 2 Hasvold T, Johnsen R. Headache and neck or shoulder pain – frequent and disabling complaints in the general population. Scand J Prim Health Care 1993; 23: 127–33. 3 Lau EMC, Sham A, Wong KC. The prevalence of and risk factors for neck pain in Hong Kong Chinese. J Public Health Med 1996; 18: 396–99. 4 Kamwendo K, Linton SJ, Mortiz U. Neck and shoulder disorders in medical secretaries. Part I: Pain prevalence and risk factors. Scand J Rehabil Med 1991; 23: 127–33. 5 Maeda K. Occupational cervicobrachial disorder and its causative factor. J Hum Ergol 1977; 6: 193–202. 6 Cote P, Cassidy DJ, Carroll L. The Saskatchewan health and back pain survey. The prevalence of neck pain and related disability in Saskatchewan adults. Spine 1998; 23: 1689–98. 7 Rempel DM, Harrison RJ Barnhart S. Work related cumulative trauma disorders of the upper extremity. JAMA 1992; 267: 838–42. 8 Chen J, Solinger AB, Poncet JF, Lantz CA. Meta-analysis of normal cervical motion. Spine 1999; 24: 1571–78. 9 Barton PM, Hayes KC. Neck exor muscle strength, ef ciency, and relaxation times in normal subjects and subjects with unilateral neck pain and headache. Arch Phys Med Rehabil 1996; 77: 680–87. 10 Jordan A, Bendix T, Nielsen H, Hansen FR, Host D, Winkel A. Intensive training, physiotherapy, or manipulation for patients with chronic neck pain: A prospective, single-blinded, randomized clinical trial. Spine 1998; 23: 311–19. 11 Leggett SH, Graves JE, Pollock ML et al. Quantitative assessment and training of isometric cervical extension strength. Am J Sports Med 1991; 19: 653–59.Downloaded from at PENNSYLVANIA STATE UNIV on April 14, 2008 © 2002 SAGE Publications. All rights reserved. Not for commercial use or unauthorized distribution.。
MIL-PRF-6081D
INCH-POUNDMIL-PRF-6081D10 November 1997SUPERSEDINGMIL-L-6081C15 April 1964PERFORMANCE SPECIFICATIONLUBRICATING OIL, JET ENGINEThis specification is approved for use by all Departments andAgencies of the Department of Defense.1. SCOPE1.1 Scope. This specification covers the requirements for two grades of jet engine lubricating oil.1.2 Classification. The lubricating oil will be furnished in the following grades, as specified:Grade NATO Symbol100510100-133Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: ASC/ENSI, 2530 Loop Road W, Wright-Patterson AFB OH 45433-7101, by using the self-addressed Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document, or by letter.AMSC N/A FSC 9150 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.2. APPLICABLE DOCUMENTS2.1 General. The documents listed in this section are specified in sections 3 and 4 of this specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed.2.2 Government documents2.2.1 Specifications, standards, and handbooks. The following specifications, standards, and handbooks form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents will be those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solicitation (see 6.2).STANDARDSFEDERALFED-STD-791Lubricants, Liquid Fuels, and Related Products; Methods of Testing MILITARYMIL-STD-290Packaging of Petroleum and Related Products(Unless otherwise indicated, copies of the above specifications, standards, and handbooks are available from the Defense Automated Printing Service, 700 Robbins Avenue, Bldg 4D, Philadelphia PA 19111-5094.)2.2.2 Other government documents, drawings, and publications. The following other Government documents drawings, and publications form a part of this document to the extent specified herein. Unless otherwise specified the issues are those cited in the solicitation.CODE OF FEDERAL REGULATIONS (CFR)DEPARTMENT OF LABOR29 CFR 1910.1200Occupational Safety and Health Standards – Hazard Communications2.3 Non-government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of the documents which are DoD adopted are those listed in the issue of the DoDISS cited in the solicitation. Unless otherwise specified, the issues of documents not listed in the DoDISS are the issues of the documents cited in the solicitation (see 6.2).AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM)ASTM D92Standard Test Method for Flash and Fire Points by Cleveland OpenCup, (AASHTO No. T48) (DoD-adopted)ASTM D97Standard Test Method For Pour Point of Petroleum OilsASTM D130Standard Test Method for Detection of Copper Corrosion from PetroleumProducts by the Copper Strip Tarnish TestASTM D445Standard Test Method for Kinematic Viscosity of Transparent andOpaque Liquids (the Calculation of Dynamic Viscosity)(DoD adopted)ASTM D974Standard Test Method for Acid and Base Number By Color-IndicatorTitrationASTM D1500Standard Test Method for ASTM Color of Petroleum ProductsASTM D2273Standard Test Method for Trace Sediment in Lubricating Oils(DoD adopted)ASTM D2532Standard Test Method for Viscosity and Viscosity Change AfterStanding at Low Temperature of Aircraft Turbine Lubricants(DoD adopted)ASTM D4636Standard Test Method for Corrosiveness and Oxidation Stability ofHydraulic Oils, Aircraft Turbine Engine Lubricants, and Other HighlyRefined Oils(Application for copies should be addressed to the American Society for Testing and Materials, 100 Barr Harbor Drive, West Conshohocken PA 19428-2959.)2.4 Order of precedence. In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.3. REQUIREMENTS3.1 Qualification. The jet engine lubricating oils furnished under this specification shall be products which are authorized by the qualifying activity for listing on the applicable qualified products list at the time of award of contract (see4.2 and 6.3).3.2 Materials. The composition of this lubricating oil is not limited; however, viscosity index improvers and known or suspected human carcinogens (as defined by the Occupational Safety and Health Standards – Hazard Communications, 29 CFR 1910.1200) are prohibited. The lubricating oil may contain oxidation inhibitors and pour-point depressants. The engine lubricating oil shall have no adverse effect on the health of personnel when used for its intended purpose. Recycled basestocks are permitted; however, each batch must be fully tested in accordance with all qualification requirements of this specification. The manufacturer may be required to submit certification of conformance to this paragraph (see 6.2).3.2.1Ozone depleting chemicals. The following tests currently require the use of toxic or ozone depleting chemicals (ODCs), but an acceptable substitute has been identified for each test.ASTM Test Method Toxic Chemicals/ODC SubstanceAcceptable SubstitutesASTM D2532Viscosity and Viscosity ChangeAfter Standing at Low Temperatureof Aircraft Turbine LubricantsToluene n-HeptaneASTM D4636Corrosiveness and Oxidation Stability of Hydraulic Oils, Aircraft Turbine Engine Lubricants, and Other Highly Refined Oils Trichlorotrifluoroethane1,1,1-Trichloroethanen-HeptaneFederal Test MethodFTM 5308 Corrosiveness and Oxidation Stability of Light Oils (Metal Squares)1,1,1-Trichloroethane n-HeptaneorAcetone3.3 Chemical and physical requirements. All classifications of the finished lubricating oil shall conform to the requirements listed in section 3 and table I when tested in accordance with the applicable test methods.TABLE I. Chemical, physical, and performance requirements.Characteristic Requirement Test MethodGrade 1005Grade 1010ASTM FED-STD-791 Acid number (T.A.N.), mg KOH/g0.10 max 1/0.10 max 1/D974Viscosity at:37.8°C (100°F), cs 5.0 min10.0 min D445-40°C (-40°F), cs3000 max D2532-54°C (-65°F), cs2600 max D2532Viscosity stability cs, % change@ 3 hours:-54ºC (-65ºF) -40ºC (-40ºF)3 max 2/2 max 2/D2532Flash point, °C(°F)107(225) min132(270) min D92 Pour point, ºC(ºF)-57(-70)max D97 ASTM Color No. 5.5 max No. 5.5 max D1500 Copper strip corrosion at 121ºC(250ºF) 1 max 1 max D130 Corrosion and oxidation stabilityat 121ºC (250ºF).3/Post Test Oil PropertiesViscosity change, % 4/ Acid number change Sludge volume, ml-5 to +20 max0.2 maxno visible sludge-5 to +20 max0.2 maxno visible sludgeD4636FTM 53085/Post Test Metal Specimen Weight change, mg/cm26/CopperSteelAluminum alloyMagnesium alloyCadmium-plated steel ±0.2 max±0.2 max±0.2 max±0.2 max±0.2 max±0.2 max±0.2 max±0.2 max±0.2 max±0.2 maxTrace sediment, (ml / 200 ml of oil) 7/0.005 ml max 8/0.005 ml max 8/D22731/Titrate to a pH 11 end point.2/Viscosity measurements taken at the specified temperature after three hours at test temperature, 121ºC (250ºF).3/ Measurements taken after metal has been subjected to the lubricating oil for 168 hours at 121ºC (250ºF).4/Compared with viscosity of new oil samples tested at 37.8ºC (100ºF).5/ When substituting heptane or acetone for 1,1,1-trichloroethane, use the heptane or acetone at ambient temperature; do not heat asrequired by paragraphs 6.6.1 and 6.10.1 of FTM 5308.6/ There shall be no pitting etching or visible corrosion on the surface of any of the metals when viewed under a magnification of 20diameters. A slight brown stain on the surface of the copper shall be permitted, but dark brown, gray, or black stain shall be cause for rejection. A slight discoloration of the cadmium will be permitted.7/When using Method D2273 to determine presence of trace sediment in the lubricating oil, no diluents shall be used.8/Measurements taken after centrifuging.3.4 Workmanship. The finished lubricating oil shall be transparent and uniform in appearance, and free from cloudiness, suspended matter, or other adulterations when examined visually by transmitted light.3.5 Material safety data sheets. Material safety data sheets shall be prepared and submitted in accordance with FED-STD-313 (see 6.4).4. VERIFICATION4.1 Classification of inspections. The inspection and testing of lubricating oils shall be classified as follows:a.Qualification inspection (see 4.2).b.Conformance inspection (see 4.3).4.2 Qualification inspection. Qualification inspection shall consist of testing to all the requirements specified in section 3 and table I. When required by the qualifying activity, additional evaluations may be required on candidate formulations.4.2.1 Qualification inspection sample. The qualification test sample shall consist of two gallons of finished lubricating oil, one gallon of the petroleum oil-base stock before the addition of ingredients, and one ounce of each of the additive ingredients used in the manufacture of the qualification sample; and shall be submitted prior to qualification. In the event that additives are supplied as concentrated solutions, an equivalent quantity of the solution shall be furnished. Each lubricant ingredient submitted shall be from the same bulk lot used in preparation of the qualification test sample. Upon receiving authorization from AFRL/PRSL, these samples shall be forwarded to AFRL/PRSL, Bldg 490, 1790 Loop Road North, Wright-Patterson AFB OH 45433-7103. Each sample shall be plainly identified by a securely attached, durable label marked with the following information:QUALIFICATION INSPECTION SAMPLELUBRICATING OIL, JET ENGINE,MIL-PRF-6081Type of sample: (basestock, additive, or finished oil)Classification of oil: (Grade 1005 or Grade 1010)Name of manufacturer:Product code number:Batch number:Date of manufacture:Submitted by (name) on (date) for qualification inspection in accordance with MIL-PRF-6081 underauthorization of (reference authorization letter, see 6.3).4.2.2 Qualification inspection test report. The manufacturer shall forward a letter to the activity responsible for qualification (see 6.3) before the test sample is supplied. The letter shall contain the following:a. Request for authorization to submit test sample for qualification.b. Certified test report that contains data on the specific batch of test sample to be submitted showing results ofthe tests specified herein.c. Complete formulation data, including chemical composition, percentages of each ingredient, themanufacturer and trade name of each ingredient, and the purity of each ingredient. Formulation data will be respected as highly proprietary information.d. Verification that the composition of the test sample complies with the requirements of 3.2.e. Identification of the manufacturing site of the specific batch of test sample to be submitted.f. MSDS (see 3.5) of the candidate product and for each of the additive components used in the formulation.4.2.3 Requalification. Requalification shall be required when any change is made in source of manufacture, purity, or composition of the lubricating oil base stocks or additives. A minor change in the oil formulation may be made without requalification testing, but only after notification to, and approval by, the qualifying activity (see 6.3). Each reformulation request shall include a certified test report (see 4.2.2).4.3 Conformance inspection. Conformance inspection of production lots shall consist of all the tests specified in table II. Failure of production lots to pass any of the conformance tests shall be cause for rejection of the lot.4.3.1 Sampling. Each bulk lot (see 6.7) of material shall be sampled at random in accordance with ASTM D4057 or ASTM D4177 for the conformance inspection tests (see 4.3).4.3.2 Inspection. Inspections shall be conducted in accordance with FED-STD-791, method 9601, “Inspection Requirements”4.3.2.1 Examination of filled containers. A random sample of filled containers from each lot (see 6.7), taken in accordance with ASQC-Z1.4, shall be examined for conformance to MIL-STD-290 with regard to fill, closure, sealing, leakage, packaging, packing, and markings. Reject any container having one or more defects or for being under the required fill. If the number of defective or underfilled containers exceeds the acceptance number for the appropriate sampling plan of ASQC-Z1.4, reject the lot represented by the sample.4.3.3 Conformance inspection test report. A copy of the conformance inspection report on each lot of oil produced for US Government use shall be forwarded to the Propulsion Directorate, AFRL/PRSL, Bldg 490, 1790 Loop Road North, Wright-Patterson AFB OH 45433-7103.4.4 Test methods. All tests shall be performed in accordance with tables I and II.4.4.1 Reported data. Test results of all determinations shall be included in reporting data.TABLE II: Conformance tests.Test Test MethodCharacteristic Paragraph ASTMCopper strip corrosion (see table I)--D130Viscosity stability at -54ºC (-65ºF)and –40ºC (-40ºF), %1/--D2532Acid number, mg KOH/g(see table I)--D974Viscosity (see table I), cSt at 37.8 °C (100 °F)at -40 °C (-40 °F)at –54 °C (-65°F)--D445D445D2532Flash point ºC (ºF). (see table I)--D92Pour point ºC (ºF). (see table I)--D97ASTM color (see table I)--D1500Trace sediment in lubricating oils(see table I)--D2273 1/ Viscosity measurements taken at the specified temperature after three hours at test temperature, 121ºC (250ºF).5. PACKAGING5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract or order (see6.2). When actual packaging of material is to be performed by DoD personnel, these personnel need to contact the responsible packaging activity to ascertain requisite packaging requirements. Packaging requirements are maintained by the Inventory Control Point’s packaging activity within the Military Department or Defense Agency, or within the Military Department’s System Command. Packaging data retrieval is available from the managing Military Department’s or Defense Agency’s automated packaging files, CD-ROM products, or by contacting the responsible packaging activity.6. NOTES(This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.)6.1 Intended use. The lubricating oil procurable to this specification is intended for the use in specific models of aircraft jet engines.6.2 Acquisition requirements. Acquisition documents should specify the following:a.Title, number, grade, and date of this specification, including any amendments.b.Issue of DoDISS to be cited in the solicitation and, if required, the specific issue of individual documentsreferenced (see 2.2 and 2.3).c.Type and size of containers required (see 5.1).d.Quantity desired.e.Submittal of conformance test results (see 4.3.3).f.If certification of conformance to material prohibitions is required (see 3.2).6.3 Qualification. With respect to products which require qualification, awards will be made only for products which are, at the time of award of contract, qualified for inclusion in QPL-6081 whether or not such products have actually been so listed by that date. The attention of the contractors is called to these requirements, and manufacturers are urged to have the products they propose to offer to the Federal Government tested for qualification in order that they may be eligible to be awarded contracts or purchase orders for the products covered by this specification. The activity responsible for the Qualified Products List is the Propulsion Directorate, ATTN:AFRL/PRSL, Bldg 490, 1790 Loop Road North, Wright-Patterson AFB OH 45433-7103, and information pertaining to qualification of products may be obtained from that activity. To initiate the qualification process, prospective suppliers will forward a written request for such action to the Propulsion Directorate at the above address. This letter will contain general information on the proposed candidate material. The Propulsion Directorate will respond, providing detailed instructions for the submission of product samples and test data.6.3.1 Reblend lubricating oil qualification. A reblend lubricating oil is an original qualified lubricating oil as specified in 4.2, in which one or more ingredients have been blended by a manufacturer other than the manufacturer of the original formulation. A bulk lot of the reblended oil will be subjected to the qualification tests (see 4.2). Reblend approvals may be initiated by the process described in 6.3.6.3.2 Rebrand lubricating oil qualification. A rebrand lubricating oil is a qualified, fully-formulated oil which has successfully passed all qualification tests (see 4.2) and is manufactured by the original formulator at the original manufacturing site but which is packaged by a supplier other than the manufacturer of the fully-formulated oil. Rebrand approvals may be initiated by the process described in 6.3.6.4 Material Safety Data Sheets. Contracting officers will identify those activities requiring copies of completed Material Safety Data Sheets prepared in accordance with FED-STD-313. The pertinent Government mailing addresses for submission of data are listed in FED-STD-313.6.5 Subject term (key word) listing.a ircraft engine oilpetroleum productturbine engine lubricating oilviscosity6.6 International standardization agreements. Certain provisions of this specification are the subject of international standardization agreements (ASCC Air Standard 15/9 and STANAG 1135). When amendment, revision, or cancellation of this specification is proposed which will modify the international agreement concerned, the preparing activity will take appropriate action through international standardization channels, including departmental standardization offices, to change the agreement or make other appropriate accommodations.6.7 Definitions.Bulk lot - A bulk lot is defined as an indefinite quantity of a homogeneous mixture of materialoffered for acceptance in a single, isolated container or manufactured by a single plant run(not to exceed 24 hours), through the same processing equipment, with no change iningredient material.Packaged lot - A packaged lot is defined as an indefinite number of 208-liter (55-gallon) drums, orsmaller unit packages of identical size and type, offered for acceptance and filled with ahomogeneous mixture of material from one isolated container; or filled with ahomogeneous mixture of material manufactured by a single plant run (not to exceed 24hours), through the same processing equipment, with no change in ingredient material. 6.8 Changes from previous issue. Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes. The changes are due to Acquisition Reform initiatives requiring Government specifications to be performance-based. These changes have no impact on the chemical, physical, or performance requirements with respect to the previous issue.Custodians:Preparing activity: Air Force - 11Air Force - 11Navy – AS(Project. 9150-0818)STANDARDIZATION DOCUMENT IMPROVEMENT PROPOSALINSTRUCTIONS1. The preparing activity must complete blocks 1, 2, 3, and 8. In block 1, both the document number and revision letter shouldbegiven.2. The submitter of this form must complete blocks 4, 5, 6, and 7.3. The preparing activity must provide a reply within 30 days from receipt of the form.NOTE: This form may not be used to request copies f documents, nor to request waivers, or clarification of requirements on current contracts. Comments submitted on this form do not constitute or imply authorization to waiver any portion of the referenced document(s) or to amend contractual requirements.I RECOMMEND A CHANGE: 1. DOCUMENT NUMBERMIL-PRF6081D 2. DOCUMENT DATE (YYMMDD)9711103. DOCUMENT TITLELUBRICATING OIL, JET ENGINE4. NATURE OF CHANGE (Identify paragraph number and include proposed rewrite, if possible. Attach extra sheets as needed.)5. REASON FOR RECOMMENDATION6. SUBMITTERa. NAME (Last, Middle Initial)b. ORGANIZATIONc. ADDRESS (include Zip Code)d. TELEPHONE (Include Area Code)(1) Commercial e. DATE SUBMITTED(YYMMDD)(2) AUTOVON(If applicable)8. PREPARING ACTIVITYa. NAMEb. TELEPHONE (Include Area Code)ASC/ENSIAir Force Code 11(1) Commercial(937) 255-0175(2) AUTOVON785-0175c. ADDRESS (Include Zip Code)2530 Loop Road WestWright-Patterson AFB OH 45433-7101IF YOU DO NOT RECEIVE A REPLY WITHIN 45 DAYS, CONTACT: Defense Quality and Standardization Office5203 Leesburg Pike, Suite 1403, Falls Church, VA 22041-3466 Telephone (703) 756-2340 AUTOVON 289-2340DD FORM 1426, OCT 89 (EF-V1) PREVIOUS EDITIONS ARE OBSOLETE。
1999年AMC8试题
19991(6?3)+4−(2−1)=5.To make this statement true,the question mark between the 6and the 3should be replaced by(A)÷(B)×(C)+(D)−(E)None of these 2What is the degree measure of the smaller angle formed by the hands of a clock at 10o’clock?(A)30(B)45(C)60(D)75(E)903Which triplet of numbers has a sum NOT equal to 1?(A)(1/2,1/3,1/6)(B)(2,−2,1)(C)(0.1,0.3,0.6)(D)(1.1,−2.1,1.0)(E)(−3/2,−5/2,5)4The diagram shows the miles traveled by bikers Alberto and Bjorn.After four hours,about how many more miles has Alberto biked than Bjorn?B j o r n A l b e r t o 01234501530456075H O U R SM I L E S (A)15(B)20(C)25(D)30(E)355A rectangular garden 50feet long and 10feet wide is enclosed by a fence.To make the garden larger,while using the same fence,its shape is changed to a square.By how many square feet does this enlarge the garden?(A)100(B)200(C)300(D)400(E)5006Bo,Coe,Flo,Joe,and Moe have different amounts of money.Neither Jo nor Bo has as much money as Flo.Both Bo and Coe have more than Moe.Jo has more than Moe,but less than Bo.Who has the least amount of money?(A)Bo (B)Coe (C)Flo (D)Joe (E)Moe 7The third exit on a highway is located at milepost 40and the tenth exit is at milepost 160.There is a service center on the highway located three-fourths of the way from the third exit to the tenth exit.At what milepost would you expect to find this service center?(A)90(B)100(C)110(D)120(E)130This file was downloaded from the AoPS Math Olympiad Resources PagePage 119998Six squares are colored,front and back,(R=red,B=blue,O=orange,Y=yellow,G= green,and W=white).They are hinged together as shown,then folded to form a cube.The face opposite the white face isR BG YWO(A)B(B)G(C)O(D)R(E)Y9Threeflower beds overlap as shown.Bed A has500plants,bed B has450plants,and bedC has350plants.Beds A and B share50plants,while beds A and C share100.The totalnumber of plants isABC(A)850(B)1000(C)1150(D)1300(E)145010A complete cycle of a traffic light takes60seconds.During each cycle the light is green for 25seconds,yellow for5seconds,and red for30seconds.At a randomly chosen time,what is the probability that the light will NOT be green?(A)14(B)13(C)512(D)12(E)71211Each of thefive numbers1,4,7,10,and13is placed in one of thefive squares so that the sum of the three numbers in the horizontal row equals the sum of the three numbers in the vertical column.The largest possible value for the horizontal or vertical sum is1999(A)20(B)21(C)22(D)24(E)3012The ratio of the number of games won to the number of games lost(no ties)by the Middle School Middies is11:4.To the nearest whole percent,what percent of its games did the team lose?(A)24(B)27(C)36(D)45(E)7313The average age of the40members of a computer science camp is17years.There are20 girls,15boys,and5adults.If the average age of the girls is15and the average age of the boys is16,what is the average age of the adults?(A)26(B)27(C)28(D)29(E)3014In trapezoid ABCD,the sides AB and CD are equal.The perimeter of ABCD isA B CD8163(A)27(B)30(C)32(D)34(E)4815Bicycle license plates in Flatville each contain three letters.Thefirst is chosen from the set {C,H,L,P,R},the second from{A,I,O},and the third from{D,M,N,T}.When Flatville needed more license plates,they added two new letters.The new letters may both be added to one set or one letter may be added to one set and one to another set.What1999is the largest possible number of ADDITIONAL license plates that can be made by adding two letters?(A)24(B)30(C)36(D)40(E)6016Tori’s mathematics test had75problems:10arithmetic,30algebra,and35geometry prob-lems.Although she answered70%of the arithmetic,40%of the algebra,and60%of the geometry problems correctly,she did not pass the test because she got less than60%of the problems right.How many more problems would she have needed to answer correctly to earn a60%passing grade?(A)1(B)5(C)7(D)9(E)1117Problems17,18,and19refer to the following:At Central Middle School the108students who take the AMC8meet in the evening to talk about problems and eat an average of two cookies apiece.Walter and Gretel are baking Bonnie’s Best Bar Cookies this year.Their recipe,which makes a pan of15cookies,lists this items:1.5cupsflour,2eggs,3tablespoons butter,3/4cups sugar,and1package of chocolate drops.They will make only full recipes,not partial recipes.Walter can buy eggs by the half-dozen.How many half-dozens should he buy to make enough cookies?(Some eggs and some cookies may be left over.)(A)1(B)2(C)5(D)7(E)1518Problems17,18,and19refer to the following:At Central Middle School the108students who take the AMC8meet in the evening to talk about problems and eat an average of two cookies apiece.Walter and Gretel are baking Bonnie’s Best Bar Cookies this year.Their recipe,which makes a pan of15cookies,lists this items:1.5cupsflour,2eggs,3tablespoons butter,3/4cups sugar,and1package of chocolate drops.They will make only full recipes,not partial recipes.They learn that a big concert is scheduled for the same night and attendance will be down 25%.How many recipes of cookies should they make for their smaller party?(A)6(B)8(C)9(D)10(E)1119Problems17,18,and19refer to the following:At Central Middle School the108students who take the AMC8meet in the evening to talk about problems and eat an average of two cookies apiece.Walter and Gretel are baking Bonnie’s Best Bar Cookies this year.Their recipe,which makes a pan of15cookies,lists this items:1.5cupsflour,2eggs,3tablespoons butter,3/4cups sugar,and1package of chocolate drops.They will make only full recipes,not partial recipes.1999The drummer gets sick.The concert is cancelled.Walter and Gretel must make enough pans of cookies to supply 216cookies.There are 8tablespoons in a stick of butter.How many sticks of butter will be needed?(Some butter may be left over,of course.)(A)5(B)6(C)7(D)8(E)920Figure 1is called a ”stack map.”The numbers tell how many cubes are stacked in eachposition.Fig.2shows these cubes,and Fig.3shows the view of the stacked cubes as seen from the front.Which of the following is the front view for the stack map in Fig.4?Figure 1Figure 2Figure 3Figure 41234131224(A)(B)(C)(D)(E)21The degree measure of angle A is199940◦100◦110◦A(A)20(B)30(C)35(D)40(E)4522In a far-offland three fish can be traded for two loaves of bread and a loaf of bread can betraded for four bags of rice.How many bags of rice is one fish worth?(A)38(B)12(C)34(D)223(E)31323Square ABCD has sides of length 3.Segments CM and CN divide the square’s area intothree equal parts.How long is segment CM ?AMB CD N (A)√10(B)√12(C)√13(D)√14(E)√15199924When 19992000is divided by 5,the remainder is(A)4(B)3(C)2(D)1(E)025Points B ,D ,and J are midpoints of the sides of right triangle ACG .Points K ,E ,I aremidpoints of the sides of triangle ,etc.If the dividing and shading process is done 100times (the first three are shown)and AC =CG =6,then the total area of the shaded triangles isnearestA DE F (A)6(B)7(C)8(D)9(E)10The problems on this page are copyrighted by the Mathematical Association ofAmerica’s American Mathematics Competitions.。
MIL-STD-202G_NOTICE-1
MIL-STD-202GNOTICE 118 July 2003DEPARTMENT OF DEFENSETEST METHOD STANDARDELECTRONIC AND ELECTRICAL COMPONENT PARTSTO ALL HOLDERS OF MIL-STD-202G:1. THE FOLLOWING PAGES OF MIL-STD-202G HAVE BEEN REVISED AND SUPERSEDE THE PAGES LISTED:METHOD NEW PAGE DATE SUPERSEDED PAGE DATE7 18 July 2003 7 8 February 2002106G 1 8 February 2002 1 REPRINTED WITHOUT CHANGE 106G 2 18 July 2003 2 8 February 2002107G 3 28 March 1984 3 REPRINTED WITHOUT CHANGE 107G 4 18 July 2003 4 28 March 1984112E 7 18 July 2003 7 11 October 1988112E 8 11 October 1988 8 REPRINTED WITHOUT CHANGE 2. THE FOLLOWING TEST METHODS OF MIL-STD-202G HAVE BEEN REVISED AND SUPERSEDE THE TESTMETHODS LISTED:NEW METHOD DATE SUPERSEDED METHOD DATE 303A 18 July 2003 303 6 February 1956305A 18 July 2003 305 24 October 19563. RETAIN THIS NOTICE PAGE AND INSERT BEFORE THE TABLE OF CONTENTS.4. Holders of MIL-STD-202G will verify that the changes indicated above have been entered. This notice page will be retained as a check sheet. This issuance, together with appended pages, is a separate publication. Each notice is to be retained by stocking points until the standard is completely revised or canceled.5. The margins of this notice are marked with asterisks to indicate where changes were made. This was done as a convenience only and the Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations and relationship to the last previous issue.Custodians: Preparing activity:Army - CR DLA - CCNavy - ECAir Force - 11 (Project 59GP-0186) Review activities:Army - AR, AT, AV, CR4, MI, SM, TENavy - AS, OS, SHAir Force - 19, 99NSA - NSAMSC N/A FSC 59GP DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.NOTICE 118 July 2003NUMERICAL INDEX OF TEST METHODS Test MethodNumberDate TitleEnvironmental tests (100 class)101E 102A 103B 104A 105C 106G 107G 108A 109C 110A 111A 112E 8 February 2002Cancelled12 September 196324 October 195612 September 19638 February 200228 March 198412 September 19638 February 200216 April 197316 April 197311 October 1988Salt atmosphere (corrosion) (formerly called salt spray)Superseded by Method 107 (see note on Method 102)Humidity (steady state)ImmersionBarometric pressure (reduced)Moisture resistanceThermal shockLife (at elevated ambient temperature)ExplosionSand and dustFlammability (external flame)SealPhysical characteristics tests (200 class)201A 202D 203C 204D 205E 206 207B 208H 209 210F 211A 212A 213B 214A 215K 216 217A 24 October 1956Cancelled8 February 20021 April 1980Cancelled12 September 19638 February 200231 January 199618 May 19628 February 200214 April 196916 April 197316 April 197328 March 19848 February 2002Cancelled8 February 2002VibrationSuperseded by Method 213 (see note on Method 202)Random dropVibration, high frequencySuperseded by Method 213 (see note on Method 205)Life (rotational)High-impact shockSolderabilityRadiographic inspectionResistance to soldering heatTerminal strengthAccelerationShock (specified pulse)Random vibrationResistance to solventsSuperseded by Method 210 (see note on Method 216)Particle impact noise detection (PIND)Electrical characteristics tests (300 class)301302 * 303A304 * 305A306307308309310311312 6 February 19566 February 195618 July 200324 October 195618 July 200324 October 195624 October 195629 November 196127 May 196520 January 196714 April 196916 April 1973Dielectric withstanding voltageInsulation resistanceDC resistanceResistance temperature characteristicCapacitanceQuality factor (Q)Contact resistanceCurrent-noise test for fixed resistorsVoltage coefficient of resistance determination procedureContact-chatter monitoringLife, low level switchingIntermediate current switching7NOTICE 118 July 2003METHOD 106GMOISTURE RESISTANCE1. PURPOSE. The moisture resistance test is performed for the purpose of evaluating, in an accelerated manner, the resistance of component parts and constituent materials to the deteriorative effects of the high-humidity and heat conditions typical of tropical environments. Most tropical degradation results directly or indirectly from absorption of moisture vapor and films by vulnerable insulating materials, and from surface wetting of metals and insulation. These phenomena produce many types of deterioration, including corrosion of metals, physical distortion and decomposition of organic materials, leaching out and spending of constituents of materials; and detrimental changes in electrical properties. This test differs from the steady-state humidity test (method 103 of this standard) and derives its added effectiveness in its employment of temperature cycling, which provides alternate periods of condensation and drying essential to the development of the corrosion processes and, in addition, produces a "breathing" action of moisture into partially sealed containers. Increased effectiveness is also obtained by use of a higher temperature, which intensifies the effects of humidity. The test includes low temperature and vibration subcycles (when applicable, see 3.4.2) that act as accelerants to reveal otherwise indiscernible evidence of deterioration since stresses caused by freezing moisture and accentuated by vibration tend to widen cracks and fissures. As a result, the deterioration can be detected by the measurement of electrical characteristics (including such tests as dielectric withstanding voltage and insulation resistance) or by performance of a test for sealing. Provision is made for the application of a polarizing voltage across insulation to investigate the possibility of electrolysis, which can promote eventual dielectric breakdown. This test also provides for electrical loading of certain components, if desired, in order to determine the resistance of current-carrying components, especially fine wires and contacts, to electro-chemical corrosion. Results obtained with this test are reproducible and have been confirmed by investigations of field failures. This test has proven reliable for indicating those parts which are unsuited for tropical field use.2. APPARATUS.2.1 Chamber. A test chamber shall be used which can meet the temperature and humidity cycling specified on figure 106-1. The material used to fabricate the platforms and standoffs, which support the specimens, shall be non-reactive in high humidity. Wood or plywood shall not be used because they are resiniferous. Materials shall not be used if they contain formaldehyde or phenol in their composition. Provisions shall be made to prevent condensate from the chamber ceiling dripping onto the test specimens.2.1.1 Opening of the chamber door. During the periods when the humidity is ascending or descending, the chamber door should not be opened. If the chamber door must be opened, it should be opened during the 16th hour through the 24th hour of an individual cycle. While the chamber is at 25°C (77°F), and the relative humidity tolerance must be maintained, the chamber door should be opened only for a short period of time.2.1.2 Water. Steam, or distilled and demineralized, or deionized water, having a pH value between 6.0 and 7.2 at 23°C (73.4°F) shall be used to obtain the specified humidity. No rust or corrosive contaminants shall be imposed on the test specimens by the test facility.3. PROCEDURE.3.1 Mounting. Specimens shall be mounted by their normal mounting means, in their normal mounting position, but shall be positioned so that they do not contact each other, and so that each specimen receives essentially the same degree of humidity.3.2 Initial measurements. Prior to step 1 of the first cycle, the specified initial measurements shall be made at room ambient conditions, or as specified.REPRINTED WITHOUT CHANGE METHOD 106G8 February 20021 of 4NOTICE 1NOTES:1. Allowance of 100 percent RH is intended to avoid problems in reading values close to 100 percent RH, butactual chamber operation shall be such so as to avoid condensation.2. Unless otherwise specified, the steady state temperature tolerance is ±2°C at all points within the immediatevicinity of the specimens and the chamber surfaces.3. Rate of change of temperature is unspecified; however, specimens shall not be subjected to radiant heat fromchamber-conditioning processes.4. Circulation of air in the chamber shall be at a minimum cubic rate per minute equivalent to 5 times the volumeof the chamber.FIGURE 106-1. Graphical representation of moisture-resistance test.Supersedes page 2 of MIL-STD-202GMETHOD 106G8 February 20022NOTICE 1 18 July 2003TABLE 107-II. Exposure time in air at temperature extremes.Weight of specimenMinimum time (for steps 1 and 3)1 ounce (28 grams and below)Above 1 ounce (28 grams) to .3 pound (136 grams), inclusiveAbove .3 pounds (136 grams) to 3 pounds (1.36 kilograms), inclusiveAbove 3 pounds (1.36 kilograms) to 30 pounds (13.6 kilograms), inclusive Above 30 pounds (13.6 kilograms) to 300 pounds (136 kilograms), inclusive Above 300 pounds (136 kilograms)Hours1/4 (or as specified)½ 1 2 4 8TABLE 107-III. Thermal shock conditions (liquid).Test condition Number of cycles Test condition Number of cycles Test condition Numberof cyclesTest condition Numberof cycles Step AA 5 BB 5 CC 5 DD 5 AA-1 15 BB-1 15 CC-1 15 DD-1 15 AA-2 25 BB-2 25 CC-2 25 DD-2 25 Temperature Time Temperature Time Temperature TimeTemperature Time1 2 °C -0 +2, -10 100 +10, -2 See table 107-V See table 107-V °C -65 +0, -10 125 +10, -0 See table 107-V See table 107-V °C-65 +0, -10150 +10, -0See table107-V See table 107-V°C-65 +0, -10200 +10, -0See table107-V See table 107-VREPRINTED WITHOUT CHANGE METHOD 107G28 March 19843NOTICE 118 July 2003TABLE 107-IV. Suggested thermal fluids. 1/ 2/1/ See 2.2.2/ Ethylene glycol shall not be used as a thermal shock test fluid.3/ Tap water is indicated as an acceptable fluid for this temperature range. Its suitability chemically shall be established prior to use. A mixture of water and alcohol may be used to prevent freezing at the low temperature extreme. The water shall not be allowed to boil at the upper temperature extreme.4/ FC77, FC70, FC40 are the registered trademark of 3M.5/ UCON-WS process fluid is the registered trademark of Union Carbide Corporation.6/ D02, D02-TS, D03, D05, D/80, LS/215 and LS/230 are the registered trademark of Ausimont (Division of Montedison).TABLE 107-V. Exposure time in liquid at temperature extremes.Weight of specimen Minimum time(for steps 1 and 2).05 ounce (1.4 grams) and belowAbove .05 ounce (1.4 grams) to .5 ounce (14 grams) Above .5 ounce (14 grams) to 5 ounces (140 grams) Minutes½25Supersedes page 4 of MIL-STD-202GMETHOD 107G28 March 19844 *NOTICE 1 18 July 20035.4.3.2.1 Procedure IIIa. The device(s) shall be tested using the appropriate conditions specified in table I for the internal cavity volume of the package under test. The time (t) is the time under pressure and time (t z ) is themaximum time allowed after release of pressure before the device(s) shall be read. This method shall not be used if the maximum equivalent standard leak rate limit given in the procurement document is less than the limits specified herein for procedure IIIc. Upon completion of this procedure, the specimen shall be checked for gross leaks by subjecting the specimen either to test condition A, B, or D. Water, at room ambient temperature and a pressure of 2.5 inches (63.5 mm) of mercury, may be used in place of silicone oil, if test condition B is used to verify gross leaks.TABLE I. Fixed conditions procedure IIIa.Bomb condition Volume ofpackage (cm 3)1bf/in 2gage Exposure timehours Maximum dwell hoursR1 Reject limit(atm cm 3/s He)V < 0.40 60 ±2 2 +0.2, -0 1 5 x 10-8V > 0.4060 ±2 2 +0.2, -0 1 2 x 10-7 V > 0.4030 ±24 +0.4, -011 x 10-75.4.3.2.2 Procedure IIIb.5.4.3.2.2.1 Activation parameters. The activation pressure and soak time shall be determined in accordance with the following equation:tP skT Rs Q =The parameters of equation (1) are defined as follows:Q S = The maximum calculated leak rate allowable, in atm cm 3/sKr, for the devices to be tested.R = Counts per minute above the ambient background after activation if the device leak rate were exactlyequal to Q S . This is the reject count above the background of both the counting equipment and the component, if it has been through prior radioactive leak tests.s = The specific activity, in microcuries per atmospheric cubic centimeter, of the krypton 85 tracer gas inthe activation system.k = The overall counting efficiency of the scintillation crystal in counts per minute per microcurie of krypton85 in the internal void of the specific component being evaluated. This factor depends uponcomponent configuration and dimensions of the scintillation crystal. The counting efficiency shall be determined in accordance with 5.4.3.2.2.2.T = Soak time, in hours, that the devices are to be activated. _P = P e 2 - P i 2, where P e is the activation pressure in atmospheres absolute and P i is the original internalpressure of the devices in atmospheres absolute. The activation pressure (P e ) may be established by specification or if a convenient soak time (T) has been established, the activation pressure (P e ) can be adjusted to satisfy equation (1).t = Conversion of hours to seconds and is equal to 3,600 seconds per hour.Supersedes page 7 of MIL-STD-202G METHOD 112E 11 October 19887*NOTICE 1 18 July 20035.4.3.2.2.2 Determination of counting efficiency (k). The counting efficiency (k) of equation in 5.4.3.2.2.1 shall bedetermined as follows:a. Five representative units of the device type being tested shall be tubulated and the internal void of thedevice shall be backfilled through the tubulation with a known volume and known specific activity of krypton 85 tracer gas and the tubulation shall be sealed off.b. The counts per minute shall be directly read in the shielded scintillation crystal of the counting station inwhich the devices are read. From this value, the counting efficiency, in counts per minute per microcurie, shall be calculated.5.4.3.2.2.3 Evaluation of surface sorption. All device encapsulations consisting of glass, metal, and ceramic or combinations thereof, including coatings and external sealants, shall be evaluated for surface sorption of krypton 85 before establishing the leak test parameters. Representative samples of the questionable material shall besubjected to the predetermined pressure and time conditions established for the device configuration as specified by 5.4.3.2.2.1. The samples shall then be counted every 10 minutes, with count rate noted, until the count ratebecomes asymptotic with time. (This is the point in time at which surface sorption is no longer a problem.) This time lapse shall be noted and shall determine the "wait time" specified in 5.4.3.2.2.4.5.4.3.2.2.4 Specific procedure IIIb. The devices shall be placed in radioactive tracer gas activation tank. The activation chamber may be partially filled with inert material to reduce pumpdown time. The tank shall be evacuated to 0.5 torr. The devices shall be subjected to a minimum of 2 atmospheres absolute pressure of krypton 85/dry nitrogen mixture for the time necessary to satisfy the equation. Actual pressure and soak time shall be determined in accordance with 5.4.3.2.2.1. The R value in counts per minute shall be not less than 600 above ambientbackground. The krypton 85/dry nitrogen gas mixture shall be evacuated to storage until 0.5 torr vacuum exists in the activation tank. This evacuation shall be completed within 3 minutes maximum. The activation tank shall then be backfilled with air (air wash). The devices shall then be removed from the activation tank and leak tested within 1 hour after gas exposure with a scintillation-crystal-equipped counting station. Device encapsulations that come under the requirements of 5.4.3.2.2.3 shall be exposed to ambient air for a time not less than the "wait time"determined by 5.4.3.2.2.3. In no case will the time between removal from the activation chamber and test exceed 1 hour. This exposure shall be performed after gas exposure but before determining leak rate with the countingstation. Device encapsulations that do not come under the requirements of 5.4.3.2.2.3 may be tested without a "wait time". (The number of devices removed from pressurization for leak testing shall be limited such that the test of the last device can be completed within 1 hour.) The actual leak rate of the component shall be calculated with the following equation:RQ X MINUTE PER COUNTS NET IN READOUT ACTUAL Q S)(=Where Q = Actual leak rate in atm cm 3/s, and Q S and R are defined in 5.4.3.2.2.1.Unless otherwise specified, devices that exhibit a leak rate equal to or greater than 1 x 10-8atmospheric cubic centimeters of krypton 85 per second shall be considered a failure.Upon completion of this procedure, the specimen shall be checked for gross leaks by subjecting the specimen either to test condition A, B, or D. Water, at room ambient temperature and a pressure of 2.5 inches (63.5 mm) of mercury, may be used in place of silicone oil, if test condition B is used to verify gross leaks.5.4.3.2.2.5 Personnel precautions. A Nuclear Regulatory Commission (NRC) license is necessary for possession and use of the krypton 85 leak-test equipment. In the use of gas, code of Federal regulations Nuclear Regulatory Commission Rules and Regulations, Title 10, Chapters 1, 20, 30, 31, and 32 should be followed and the maximum permissible tolerance levels prescribed by the National Committee on Radiological Protection should be observed.REPRINTED WITHOUT CHANGEMETHOD 112E 11 October 19888NOTICE 1 18 July 2003METHOD 303ADC RESISTANCE1. PURPOSE. The purpose of this test is to measure the direct-current (dc) resistance of resistors,electromagnetic windings of components, and conductors. It is not intended that this test apply to the measurement of contact resistance.1.1. Precautions. The temperature at which the dc resistance measurement is made will affect the final value of resistance. In addition, resistance values may vary with the measuring voltage.2. PROCEDURE. DC resistance shall be measured with a resistance bridge or other suitable test equipment. The limit of error in the bridge or other test equipment shall not exceed one-tenth of the specified tolerance on the measured resistance (for example, the limit of error in the bridge or other test equipment shall not exceed ± 0.5percent if the specified tolerance on the measured resistance is ± 5 percent), unless otherwise specified. For inplant quality conformance testing, the accuracy of the measurement shall be such to insure that the resistance value is within the required tolerance. If a plus or minus tolerance is not specified, the limit of error in the bridge or other test equipment shall not exceed ± 2 percent. The test current through the specimen shall be as small as practical considering the sensitivity of the indicating instruments, unless the test current or voltage is specified. When it is important that the temperature of the specimen shall not rise appreciably during the measurement, the test voltage shall be applied uninterruptedly for as short a time as practicable, but in no case for more than 5 seconds, unless otherwise specified. Unless otherwise specified, the measurement shall be made at a temperature of 25°C ± 5°C. In the case of measurement dispute, dc resistance measurements shall be made at or corrected to 25°C .3. SUMMARY. The following details are to be specified in the individual specification:a. Limit of error of measuring apparatus, if other than one-tenth of specified tolerance (see 2).b. Test voltage or current, if applicable (see 2).c. Maximum period of uninterrupted test-voltage application, if other than 5 seconds (see 2).d. Test temperature, if other than that specified (see 2).METHOD 303A 18 July 20031**NOTICE 1 18 July 2003METHOD 305ACAPACITANCE1. PURPOSE. The purpose of this test is to measure the capacitance of component parts. Preferred test frequencies for this measurement are 60 Hz, 100 Hz, 120 Hz, 1 kHz, 100 kHz, and 1 MHz.2. PROCEDURE. The capacitance of the specimen shall be measured with a capacitance bridge or other suitable method at the frequency specified. Unless otherwise specified, the measurement shall be made at a temperature of 25°C ± 5°C. In the case of measurement dispute, capacitance measurements shall be made at or corrected to 25°C. The inherent accuracy of the measurement shall be ±(0.5 percent +0.2 picofarad) unless otherwise specified. Suitable measurement technique shall be used to minimize errors due to the connections between the measuring apparatus and the specimen. The alternating-current (ac) voltage actually impressed across the specimen shall be as low as practicable. When a direct-current (dc) polarizing voltage is required, it shall be as specified and shall exceed the peak ac voltage impressed across the specimen; however, the sum of the peak ac and the dc voltages shall not exceed the voltage rating of the specimen.SUMMARY. The following details are to be specified in the individual specification:a. Test frequency (see 2).b. Test temperature, if other than that specified (see 2).c. Limit of accuracy, if other than that specified (see 2).d. Magnitude of polarizing voltage, if applicable (see 2).e. Magnitude of AC rms test signal, if applicable (see 2).METHOD 305A 18 July 20031* **。
2003年AMC8试题
20031Jamie counted the number of edges of a cube,Jimmy counted the number of corners,and Judy counted the number of faces.They then added the three numbers.What was the resulting sum?(A)12(B)16(C)20(D)22(E)262Which of the following numbers has the smallest prime factor?(A)55(B)57(C)58(D)59(E)613A burger at Ricky C’s weighs120grams,of which30grams arefiller.What percent of the burger is notfiller?(A)60%(B)65%(C)70%(D)75%(E)90%4A group of children riding on bicycles and tricycles rode past Billy Bob’s house.Billy Bob counted7children and19wheels.How many tricycles were there?(A)2(B)4(C)5(D)6(E)75If20%of a number is12,what is30%of the same number?(A)15(B)18(C)20(D)24(E)306Given the areas of the three squares in thefigure,what is the area of the interior triangle?16925144(A)13(B)30(C)60(D)300(E)1800Thisfile was downloaded from the AoPS Math Olympiad Resources Page Page120037Blake and Jenny each took four100point tests.Blake averaged78on the four tests.Jenny scored10points higher than Blake on thefirst test,10points lower on the second test,and 20points higher on both the third and fourth test.What is the difference between Blake’s average on the four tests and Jenny’s average on the four tests?(A)10(B)15(C)20(D)25(E)408Bake Sale Four friends,Art,Roger,Paul and Trisha,bake cookies,and all cookies have the same thickness.The shapes of the cookies differ,as shown.◦Art’s cookies are trapezoids:3in3in◦Roger’s cookies are rectangles:2in4in◦Paul’s cookies are parallelograms:2in3in◦Trisha’s cookies are triangles:20034inEach friend uses the same amount of dough,and Art makes exactly12cookies.Who gets the fewest cookies from one batch of cookie dough?(A)Art(B)Roger(C)Paul(D)Trisha(E)There is a tie for fewest.9Bake Sale Four friends,Art,Roger,Paul and Trisha,bake cookies,and all cookies have the same thickness.The shapes of the cookies differ,as shown.◦Art’s cookies are trapezoids:3in3in◦Roger’s cookies are rectangles:2in4in◦Paul’s cookies are parallelograms:2in3in2003◦Trisha’s cookies are triangles:4in3inEach friend uses the same amount of dough,and Art makes exactly12cookies.Art’s cookies sell for60cents each.To earn the same amount from a single batch,how much should one of Roger’s cookies cost in cents?(A)18(B)25(C)40(D)75(E)9010Bake Sale Four friends,Art,Roger,Paul and Trisha,bake cookies,and all cookies have the same thickness.The shapes of the cookies differ,as shown.◦Art’s cookies are trapezoids:3in3in◦Roger’s cookies are rectangles:2in4in◦Paul’s cookies are parallelograms:20032in3in◦Trisha’s cookies are triangles:4in3inEach friend uses the same amount of dough,and Art makes exactly12cookies.How many cookies will be in one batch of Trisha’s cookies?(A)10(B)12(C)16(D)18(E)2411Business is a little slow at Lou’s Fine Shoes,so Lou decides to have a sale.On Friday,Lou increases all of Thursday’s prices by10percent.Over the weekend,Lou advertises the sale:”Ten percent offthe listed price.Sale starts Monday.”How much does a pair of shoes cost on Monday that cost40dollars on Thursday?(A)36(B)39.60(C)40(D)40.40(E)4412When a fair six-sided dice is tossed on a table top,the bottom face cannot be seen.What is the probability that the product of the5faces than can be seen is divisible by6?(A)1/3(B)1/2(C)2/3(D)5/6(E)113Fourteen white cubes are put together to form thefigure on the right.The complete surface of thefigure,including the bottom,is painted red.Thefigure is then separated into individual cubes.How many of the individual cubes have exactly four red faces?2003(A)4(B)6(C)8(D)10(E)1214In this addition problem,each letter stands for a different digit.T W O+T W OF O U RIf T=7and the letter O represents an even number,what is the only possible value for W?(A)0(B)1(C)2(D)3(E)415Afigure is constructed from unit cubes.Each cube shares at least one face with another cube.What is the minimum number of cubes needed to build afigure with the front and side views shown?FRONT SIDE(A)3(B)4(C)5(D)6(E)716Ali,Bonnie,Carlo,and Dianna are going to drive together to a nearby theme park.The car they are using has4seats:1Driver seat,1front passenger seat,and2back passenger seat.Bonnie and Carlo are the only ones who know how to drive the car.How many possible seating arrangements are there?(A)2(B)4(C)6(D)12(E)24200317The six children listed below are from two families of three siblings each.Each child has blue or brown eyes and black or blond hair.Children from the same family have at least one ofthese characteristics in common.Which two children are Jim’s siblings?Child Eye Color Hair ColorBenjamin Blue BlackJim Brown BlondeNadeen Brown BlackAustin Blue BlondeTevyn Blue BlackSue Blue Blonde(A)Nadeen and Austin(B)Benjamin and Sue(C)Benjamin and Austin(D)Nadeen and Tev 18Each of the twenty dots on the graph below represents one of Sarah’s classmates.Classmates who are friends are connected with a line segment.For her birthday party,Sarah is invitingonly the following:all of her friends and all of those classmates who are friends with at leastone of her friends.How many classmates will not be invited to Sarah’s party?(A)1(B)4(C)5(D)6(E)719How many integers between1000and2000have all three of the numbers15,20,and25as factors?(A)1(B)2(C)3(D)4(E)520What is the measure of the acute angle formed by the hands of the clock at4:20PM?(A)0(B)5(C)8(D)10(E)12200321The area of trapezoid ABCD is 164cm 2.The altitude is 8cm,AB is 10cm,and CD is 17cm.What is BC ,in centimeters?ADBC 10817(A)9(B)10(C)12(D)15(E)2022The following figures are composed of squares and circles.Which figure has a shaded regionwith largestarea?(A)A only (B)B only (C)C only (D)both A and B (E)all are equal 23In the pattern below,the cat (denoted as a large circle in the figures below)moves clock-wise through the four squares and the mouse (denoted as a dot in the figures below)moves counterclockwise through the eight exterior segments of the four squares.123452003If the pattern is continued,where would the cat and mouse be after the247th move?(A)(B)(C)(D)(E)200324A ship travels from point A to point B along a semicircular path,centered at Island X.Thenit travels along a straight path from B to C.Which of these graphs best shows the ship’s distance from Island X as it moves along its course?X CBA (A)distance traveledd i s t a n ce t o X (B)2003distance traveledd i s t a n ce t o X (C)distance traveledd i s t a n ce t o X (D)distance traveledd i s t a n ce t o X (E)distance traveledd i s t a n ce t o X200325In thefigure,the area of square WXYZ is25cm2.The four smaller squares have sides1cm long, either parallel to or coinciding with the sides of the large square.In∆ABC,AB=AC,and when∆ABC is folded over side BC,point A coincides with O,the center of square WXYZ.What is the area of∆ABC,in square centimeters?A OBCW XYZ(A)154(B)214(C)274(D)212(E)272The problems on this page are copyrighted by the Mathematical Association of America’s American Mathematics Competitions.。
2000年AMC8试题
20001Aunt Anna is 42years old.Caitlin is 5years younger than Brianna,and Brianna is half as old as Aunt Anna.How old is Caitlin?(A)15(B)16(C)17(D)21(E)372Which of these numbers is less than its reciprocal?(A)−2(B)−1(C)0(D)1(E)23How many whole numbers lie in the interval between 53and 2π?(A)2(B)3(C)4(D)5(E)infinitely many 4In 1960only 5%of the working adults in Carlin City worked at home.By 1970the ”at-home”work force increased to 8%.In 1980there were approximately 15%working at home,and in 1990there were 30%.The graph that best illustrates this is1960197019801990102030%1960197019801990102030%1960197019801990102030%1960197019801990102030%1960197019801990102030%(A)(B)(C)(D)(E)5Each principal of Lincoln High School serves exactly one 3-year term.What is the maximum number of principals this school could have during an 8-year period?(A)2(B)3(C)4(D)5(E)86Figure ABCD is a square.Inside this square three smaller squares are drawn with the side lengths as labeled.The area of the shaded L-shaped region is This file was downloaded from the AoPS Math Olympiad Resources PagePage 12000AB C D (A)7(B)10(C)12.5(D)14(E)157What is the minimum possible product of three different numbers of the set {−8,−6,−4,0,3,5,7}?(A)−336(B)−280(C)−210(D)−192(E)08Three dice with faces numbered 1through 6are stacked as shown.Seven of the eighteen faces are visible,leaving eleven faces hidden (back,bottom,between).The total number of dots NOT visible in this viewis(A)21(B)22(C)31(D)41(E)5320009Three-digit powers of2and5are used in this”cross-number”puzzle.What is the only possible digit for the outlined square?ACROSS DOWN2.2m1.5n12(A)0(B)2(C)4(D)6(E)810Ara and Shea were once the same height.Since then Shea has grown20%while Ara has grow half as many inches as Shea.Shea is now60inches tall.How tall,in inches,is Ara now?(A)48(B)51(C)52(D)54(E)5511The number64has the property that it is divisible by its units digit.How many whole numbers between10and50have this property?(A)15(B)16(C)17(D)18(E)2012A block wall100feet long and7feet high will be constructed using blocks that are1foot high and either2feet long or1foot long(no blocks may be cut).The vertical joins in the blocks must be staggered as shown,and the wall must be even on the ends.What is the smallest number of blocks needed to build this wall?2000(A)344(B)347(C)350(D)353(E)35613In triangle CAT ,we have ∠ACT =∠AT C and ∠CAT =36◦.If T R bisects ∠AT C ,then∠CRT =ATC R(A)36◦(B)54◦(C)72◦(D)90◦(E)108◦14What is the units digit of 1919+9999?(A)0(B)1(C)2(D)8(E)915Triangles ABC ,ADE ,and EF G are all equilateral.Points D and G are midpoints of AC and AE ,respectively.If AB =4,what is the perimeter of figure ABCDEF G ?A B CDE FG(A)12(B)13(C)15(D)18(E)21200016In order for Mateen to walk a kilometer(1000m)in his rectangular backyard,he must walk the length25times or walk its perimeter10times.What is the area of Mateen’s backyard in square meters?(A)40(B)200(C)400(D)500(E)100017The operation⊗is defined for all nonzero numbers by a⊗b=a2b.Determine[(1⊗2)⊗3]−[1⊗(2⊗3)].(A)−23(B)−14(C)0(D)14(E)2318Consider these two geoboard quadrilaterals.Which of the following statements is true?III(A)The area of quadrilateral I is more than the area of quadrilateral II.(B)The area of quadrilateral I is less than the area of quadrilateral II.(C)The quadrilaterals have the same area and the same perimeter.(D)The quadrilaterals have the same area,but the perimeter of I is more than the perimeter of II.(E)The quadrilaterals have the same area,but the perimeter of I is less than the perimeter of II. 19Three circular arcs of radius5units bound the region shown.Arcs AB and AD are quarter-circles,and arc BCD is a semicircle.What is the area,in square units,of the region?2000AB CD(A)25(B)10+5π(C)50(D)50+5π(E)25π20You have nine coins:a collection of pennies,nickels,dimes,and quarters having a total valueof $1.02,with at least one coin of each type.How many dimes must you have?(A)1(B)2(C)3(D)4(E)521Keiko tosses one penny and Ephraim tosses two pennies.The probability that Ephraim getsthe same number of heads that Keiko gets is(A)14(B)38(C)12(D)23(E)3422A cube has edge length 2.Suppose that we glue a cube of edge length 1on top of the bigcube so that one of its faces rests entirely on the top face of the larger cube.The percent increase in the surface area (sides,top,and bottom)from the original cube to the new solid formed is closestto2000(A)10(B)15(C)17(D)21(E)2523There is a list of seven numbers.The average of the first four numbers is 5,and the averageof the last four numbers is 8.If the average of all seven numbers is 647,then the number common to both sets of four numbers is(A)537(B)6(C)647(D)7(E)73724If ∠A =20◦and ∠AF G =∠AGF ,then ∠B +∠D =ABCDE FG (A)48◦(B)60◦(C)72◦(D)80◦(E)90◦25The area of rectangle ABCD is 72.If point A and the midpoints of BC and CD are joinedto form a triangle,the area of that triangleisA BC D2000(A)21(B)27(C)30(D)36(E)40The problems on this page are copyrighted by the Mathematical Association of America’s American Mathematics Competitions.。
MIL-PRF-23377H
PERFORMANCE SPECIFICATIONPRIMER COATINGS: EPOXY, HIGH-SOLIDSThis specification is approved for use by all Departments and Agencies of the Department of Defense.1. SCOPE 1.1 Scope. This specification covers the requirements for corrosion inhibiting, chemical and solvent resistant, solvent-borne, epoxy primer coatings that have a maximum volatileorganic compound (VOC) content of 340 grams per liter (g/L)(2.8 pounds per gallon [lb/gal]).1.2 Classification. The primer coatings will be of the following types and classes, asspecified (see 6.2):1.2.1 Types. The types of primer coatings are as follows:Type I-Standard pigments Type II -Low infrared reflective pigments 1.2.2 Classes. The classes of primer coatings are as follows:Class C-Strontium chromate based corrosion inhibitors Class N -Non-chromate based corrosion inhibitorsAMSC N/A FSC 8010DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited.NOT MEASUREMENT SENSITIVEMIL-PRF-23377H30 April 2002SUPERSEDINGMIL-PRF-23377G30 September 1999Beneficial comments (recommendations, additions, deletions) and any pertinent data which may be of use in improving this document should be addressed to: Commander, Naval Air Warfare Center Aircraft Division, Code 414100B120-3, Highway 547, Lakehurst, NJ08733-5100, by using the Standardization Document Improvement Proposal (DD Form 1426) appearing at the end of this document or by letter.2. APPLICABLE DOCUMENTS2.1 General. The documents listed in this section are specified in sections 3 and 4 ofthis specification. This section does not include documents cited in other sections of this specification or recommended for additional information or as examples. While every effort has been made to ensure the completeness of this list, document users are cautioned that they must meet all specified requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed.2.2 Government documents.2.2.1 Specifications and standards. The following specifications and standards form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those listed in the issue of the Department of Defense Index of Specifications and Standards (DoDISS) and supplement thereto, cited in the solicitation (see 6.2).SPECIFICATIONSDEPARTMENT OF DEFENSEMIL-C-5541-Chemical Conversion Coatings on Aluminum and AluminumAlloysMIL-C-8514-Coating Compound, Metal Pretreatment, Resin-AcidMIL-A-8625-Anodic Coatings, for Aluminum and Aluminum AlloysMIL-PRF-23699-Lubricating Oil, Aircraft Turbine Engine, Synthetic Base,NATO Code Number 0-156MIL-T-81772-Thinner, Aircraft CoatingMIL-PRF-83282-Hydraulic Fluid, Fire Resistant, Synthetic Hydrocarbon Base,Metric, NATO Code Number H-537MIL-PRF-85285-Coating: Polyurethane, High-SolidsSTANDARDSFEDERALFED-STD-141-Paint, Varnish, Lacquer and Related Materials: Methods ofInspection, Sampling and TestingFED-STD-595-Colors Used in Government Procurement(Unless otherwise indicated, copies of the above specifications and standards are available from the Standardization Document Order Desk, 700 Robbins Avenue, Building 4D, Philadelphia, PA 19111-5094.)22.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of the documents which are DoD adopted are those listed in the issue of the DoDISS cited in the solicitation. Unless otherwise specified, the issues of documents not listed in the DoDISS are the issues of the documents cited in the solicitation (see 6.2).AMERICAN SOCIETY FOR TESTING AND MATERIALS (ASTM)ASTM-B117-Salt Spray (Fog) Apparatus, Operating. (DoD adopted)ASTM-D1200 -Cup, Viscosity by Ford Viscosity. (DoD adopted)ASTM-D1210-Fineness Of Dispersion Of Pigment-Vehicle Systems By Hegman-TypeGage. (DoD adopted)ASTM-D1296-Solvents and Diluents, Volatile, Odor of. (DoD adopted)ASTM-D1640-Organic Coating, Drying, Curing, or Film Formation of at RoomTemperature. (DoD adopted)ASTM-D1649-Strontium Chromate PigmentASTM-D1849-Paint, Package Stability of. (DoD adopted)ASTM-D2803-Metal, Organic Coatings on, Filiform Corrosion Resistance of. (DoDadopted)ASTM-D3335-Lead, Cadmium, and Cobalt in Paint by Atomic AbsorptionSpectroscopy, Test for Low Concentrations of. (DoD adopted) ASTM-D3718-Paint, Chromium in, by Atomic Absorption Spectroscopy, LowConcentrations of. (DoD adopted)ASTM-D3742-1,1,1-Trichloroethane ContentASTM-D3924- Paint, Varnish, Lacquer, and Related Materials, Conditioning andTesting, Standard Environment for. (DoD adopted)ASTM-D3960-Paints and Related Coatings, Determining Volatile Organic Compound(VOC) Content of. (DoD adopted)(Application for copies should be addressed to the American Society for Testing and Materials, 100 Barr Harbor Drive, West Conshohocken, PA 19428-2959.)AMERICAN SOCIETY FOR QUALITY CONTROL (ASQC)ASQC-Z1.4-Procedures, Sampling and Tables for Inspection by Attributes.(DoD adopted)(Application for copies should be addressed to the American Society for Quality Control, P.O. Box 3005, 611 East Wisconsin Avenue, Milwaukee, WI 53201-4606.)3SOCIETY OF AUTOMOTIVE ENGINEERS (SAE)SAE-AMS1640- Compound, Corrosion Removing for Aircraft SurfacesSAE-AMS-QQ-A-250/4- Aluminum Alloy 2024, Plate and Sheet. (DoD adopted)SAE-AMS-QQ-A-250/5- Aluminum Alloy Alclad 2024, Plate and Sheet. (DoDadopted)(Application for copies should be addressed to the Society of Automotive Engineers,400 Commonwealth Drive, Warrendale, PA 15096-0001.)2.4 Order of precedence. In the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.3. REQUIREMENTS3.1 Qualification. The primer coating furnished under this specification shall be a product that is authorized by the qualifying activity for listing on the applicable qualified products list before contract award (see4.2 and 6.3).3.2 Material. Materials used in the manufacture of the primer coating supplied under this specification shall be of such a quality as to produce products conforming to the requirements of this specification.3.3 Toxicity. The primer coating supplied under this specification shall have no adverse effect on the health of personnel (see 6.9), when used for its intended purpose and with the precautions listed in 3.11.3.4 Composition. The primer coating shall consist of two components, as follows:Component A - a base component composed of epoxy resin and solventsComponent B - a curing agent containing polyamide or amine resin and solvents Component B shall act as the curing agent for component A. The components shall be packaged separately and furnished as a kit (see 6.7.1). When the components are mixed in the proportions specified by the manufacturer, a primer coating meeting the requirements of this specification shall result. Chlorinated solvents, except for para-chlorotrifluoromethylbenzene or equal, shall be prohibited in the formulation of this primer coating. Incidental cadmium and cadmium compounds shall be not greater than one part per million (ppm). The non-volatile portion shall contain not more than 0.06 percent by weight of lead metal or lead compounds.43.4.1 Pigment.3.4.1.1 Class C. Coatings containing strontium chromate conforming to ASTM-D1649 as the corrosion inhibitor, along with extenders and other pigments, shall be identified as class C.3.4.1.2 Class N. Coatings containing non-chromium corrosion inhibitors, along with extenders and other pigments, shall be identified as class N. Incidental chromium content of class N shall be not greater than 5 ppm (see 4.5).3.4.2 Volatile organic compound (VOC) solvent content. The VOC content of admixed primer coatings shall be not greater than 340 g/L (2.8 lb/gal). The resistivity of the solvents shall permit application of the coating by electrostatic spray application (see 4.5).3.4.2.1 Thinner compatibility. The admixed primer coatings shall be compatible with thinner conforming to MIL-T-81772, type II (see 6.11).3.5 Physical properties – components before mixing.3.5.1 Fineness of grind. The fineness of grind of the pigmented component shall be 5 or greater on the Hegman scale (see4.5).3.5.2 Condition in container. Components A and B shall be free of grit, seeds, lumps, abnormal thickening or livering, and shall not show pigment flotation nor excessive settling. They shall mix to a smooth, homogeneous, and pourable condition. In addition, the containers shall exhibit no deformation (see4.5.1).3.5.3 Storage stability. The primer coating components, as packaged by the manufacturer, shall meet all requirements of this specification after storage for not less than one year (see4.5).3.5.4 Accelerated storage stability. The primer coating, as packaged by the manufacturer, shall meet all requirements of this specification after storage for 14 days (see4.5.2). The container shall not become deformed or the lid shall not become unsealed during the storage period.3.6 Physical properties - admixed components.3.6.1 Color.3.6.1.1 Type I. The color of the admixed type I primer coating shall be the natural color of the corrosion inhibiting pigments used, except that tinting to a darker shade is permitted.3.6.1.2Type II. The color of the admixed type II primer coating shall be dark green or gray.53.6.2 Odor. The odor of the admixed coating, wet or dry, shall be characteristic of the solvents used (see4.5).3.6.3 Viscosity. Immediately after mixing components A and B, the maximum viscosity of the unthinned, admixed primer coating shall be 40 seconds through a #4 Ford cup (see4.5).3.6.4 Pot life. After mixing and storage at room temperature in a closed container(see4.5) for 4 hours, the maximum viscosity of the unthinned primer coating from 3.6.3 shall be 70 seconds through a #4 Ford cup (see 4.5).3.7 Physical properties - film.3.7.1 Surface appearance. The admixed primer coating, applied to a vertical surface, shall not sag, run, or streak. The dried film shall have a smooth, uniform surface free of grit, seeds, craters, blisters, and other irregularities (see4.4.1). No orange peel (wavy appearance) shall be evident when viewed from at least six feet away.3.7.2 Drying time. The admixed primer coating shall be tack free within 5 hours and shall dry hard within 8 hours (see table II).3.7.3 Lifting. There shall be no evidence of lifting or any other film irregularity after topcoating the admixed primer coating that has air dried for 5 hours (see4.5.3).3.7.4 Adhesion. The primer coating shall not peel when tested in accordance with4.5.4.3.7.5 Flexibility. The primer coating shall exhibit an elongation of not less than 10 percent when tested in accordance with4.5.5.3.7.6 Infrared reflectance (type II primer coating only). The total reflectance (specular and diffuse) of the type II primer coating, relative to barium sulfate, shall be not greater than ten percent throughout the range of 700 to 2,600 nanometers (nm) (see4.5.6).3.8 Resistance properties.3.8.1 Water resistance. The topcoated primer coating shall withstand immersion in distilled water maintained at 49 ±3 °C (120 ±5 °F) for four days without exhibiting any evidence of wrinkling, blistering, or any other coating deficiency (see4.5.7).3.8.2 Corrosion resistance.3.8.2.1 Salt spray. The primer coating, with and without a topcoat, shall not exhibit6blistering, lifting of either coating, nor substrate pitting after exposure to a 5 percent salt spray for 2,000 hours. Class C primer shall exhibit no corrosion in the scribe (see 4.5.8.1).3.8.2.2 Filiform. The topcoated primer coating shall not exhibit filiform corrosion extending beyond 6.35 millimeters (mm) (0.25 inch) from the scribe, and the majority of the filaments shall be less than 3.175 mm (0.125 inch) in length (see4.5.8.2).3.8.3 Solvent resistance (cure). The primer coating shall withstand 50 passes (25 back and forth rubs) by a cloth rag soaked in methyl ethyl ketone (MEK). Rubbing through to bare substrate constitutes failure of the primer coating to properly cure (see4.5.9).3.8.4 Fluid resistance. The primer coating shall withstand immersion for 24 hours in each of synthetic lubricating oil conforming to MIL-PRF-23699 and synthetic hydraulic fluid conforming to MIL-PRF-83282. Four hours after removal from the respective fluid, the coating shall not exhibit any softening, blistering, loss of adhesion, nor any other coating deficiency. Discoloration of the coating is acceptable and shall not be cause for rejection (see4.5.10).3.9 Working properties.3.9.1 Mixing and dilution. The components of the primer coating, including thinner if required (see 6.11), shall homogeneously blend when mixed by a mechanical mixer in the volume mixing ratio specified by the manufacturer. Within one hour of mixing, the admixed coating shall not separate into visually distinct layers (see4.5.11.1).3.9.2 Application. The admixed primer coating shall be capable of being applied by conventional, airless, high volume, low pressure (HVLP), or electrostatic spray equipment. Application shall yield a uniform film with no runs or sags at a dry-film thickness of15 to 23 microns (µm) (0.6 to 0.9 mil) (see 4.5.11.2).3.10 Identification of material. Individual containers greater than one pint and cases of containers less than one pint shall be identified with the following information:MIL-PRF-23377H, “Primer Coatings: Epoxy, High Solids” type I or II, class C or N Component identification (as applicable):Component A - base component or Component B - curing agentManufacturer’s name and product numberDate of manufacture (month/year)Batch number/net contentsVOC content in grams/literMixing and thinning instructions73.10.1 Component containers. Component A and component B containers shall have the following warning:“WARNING! FLAMMABLE.”3.11 Precaution sheet. A printed precaution sheet with the following information shall be included with each kit:PRECAUTIONSa.The surface to be coated must be clean (free of oil, dust, etc.).b.Spray equipment must be adequately grounded. Clean equipment immediately after usewith thinner conforming to MIL-T-81772, type II.c.Mix only the amount of primer coating to be used within 4 hours.d.Always add component B to component A – NEVER THE REVERSE.e.Never mix coating or individual component from one vendor with that of another vendor.f.Apply over pretreated metal. On fiberglass-reinforced plastic, a prior coating of washprimer in accordance with MIL-C-8514will facilitate stripping without damage to thefiberglass.4. VERIFICATION4.1 Classification of inspections. The inspection requirements specified herein are classified as follows:a. Qualification inspection (see 4.2).b. Conformance inspection (see 4.3).4.2 Qualification inspection. Qualification inspection shall consist of all the inspections listed in this specification. The qualification inspection performed by the qualification laboratory (see 6.3) shall consist of a review for approval of the submitted manufacturer’s test report and subjecting the qualification test sample to examination and testing to determine conformance to all requirements in section 3. The qualification test sample shall consist of not less than one quart of each component of the primer coating. The samples shall be legibly identified (see 6.3.1.1).4.3 Conformance inspection.4.3.1 Primer coating inspection. The conformance inspection shall consist of all the tests specified in 4.5, with the exception of storage stability (see 3.5.3), accelerated storage stability (see 3.5.4), and corrosion resistance (see 3.8.2.1 and 3.8.2.2). There shall be no failures (see6.5). Samples for tests shall consist of one complete unopened kit selected at random from each batch. Containers shall only be opened when being tested.84.3.2 Visual inspection of filled containers. Samples shall be selected at random from each lot (see 6.6) in accordance with ASQC-Z1.4, inspection level S-2. The lot size for this inspection shall be the number of kits fully prepared for delivery. The selected samples shall be examined for container fill, proper location, and completion of item identification (see 3.10), warning statements (see 3.10.1), and the precaution sheet (see 3.11). There shall be no defects (see 6.5).4.4 Test panels. Test panels shall be prepared under laboratory conditions (see 4.5). Test panels shall be constructed of aluminum alloy. Alloy composition and pretreatments of test panels shall be in accordance with table I. Unless otherwise specified in the test method, the primer coating shall be applied in accordance with 4.4.1 and the topcoat, when required, shall be applied in accordance with 4.4.2.4.4.1 Application of primer coating. When required by the test method, the primer coating shall be prepared and applied as follows:a.Thoroughly mixing each component separately.b.Slowly pouring component B into component A while stirring the mixture to achievethe manufacturer's specified volume mixing ratio.c.Diluting the admixed primer coating, if necessary, with thinner conforming toMIL-T-81772, type II. If dilution of the primer coating is required, do not exceed340 g/L (2.8 lb/gal) (see 6.11).d.Allowing admixed coating to stand undisturbed for 30 minutes prior to use, unless themanufacturer’s directions state otherwise.e.Spraying the test panels with primer coating to a dry-film thickness of 15 to 23 µm (0.6to 0.9 mil).If a topcoat is not used, the primer coating shall be allowed to air dry for not less than 14 days, or air dry for not less than one hour followed by 24 hours at 65.5 ±3 °C (150 ±5 °F) prior to testing. If a topcoat is required, the primer coating shall be air-dried for 5 hours and then coated with a polyurethane coating conforming to MIL-PRF-85285 in accordance with 4.4.2.9TABLE I. Aluminum test panels.Panel Substrate PretreatmentA SAE-AMS-QQ-A-250/4 (T3 temper)MIL-C-5541, class 1A (conversion coating)B SAE-AMS-QQ-A-250/4 (0 temper)MIL-A-8625, type I or IC (anodize)C SAE-AMS-QQ-A-250/5 (T3 temper)Deoxidized 1/D SAE-AMS-QQ-A-250/5 (T3 temper)MIL-C-5541, class 1A (conversion coating)1/Immerse test panel for 2 minutes in corrosion removing compound conforming to SAE-AMS1640, then remove test panel and rinse with distilled water. Apply the primercoating within one hour.4.4.2 Application of topcoat. When a topcoat is required by the test method, mix polyurethane coating conforming to MIL-PRF-85285 (untinted gloss white conforming toFED-STD-595, color number 17925) adding thinner, if required, and allow it to stand 30 minutes prior to application. Apply the coating to a total dry-film thickness of 43 to 58 µm(1.7 to 2.3 mils). If applied in two coats, allow the first coat to air dry for 60 minutes prior to application of the second coat. After application of the topcoat to the required thickness and prior to testing, allow the coating to air dry for not less than 14 days or allow the coating to air dry for one hour followed by 24 hours at 65.5 ±3 °C (150 ±5 °F).4.5 Test methods. The tests of this specification shall be conducted in accordance with table II and 4.5.1 through 4.5.11. Unless otherwise specified in the test method or paragraph, laboratory test conditions shall be in accordance with ASTM-D3924. Room temperature conditions are 18 to 29.5 °C (65 to 85 °F) and a relative humidity of 50 ±10 percent.4.5.1 Condition in container. Each component in its unopened container shall stand without agitation for not less than 14 days at room temperature (see 4.5). After this period, the containers shall be examined for bulging or other deformation due to internal pressure. Each component container shall be opened and examined, then mixed by hand vigorously stirring with a paddle for not more than 5 minutes, and examined for conformance to 3.5.2.10TABLE II. Test methods.Test RequirementParagraphTestParagraphFED-STD-141Test MethodASTM TestMethodLead and cadmium content 3.4------ASTM-D3335 Chlorinated solvent content 3.4------ASTM-D3742 Chromium content (class N only) 3.4.1.2------ASTM-D3718 VOC solvent content 3.4.2---ASTM-D3960 Fineness of grind 3.5.1------ASTM-D1210 Condition in container 3.5.2 4.5.1---Storage stability 1/ 3.5.3---3022---Accelerated storage stability 2/ 3.5.4 4.5.2---ASTM-D1849 Odor 3.6.2------ASTM-D1296 Viscosity 3.6.3------ASTM-D1200 Pot life 3.6.4------ASTM-D1200 Surface appearance 3.7.1 4.4.1Drying time 3/ 3.7.2------ASTM-D1640 Lifting 3.7.3 4.5.3------Adhesion 3.7.4 4.5.4------Flexibility 3.7.5 4.5.5------Infrared reflectance (type II only) 3.7.6 4.5.6------Water resistance 3.8.1 4.5.7------Salt-spray corrosion resistance 3.8.2.1 4.5.8.1------Filiform corrosion resistance 3.8.2.2 4.5.8.2------Solvent resistance (cure) 3.8.3 4.5.9------Fluid resistance 3.8.4 4.5.10------Mixing and dilution 3.9.1 4.5.11.1------Application 3.9.2 4.5.11.2------1/The daily ambient air temperature at the storage location shall be within the range of 1.7 to46 °C (35 to 115 °F).2/The primer coating shall be mixed with a mechanical shaker for 10 minutes instead of 300 stirs in 2 minutes.3/ Use panels designated A in table I.114.5.2 Accelerated storage stability. Not less than one full, unopened, sealed container of each component shall be stored undisturbed for not less than 14 consecutive days in a location maintained at 60 ±3 °C (140 ±5 °F). At the end of 14 days, the container(s) shall be allowed to cool to room temperature (see 4.5). (During the storage period, it is advised that the unopened containers be placed in larger, vented containers to confine any splash that may occur if the lid of the unopened container is blown off by gassing.) If, upon removal, the unopened container is deformed, do not open. If the container is not deformed, open carefully and examine its contents for conformance to 3.5.4.4.5.3 Lifting. The primer coating shall be applied to test panels designated A (see table I) in accordance with 4.4.1. Panels shall air dry for 5 hours and then be topcoated in accordance with 4.4.2. Examine for conformance to 3.7.3 during and after the drying of the topcoat.4.5.4 Adhesion. The primer coating shall be applied to test panels designated C (see table I) in accordance with 4.4.1. The test panels shall be immersed in distilled water for not less than 24 hours at room temperature (see 4.5). After removal, the panels shall be dried with absorbent paper tissue and within 3 minutes after removal from the water, be tested in accordance with FED-STD-141, Method 6301, for conformance to 3.7.4.4.5.5 Flexibility. The primer coating shall be applied to test panels designated B (seetable I) in accordance with 4.4.1. The flexibility of the coating shall then be tested at the room temperature and relative humidity conditions as specified in 4.5, using a Gardco GE Universal Impact Tester, Model #172 (see 6.8), using a specialized impacter that weighs 3.6 lb and has formed four convex spherical segments on each end, each of different radii and extension. Place the coated panel, film side downward, on the rubber pad at the bottom of the impacter guide. Drop the impacter on the panel through the impacter guide, ensuring that the impression of the entire rim of the impacter is made in the panel. Reverse the impacter ends and drop it through the guide on the panel adjacent to the first area of impact. Using 10 power magnification, examine for conformance to 3.7.5; record the percent elongation corresponding to the largest spherical impression at which no cracking occurs.4.5.6 Infrared reflectance (type II primer coating only). The type II primer coating shall be applied to test panels designated A (see table I) in accordance with 4.4.1. The total reflectance (specular and diffuse) of the primer coating relative to barium sulfate shall be measured using a near infrared spectrophotometer over a range of 700 to 2,600 nm. Examine for conformance to3.7.7.4.5.7 Water resistance. The primer coating shall be applied to test panels designated A (see table I) in accordance with 4.4.1 and topcoated in accordance with 4.4.2. The coated test panels shall then be completely immersed in distilled water maintained at 49 ±3 °C (120 ±5 °F) for four days. Two hours after removal from the water, the coating shall be examined for conformance to 3.8.1.124.5.8 Corrosion resistance.4.5.8.1 Salt spray. Test panels designated A (see table I) shall be prepared with primer coating (see 4.4.1). One half of the primer coated panels shall be topcoated (see 4.4.2). Two intersecting lines shall be scribed diagonally across the coated surface of each panel, exposing the bare substrate. The test panels shall then be placed in a 5 percent salt-spray cabinet for 2,000 hours in accordance with ASTM-B117. After removal, the test panels shall be examined for conformance to 3.8.2.1.4.5.8.2 Filiform. The primer coating shall be applied to test panels designated D (seetable I) in accordance with 4.4.1 and topcoated in accordance with 4.4.2. Two intersectinglines shall be scribed diagonally across the coated surface of the test panels, exposing thebare substrate. The test panels shall then be placed vertically in a desiccator containing 12 Normal (N) HCl for 1 hour at room temperature (see 4.5). Within 5 minutes of removal from the desiccator, the test panels shall be placed in a humidity cabinet maintained at40 ±2 °C (104 ±3 °F) and relative humidity of 80 ±5 percent for 1,000 hours. The test panels shall then be examined for conformance to 3.8.2.2. Filiform corrosion appears as threadlike filaments initiating from the exposed substrate and spreading underneath the coating film. (A description of filiform growth in described in ASTM-D2803.)4.5.9 Solvent resistance (cure). The primer coating shall be applied to test panels designated A (see table I) in accordance with 4.4.1. The primer coating shall then be examined for cure, as follows:a.Soak a cotton terry cloth rag in MEK solvent (see 6.10).b.Rub the coating with the soaked rag for 50 passes (25 back and forth rubs)with firm fingerpressure.c.Examine coating for conformance to 3.8.3.4.5.10 Fluid resistance. The primer coating shall be applied to test panels designated A (see table I) in accordance with 4.4.1. The test panels shall then be separately immersed to half their length for 24 hours in glass covered beakers containing the following liquids:a.Lubricating oil conforming to MIL-PRF-23699, maintained at 121 ±3 °C(250 ±5 °F);b.Hydraulic fluid conforming to MIL-PRF-83282, maintained at 65.5 ±3 °C(150 ±5 °F).After removal from the test fluids, cool the test panels to room temperature (see 4.5) and examine for conformance to 3.8.4.134.5.11 Working properties.4.5.11.1 Mixing and dilution. Thoroughly mix each component separately. Slowly pour component B into component A, while constantly stirring, until the manufacturer's specified volume mixing ratio is achieved. If necessary, dilute the admixed primer coating with thinner conforming to MIL-T-81772, type II (see 6.11). Stir well and allow coating to dwell for 30 minutes. Examine for conformance to 3.9.1.4.5.11.2 Application. Using conventional, airless, high volume, low pressure (HVLP), or electrostatic spray equipment, apply the primer coating to test panels to a dry film thickness of15 to 23 µm (0.6 to 0.9 mil) in accordance with 4.4.1. Examine for conformance to 3.7.1 and 3.9.2.5. PACKAGING5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract or order (see6.2). When actual packaging of materiel is to be performed by DoD personnel, these personnel need to contact the responsible packaging activity to ascertain requisite packaging requirements. Packaging requirements are maintained by the Inventory Control Point’s packaging activity within the Military Department or Defense Agency, or within the Military Department’s System Command. Packaging data retrieval is available from the managing Military Department’s or Defense Agency’s automated packaging files, CD-ROM products, or by contacting the responsible packaging activity.6. NOTES(This section contains information of a general or explanatory nature which may be helpful, but is not mandatory.)6.1 Intended use. The materials covered by this specification are low VOC, corrosion-inhibitive, chemical resistant, and strippable primer coatings. These primer coatings are formulated for the unique performance requirements of military aircraft. These requirements include adhesion to a wide variety of metals and composites, flexibility to withstand tactical maneuvers at low temperatures, corrosion resistance in a marine environment, resistance to leaking aircraft fluids, and low-infrared reflectance for stealth in combat. Type I is for general use. Type II is for use where low infrared reflectance is required. Unless a specific type or class is referenced in a contract or purchase order, type I, class C is the default reference. The non-chromated (class N) primer coatings are for use where federal, state, or local regulations restrict the use of chromate based materials. Class N primer coatings may only be used when authorization for their use is given by the engineering authority for the system or item to which the primer coatings are to be applied. For users of MIL-PRF-23377F, class 2, high-solids coating, use class C of this document.14。
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Clinical Trials The other side of clinical trial monitoring; assuring data quality and procedural adherenceGeorge W Williams Clin Trials 2006; 3; 530 DOI: 10.1177/1740774506073104 The online version of this article can be found at: /cgi/content/abstract/3/6/530Published by:On behalf of:The Society for Clinical TrialsAdditional services and information for Clinical Trials can be found at: Email Alerts: /cgi/alerts Subscriptions: /subscriptions Reprints: /journalsReprints.nav Permissions: /journalsPermissions.nav Citations (this article cites 8 articles hosted on the SAGE Journals Online and HighWire Press platforms): /cgi/content/refs/3/6/530Downloaded from at PENNSYLVANIA STATE UNIV on April 11, 2008 © 2006 The Society for Clinical Trials. All rights reserved. Not for commercial use or unauthorized distribution.Clinical Trials 2006; 3: 530–537ARTICLEThe other side of clinical trial monitoring; assuring data quality and procedural adherenceGeorge W WilliamsBackground Data monitoring can mean different things. It can mean statistical methodologies for clinical trial monitoring, interim data analysis, monitoring for quality control or assurance or safety reporting to regulatory agencies. Purpose The various facets of data monitoring will be discussed and reviewed from primarily an industry perspective. Methods By careful attention to the design and conduct of a clinical trial, the expense of monitoring can be markedly reduced. Careful attention should be given to the qualifications of investigators in the selection of clinical sites and central facilities. Site personnel must be adequately trained. The sponsor should utilize appropriately qualified individuals to supervise the overall conduct of the trial. The monitor should visit the investigator at the site of the investigation frequently enough to ensure acceptable quality. The monitor is responsible for inspecting the case report forms at regular intervals. Quality control should be applied to each stage of data handling to ensure that all data are reliable and have been processed correctly. The auditor will assess whether the site is being monitored in accordance with the monitoring plan. The determination of the extent and nature of monitoring should be based on considerations such as the objective, design and complexity of the trial. Statistical sampling may be an acceptable method for selecting the data to be verified. The monitor should ensure that adverse events are reported. Study data will be monitored on an ongoing basis to ensure patient safety. The sponsor may utilize a Data Monitoring Committee to protect the validity of a trial. Conclusions Discussions between industry, academia and regulatory groups regarding the optimal extent and methods for monitoring of clinical trials are encouraged. Clinical Trials 2006; 3: 530–537. IntroductionMonitors are employed by sponsors to review the conduct of clinical studies to assure that clinical investigators abide by their obligations for the proper conduct of clinical trials. Hence, monitoring is the act of overseeing the progress of a clinical trial and ofensuring that it is conducted, recorded and reported in accordance with the protocol, standard operating procedures (SOPs), good clinical practice (GCP) and applicable regulatory requirements. The extent to which a clinical trial is conducted according to the protocol will have a major impact on the credibility of the results. Careful monitoring can assist in identi-Amgen, Inc., Thousand Oaks, California, USA Author for correspondence: George W Williams, Amgen, Inc., One Amgen Center Drive, MS # 24-2-C, Thousand Oaks, California 91320-1799, USA. E-mail: gewillia@ Based on a presentation at the 10th International Symposium on Long-Term Clinical Trials, Keble College, Oxford, UK, September 2005.© Society for Clinical Trials 200610.1177/1740774506073104Downloaded from at PENNSYLVANIA STATE UNIV on April 11, 2008 © 2006 The Society for Clinical Trials. All rights reserved. Not for commercial use or unauthorized distribution.Monitoring of clinical trialsfying difficulties early and minimizing their subsequent occurrence or recurrence. There are many groups with monitoring responsibility – eg, the sponsor, the investigators, the medical monitor, the regulatory authorities, Institutional Review Boards (IRBs) and Data Monitoring Committees. However, the final accountability for the conduct of a clinical trial is with the study sponsor and study investigators. Instead of endorsing a single approach to study monitoring, the International Conference on Harmonization (ICH) E-6 [1] indicates that every study needs an adequate monitoring/auditing plan, appropriate to the study. Onsite monitoring can range from the industry model (frequent, all sites) to no onsite monitoring at all with central monitoring in conjunction with procedures such as investigator training, investigator meetings and extensive written guidance to assure the appropriate conduct of the trial in accordance with GCP [2]. We will now consider many of these aspects in more detail and consider some of the cost implications of different approaches.531on. These complexities impact the monitoring of clinical trials.Investigator/site selectionCareful attention should be given to the qualifications of investigators in the selection of clinical sites and central facilities for participation in the clinical trial. Many factors need to be considered in the selection of investigators, including their expertise, scientific training, ability to recruit patients and time to devote to the trial. It is the responsibility of the investigator and his site personnel to ensure the adequacy of the research facility for the conduct of the trial and the accuracy of the collected data. All the different facilities involved in the study need to be considered, for example, laboratory areas and the pharmacy, as they may generate study data that need to be examined.Training and pre-investigation meetings Impact of design on monitoringAlthough it may be impossible to avoid all errors and inconsistencies in data generated in clinical trials, careful attention should be devoted during the design, conduct, and analysis stages of clinical trials to minimize these problems.The scientific integrity of the trial and the credibility of the data from the trial depend substantially on trial design. The complexity of the protocol bears directly on the quality of the data. By careful attention to the design and conduct of a clinical trial, the expense of monitoring can be markedly reduced [3,4]. Protocols should be realistic in the amount of data to be collected and the ability of patients and investigators to comply with protocol requirements. The quantity of data that must be collected in a study is flexible, depending on the stage of development of the drug and the nature of the trial [2]. The volume of noncritical data required from a clinical trial should be kept to a minimum. Only important information should be collected. Too much noncritical data only leads to confusion rather than helping the data management and statistical aspects of the trial and often does not contribute substantially to addressing the main objectives of the trial. The more data that are collected, the more cumbersome and complicated the case record forms become, and the greater the likelihood of confusion and error [5]. The increasing complexity of trials includes interactive voice response systems for randomization assignments, imaging centers, central laboratories, contract research organizations (CROs) and so Site personnel must be adequately trained to conduct a study in order to successfully produce quality data. Training of investigators, data managers and laboratory personnel is critical and should include appropriate attention to guidelines for good clinical practices. Training sessions and certification procedures will promote standardization and minimize errors. Periodic retraining and recertification is required. It is important to document training of trial personnel. The monitor’s responsibilities include verifying that the investigator receives the current investigator’s brochure, all trial documents and all trial supplies required to support proper trial conduct and compliance with regulatory requirements. Although a visit to each site can be productive, bringing the investigators and coordinators to a central location can encourage the concentration and interaction desirable to enact the protocol effectively [4]. Topics to be included are: protocol review, the efficacy and safety profile of the treatment, safety monitoring standards and adverse event reporting procedures, case report form (CRF) completion and query resolution, GCP/ICH compliance issues, monitoring issues/regulatory concerns, and drug accountability. Investigators are instructed regarding the importance of accurate/clean data, avoiding protocol violations, and keeping patients in the study.Monitors and training of monitorsThe sponsor should utilize appropriately qualified individuals to supervise the overall conduct of the Clinical Trials 2006; 3: 530–537Downloaded from at PENNSYLVANIA STATE UNIV on April 11, 2008 © 2006 The Society for Clinical Trials. All rights reserved. Not for commercial use or unauthorized distribution.532GW Williamsdiscrepancy reports for unresolved data queries). Documentation and training requirements for new staff should be determined. Reconciliation and discrepancy reports of investigational product shipments to and from the site should be determined. There should be follow-up with the investigators as appropriate relative to the status of IRB/IEC approval of the protocol/protocol amendments and informed consent forms. Typically, the first monitoring visit is to occur within two weeks of the first subject’s randomization. If no subjects are registered within the first month, a visit should occur within four to six weeks to assist with recruitment. Following the first monitoring visit, routine site visits will occur approximately every six to eight weeks. Monitoring requirements and frequency at each clinical site may be modified. When problems are sensed through either a site visit or information transmitted to the sponsor, an unplanned site visit is scheduled. Special laboratories (exercise testing facility, echocardiography lab) must be visited and assessed for compliance.trial, to handle the data, to verify the data, to conduct the statistical analyses, and to prepare the trial reports. A monitor need not be a person qualified to diagnose and treat the disease or other condition for the treatment under study, but review of the study data should include a medically credentialed individual with experience in clinical trials and the treatment population. The factors to be considered in determining the number of monitors and the education, training or expertise necessary should include: the number of investigators conducting the study, the number and location of the facilities in which the study is being conducted, the complexity of the study and the nature of the disease or other condition under study. Monitoring workshops will introduce the study to the monitors [6].Monitoring planThe monitoring plan is designed to ensure that the clinical team members monitor the study in a consistent manner and in accordance with principles of Good Clinical Practice, ICH guidelines and SOPs. A standardized, written procedure, sufficiently detailed to cover the general aspects of clinical investigations, may be used as a basic monitoring plan and supplemented by more specific or additional monitoring procedures tailored to the individual clinical investigation. The monitoring plan is dynamic and should be revised and updated as necessary.Source document verificationThe monitor is responsible for inspecting the case report forms at regular intervals throughout the study to verify adherence to the protocol; completeness, accuracy, and consistency of the data; and adherence to local regulations on the conduct of clinical research. The monitor should have access to subject medical records and other study-related records needed to verify the entities on the case report forms. Typically, for studies conducted to support registrational filings, CRF data will be source verified for all enrolled subjects. Monitors will verify 100% for each subject screened that an informed consent form is on file with appropriately dated signatures and that all pages are present. Monitors will verify 100% that all of the inclusion and exclusion criteria are met for each subject enrolled into the study and will verify primary endpoint data.Clinical site visitsAs noted in the Food and Drug Administration (FDA) guidances [6], the monitor should visit the investigator at the site of the investigation frequently enough to ensure that the facilities continue to be acceptable; the study protocol is being followed; changes to the protocol have been approved by the IRB; accurate, complete and current records are being maintained; accurate, complete and timely reports are being made to the sponsor and the IRB; the investigator is carrying out the agreed upon activities and has not delegated them to other previously unspecified staff; and that subjects’ rights are being protected through a thorough informed consent process. In preparation for the site visit, the monitoring plan should be reviewed. Safety monitoring reports from the safety reporting database or serious adverse events reported by the site or any applicable regulatory agency safety reports (eg, Investigational New Drug (IND) safety reports) since the last monitoring visit should be reviewed. The status of outstanding data should be assessed CRFs, clinical database Clinical Trials 2006; 3: 530–537Informed consentThe clinical manager will be responsible for reviewing the draft informed consent form (ICF). The sponsor must review all ICF drafts prior to submission to the IRB, including any changes requested by the sites’ IRB and verify that the latest version of the informed consent includes the essential elements and complies with the sponsor’s sample informed consent form requirements. The sponsor assures that IRB approval has been obtained prior to the enrollment of subjects Downloaded from at PENNSYLVANIA STATE UNIV on April 11, 2008 © 2006 The Society for Clinical Trials. All rights reserved. Not for commercial use or unauthorized distribution.Monitoring of clinical trialsin the study. The sponsor assures that informed consent was obtained from all subjects in the study.533Patient recruitmentIn trials with a long-time scale for the accrual of subjects, the rate of accrual should be monitored and, if it falls appreciably below the projected level, the reasons should be identified and remedial actions taken in order to protect the power of the trial and address any concerns about quality. If the rate of accrual is above projections at specific clinical sites, it is important to verify that eligible patients are enrolled and that the site has capacity to maintain patients on the study. The monitor should ensure that all withdrawals and dropouts of enrolled subjects from the trial are reported and explained on the CRFs.to be taken and/or actions recommended to secure compliance. The detection of fraud and misconduct is a matter of concern for everybody involved in clinical trials. It requires careful judgement by the monitor including scrutiny of all original documentation for correctness. As Walsh [7] has noted, trends and patterns are most easily identified, however, when all the data from a particular center are assembled and reviewed at the same time. It is important when designing monitoring systems that provision is made for this kind of statistical review.LaboratoriesIf local laboratories are used, their participation in internal and external quality control, quality assurance and accreditation schemes should be evaluated by the study monitors. Central laboratories are frequently used. There should be periodic review of documentation and results from internal and external quality control programs implemented at each core laboratory to ascertain compliance with standards specified in the protocol. Computer systems and interfaces between instruments and databases should be validated. Internal quality control often includes replicate values obtained from aliquots of the same laboratory specimens or repeat readings. External quality control may involve the submission of duplicate laboratory specimens or resubmission of records such as electrocardiograms. The external program may also include the submission of known standards for analyses or reading to detect secular trends [3].Drug accountabilityMonitors are responsible for verifying for the investigational product that: 1) storage times and conditions are acceptable, and that supplies are sufficient throughout the trial; 2) investigational product is supplied only to subjects who are eligible to receive it and at the protocol specified doses; 3) subjects are provided with the necessary instruction on properly using, handling, storing and returning the investigational product; 4) receipt, use and return of the investigational product at the trial sites are controlled and documented adequately; and 5) disposition of unused investigational product at the trial sites complies with applicable regulatory requirements and is in accordance with the sponsor requirements.Site visit reports and follow-upAt the conclusion of a monitoring visit, the monitor should: 1) communicate deviations from the protocol, GCP and regulatory requirements to the investigator; 2) report evidence of detected or suspected scientific misconduct immediately to the clinical manager and the clinical quality assurance group for recommended actions; and 3) ensure query clarifications are made and retained by the investigator. In follow-up to a monitoring visit, the monitoring visit report should be completed. A monitoring report is a written report from the monitor to the sponsor after each site visit and/or other trial related communication according to the sponsor’s SOPs. Reports should include a summary of what the monitor reviewed and the monitor’s statements concerning the significant findings/facts, deviations and deficiencies, conclusions, actions taken or Database cleaning and report preparationQuality control should be applied to each stage of data handling to ensure that all data are reliable and have been processed correctly. To ensure the quality of clinical data across all subjects and sites, a clinical data management review will be performed on subject data received by the sponsor. During this review, subject data will be checked for consistency, omissions and any apparent discrepancies. The methods apply to the accumulating data without any unblinding of treatment allocation in individual patients or treatment groups. As Knatterud et al. [3] have noted, there should be checks of the data analyses. There should be consideration of independently reproducing tabulations and statistical calculations including correct selection of variables from the analysis file, proper definition of variables and cut points and correct formulation of transformations of original variables. Clinical Trials 2006; 3: 530–537Downloaded from at PENNSYLVANIA STATE UNIV on April 11, 2008 © 2006 The Society for Clinical Trials. All rights reserved. Not for commercial use or unauthorized distribution.534GW Williamssize and composition of the sample needs to be determined. While the use of sampling may be acceptable when conducting SDV, there may be occasions when checking the data in totality is appropriate. For example, if the number of patients at a center is relatively small, it might be sensible to check all data during an on-site visit. Alternatively, data could be checked 100% until confidence in the quality has been gained, with subsequent sampling of the data. The sample can be dependent on the nature and volume of data generated. A common approach is often to identify different categories of data, for example, critical and non-critical data. Critical data are those that are central to the objective of the study, and which must be corrected. These would generally be few in number. The non-critical data should, of course, also be correct, but if an item of such data is in error, it is not critical to the study outcome. Non-critical data must be checked for a proportion of the CRFs, for example, 25% [5]. Data validation is the cleaning of trial data after they are entered into a computer database in order to ensure that they attained a reasonable quality level. While data quality is centrally important to the success of clinical trials, perfect data are unnecessary and indeed, may be difficult if not impossible to obtain. As Fong [9] has noted, it has been generally agreed that high quality data are data used to arrive at the same conclusion as perfect data. An acceptable data quality level is one that can be considered good enough to not materially effect the results or conclusions. However, an acceptable data quality level has never been defined in regulatory guidances or the literature. Nevertheless, it is critical to optimize data quality by identifying errors from different sources before any conclusions are drawn from statistical analyses. These comments made by Clarke in a textbook on clinical data management are relevant: ‘Defining, setting up, and applying validation is a time-consuming and labor intensive process, so it is important to assess the value of the effort put into validation against the resulting improvement in the data . . . Validation should ease when there is a fair degree of certainty that any remaining errors will not materially affect the results or conclusions of any analyses or the reliability of the trial’ [10]. As Eisenstein et al. [11] have noted, data measurement and capture errors (ie, errors not evident to investigators and monitors) are more frequent than data processing errors. Inter-observer variability in clinical observations consistently exceeds transcription variability (from the medical record to the CRF). Although data capture errors are more difficult to detect and correct, they may be reduced through education. Reducing a trial’s complexity may be an effective strategy to reduce costs and increase data integrity. AuditingIt is important to note the basic difference between quality control and quality assurance in clinical trials. All of the day-to-day process controls that are accomplished by the internal and on-site monitoring staff and directed toward the control of the clinical study collectively comprise the quality control of the study. On the other hand, quality assurance involves independent review or auditing of key processes or pivotal studies in order to establish that the trial has been conducted in accord with GCP, ICH and SOP [1]. Typically, the responsibility for routinely conducting source document verification (SDV) for all patients involved in a clinical study clearly rests with the study monitor (a quality control activity). The auditor’s responsibility is to look at a proportion of the source document verification that has been undertaken to ensure that the system works and is appropriately documented (a quality assurance activity). The auditor will assess whether the site is being monitored in accordance with the protocol specific monitoring plan and applicable SOPs, if the monitoring plan is adequate for the study and site (the frequency of monitoring visits to support the number of subjects enrolled), and if the monitor is effectively monitoring and managing the site to maintain protocol and GCP compliance [5]. Quality assurance audits are performed during enrollment and early in the trial so as to provide feedback to study teams regarding potential problems with the site, the protocol or the management of the study.Costs and extent of monitoring and extent of data cleaningThe determination of the extent and nature of monitoring should be based on considerations such as the objective, purpose, design, complexity, blinding, size and endpoints of the trial. In general, there is a need for on-site monitoring, before, during and after the trial. However, in exceptional circumstances the sponsor may determine that central monitoring in conjunction with procedures such as investigator training and investigator meetings, and extensive written guidance can assure appropriate conduct of the trial in accordance with GCP [1]. In a web model of clinical trial management, much of the study monitoring is performed electronically allowing monitoring of aspects of study conduct in real time. Problems are identified earlier making them easier to resolve. Auditors need considerably less time at sites, reducing cost and increasing study efficiency [8]. Statistically controlled sampling may be an acceptable method for selecting the data to be verified. The Clinical Trials 2006; 3: 530–537Downloaded from at PENNSYLVANIA STATE UNIV on April 11, 2008 © 2006 The Society for Clinical Trials. All rights reserved. Not for commercial use or unauthorized distribution.Monitoring of clinical trials535Adverse event reportingStudy investigators, of course, have the front-line responsibility for identifying potential adverse effects experienced by study participants, adjusting the intervention accordingly and reporting the experience to the sponsor [12]. Regulations require that United States FDA be promptly notified of serious and unanticipated adverse experiences with the use of investigational articles. The monitor should ensure that adverse events, concomitant medications and comorbidities are reported in accordance with the protocol on the CRFs.Monitoring for safetyStudy data will be monitored on an ongoing basis to ensure patient safety. These reviews will include all available data on incidence of adverse events, serious adverse events, fatalities and events leading to withdrawal. Ongoing review of interval and/or cumulative line listings of reported adverse experiences by medical monitors and/or independent experts are conducted.Data monitoring committeesContinuous monitoring of blinded safety data is the responsibility of the study team. In some cases blinded monitoring of safety data is not sufficient, and, in order to ensure the safety of clinical trial subjects, it is also necessary to periodically review clinical trial data (both efficacy and safety) in an unblinded fashion. When it is necessary for the investigator and sponsor to be blinded to treatment assignments, the sponsor may utilize a committee known as a Data Monitoring Committee (DMC) to protect the validity of a trial and its conclusions. The DMC members are individuals independent of the sponsor. A data monitoring committee is generally considered to be a group of experts in relevant subject matter who review the accumulating data from a clinical trial on an interim basis and who make recommendations to the trial sponsor/ organizer regarding the appropriateness of trial continuation and the need for modifications of any protocol design or trial conduct procedures [13]. Interim monitoring of the data from clinical trials is critical to ensure the safety of the individuals participating and to maintain vigilance over the conduct of the trial. Should, for example, the treatments being tested produce some unexpected toxic effect or an unexpectedly high rate of an anticipated adverse effect, the trial organizers would need to carefully consider whether to modify the trial in some way – reduce the dose, tighten the eligibility criteria, prohibit certain concomitant medications or even stop the trial altogether. Another major purpose of monitoring is to determine whether there is any value to continuing the trial. If the results are so overwhelmingly positive or negative at an interim point in the trial that the ultimate conclusion can be readily predicted, early termination of the trial could be considered. Similarly if it has become clear that obtaining a definitive answer to the trial question is unlikely – for example because the event rate is far lower than had been anticipated and increasing the sample size to account for this is not feasible – then termination could be considered in this situation as well. A final important reason for interim monitoring is to maintain the quality of the trial conduct. If the accrual is lagging or the number of ineligible patients is high or the dropout and or non-compliance rate are high the organizers will want to know this while there is still an opportunity to make adjustments [13]. An important advantage of an independent DMC has to do with maintaining the confidentiality of the interim data. Awareness of interim comparisons can damage the trial by affecting accrual rates, drop out rates, endpoint assessment and other aspects of trial conduct. Limiting this information to the DMC minimizes this danger while still providing assurance that the trial can be modified without introducing bias or stopped if concerns arise [13].Stopping rulesFormal statistical methods of interim analysis to avoid inflated type 1 errors have been developed. These include sequential analysis, group sequential designs and analyses possibly utilizing spending functions, stochastic curtailment, repeated confidence interval approaches, and Bayesian methods. Formal guidelines are not typically defined for toxicity and accrual monitoring. Because of the complexity of randomized clinical trials these statistical procedures are intended to provide helpful guidelines rather than rigid rules about whether early trial termination should occur. Recommendations about trial termination or continuation must be based on a global consideration of all available data from the trial including information on primary and secondary efficacy measures, the frequency and severity of adverse effects and quality of trial conduct, along with relevant information external to the trial.Risk assessment/pharmacovigilance/ pharmacoepidemiologyRisk assessment during product development should be conducted in a thorough and rigorous manner. Clinical Trials 2006; 3: 530–537Downloaded from at PENNSYLVANIA STATE UNIV on April 11, 2008 © 2006 The Society for Clinical Trials. All rights reserved. Not for commercial use or unauthorized distribution.。