Horizontal-stress-contrast-in-the-shallow-marine-sediments-of-the-Gulf-of-Mexico-sites-Walker-Ridge
仪器分析专业名词英文及名词解释
仪器分析专业名词英文及名词解释仪器分析专业名词英文及名词解释一、紫外-可见光分光光度法1、透光率(transmittance):透过样品的光强度与入射光强度之比。
2、吸收度(absorbance ):透光率的负对数。
3、生色团(chromophore ):含有n—n*或n—n*跃迁的基团。
4、助色团(auxochrome):含孤对电子(非键电子)的杂原子基团。
5、摩尔吸收系数(molar absorptivity):—定波长时,溶液浓度为1mol/L,光程为1cm时的吸收度。
6、比吸收系数(specific absorptivity ):—定波长时,溶液浓度为1%(W/V ),光程为1cm时的吸收度。
7、红移(red shift):化合物结构改变(共轭,引入助色团,溶剂改变等),使吸收峰向长波长移动的现象。
8、蓝移(blue shift):当化合物结构改变或受溶剂的影响等原因使吸收峰向短波长移动的现象。
也称短移(hypso chromic shift )。
9、增色效应(hyperchromic effect):由于化合物结构改变或其他原因使吸收强度增加的效应。
10、减色效应(hypochromic effect):由于化合物结构改变或其他原因使吸收强度减弱的效应。
11、末端吸收(end absorption ):在短波长处(200nm左右) 只呈现强吸收,而不成峰形的部分。
12、标准对照法:在相同条件下配制标准溶液和样品溶液,在选定的波长下分别测定吸光度,根据朗伯-比尔定律计算样品浓度的定量定性分析方法。
13、K带:共轭双键中n—n*跃迁所产生的吸收带,强吸收,£>104。
14、R带:由n—n*引起的吸收带,弱吸收。
15、吸收带:吸收峰在紫外可见光谱中的波带位置(R、K、B和E 带)。
16、B带和E带:芳香族(含芳香族)化合物的特征吸收带。
二、荧光分析法1、荧光(fluorescence):由第一激发单线态的最低振动能级回到基态任一振动能级时发射的光。
ASTM D790
Designation:D790–03Standard Test Methods forFlexural Properties of Unreinforced and Reinforced Plastics and Electrical Insulating Materials1This standard is issued under thefixed designation D790;the number immediately following the designation indicates the year of original adoption or,in the case of revision,the year of last revision.A number in parentheses indicates the year of last reapproval.A superscript epsilon(e)indicates an editorial change since the last revision or reapproval.This standard has been approved for use by agencies of the Department of Defense.1.Scope*1.1These test methods cover the determination offlexural properties of unreinforced and reinforced plastics,including high-modulus composites and electrical insulating materials in the form of rectangular bars molded directly or cut from sheets, plates,or molded shapes.These test methods are generally applicable to both rigid and semirigid materials.However,flexural strength cannot be determined for those materials that do not break or that do not fail in the outer surface of the test specimen within the5.0%strain limit of these test methods. These test methods utilize a three-point loading system applied to a simply supported beam.A four-point loading system method can be found in Test Method D6272.1.1.1Procedure A,designed principally for materials that break at comparatively small deflections.1.1.2Procedure B,designed particularly for those materials that undergo large deflections during testing.1.1.3Procedure A shall be used for measurement offlexural properties,particularlyflexural modulus,unless the material specification states otherwise.Procedure B may be used for measurement offlexural strength only.Tangent modulus data obtained by Procedure A tends to exhibit lower standard deviations than comparable data obtained by means of Proce-dure B.1.2Comparative tests may be run in accordance with either procedure,provided that the procedure is found satisfactory for the material being tested.1.3The values stated in SI units are to be regarded as the standard.The values provided in parentheses are for informa-tion only.1.4This standard does not purport to address all of the safety concerns,if any,associated with its use.It is the responsibility of the user of this standard to establish appro-priate safety and health practices and determine the applica-bility of regulatory limitations prior to use.N OTE1—These test methods are not technically equivalent to ISO178.2.Referenced Documents2.1ASTM Standards:2D618Practice for Conditioning Plastics for TestingD638Test Method for Tensile Properties of PlasticsD883Terminology Relating to PlasticsD4000Classification System for Specifying Plastic Mate-rialsD5947Test Methods for Physical Dimensions of Solid Plastics SpecimensD6272Test Method for Flexural Properties of Unrein-forced and Reinforced Plastics and Electrical Insulating Materials by Four-Point BendingE4Practices for Force Verification of Testing Machines E691Practice for Conducting an Interlaboratory Study to Determine the Precision of a Test Method3.Terminology3.1Definitions—Definitions of terms applying to these test methods appear in Terminology D883and Annex A1of Test Method D638.4.Summary of Test Method4.1A bar of rectangular cross section rests on two supports and is loaded by means of a loading nose midway between the supports(see Fig.1).A support span-to-depth ratio of16:1 shall be used unless there is reason to suspect that a larger span-to-depth ratio may be required,as may be the case for certain laminated materials(see Section7and Note8for guidance).4.2The specimen is deflected until rupture occurs in the outer surface of the test specimen or until a maximum strain (see12.7)of5.0%is reached,whichever occursfirst.4.3Procedure A employs a strain rate of0.01mm/mm/min [0.01in./in./min]and is the preferred procedure for this test1These test methods are under the jurisdiction of ASTM Committee D20onPlastics and are the direct responsibility of Subcommittee D20.10on Mechanical Properties.Current edition approved March10,2003.Published April2003.Originally approved st previous edition approved in2002as D790–02.2For referenced ASTM standards,visit the ASTM website,,or contact ASTM Customer Service at service@.For Annual Book of ASTM Standards volume information,refer to the standard’s Document Summary page on the ASTM website.1*A Summary of Changes section appears at the end of this standard. Copyright©ASTM International,100Barr Harbor Drive,PO Box C700,West Conshohocken,PA19428-2959,United States.method,while Procedure B employs a strain rate of 0.10mm/mm/min [0.10in./in./min].5.Significance and Use5.1Flexural properties as determined by these test methods are especially useful for quality control and specification purposes.5.2Materials that do not fail by the maximum strain allowed under these test methods (3-point bend)may be more suited to a 4-point bend test.The basic difference between the two test methods is in the location of the maximum bending moment and maximum axial fiber stresses.The maximum axial fiber stresses occur on a line under the loading nose in 3-point bending and over the area between the loading noses in 4-point bending.5.3Flexural properties may vary with specimen depth,temperature,atmospheric conditions,and the difference in rate of straining as specified in Procedures A and B (see also Note 8).5.4Before proceeding with these test methods,reference should be made to the specification of the material being tested.Any test specimen preparation,conditioning,dimensions,or testing parameters,or combination thereof,covered in the materials specification shall take precedence over those men-tioned in these test methods.If there are no material specifi-cations,then the default conditions apply.Table 1in Classifi-cation System D 4000lists the ASTM materials standards that currently exist for plastics.6.Apparatus6.1Testing Machine —A properly calibrated testing ma-chine that can be operated at constant rates of crosshead motion over the range indicated,and in which the error in the load measuring system shall not exceed 61%of the maximum load expected to be measured.It shall be equipped with a deflection measuring device.The stiffness of the testing machine shall besuch that the total elastic deformation of the system does not exceed 1%of the total deflection of the test specimen during testing,or appropriate corrections shall be made.The load indicating mechanism shall be essentially free from inertial lag at the crosshead rate used.The accuracy of the testing machine shall be verified in accordance with Practices E 4.6.2Loading Noses and Supports —The loading nose and supports shall have cylindrical surfaces.In order to avoid excessive indentation,or failure due to stress concentration directly under the loading nose,the radii of the loading nose and supports shall be 5.060.1mm [0.19760.004in.]unless otherwise specified or agreed upon between the interested clients.When other loading noses and supports are used they must comply with the following requirements:they shall have a minimum radius of 3.2mm [1⁄8in.]for all specimens,and for specimens 3.2mm or greater in depth,the radius of the supports may be up to 1.6times the specimen depth.They shall be this large if significant indentation or compressive failure occurs.The arc of the loading nose in contact with the specimen shall be sufficiently large to prevent contact of the specimen with the sides of the nose (see Fig.1).The maximum radius of the loading nose shall be no more than 4times the specimen depth.N OTE 2—Test data have shown that the loading nose and support dimensions can influence the flexural modulus and flexural strength values.The loading nose dimension has the greater influence.Dimensions of the loading nose and supports must be specified in the material specification.6.3Micrometers —Suitable micrometers for measuring the width and thickness of the test specimen to an incremental discrimination of at least 0.025mm [0.001in.]should be used.All width and thickness measurements of rigid and semirigid plastics may be measured with a hand micrometer with ratchet.A suitable instrument for measuring the thickness of nonrigid test specimens shall have:a contact measuring pressure of 2562.5kPa [3.660.36psi],a movable circular contact foot 6.3560.025mm [0.25060.001in.]in diameter and a lower fixed anvil large enough to extend beyond the contact foot in all directions and being parallel to the contact foot within 0.005mm [0.002in.]over the entire foot area.Flatness of foot and anvil shall conform to the portion of the Calibration section of Test Methods D 5947.N OTE —(a )Minimum radius =3.2mm [1⁄8in.].(b )Maximum radius supports 1.6times specimen depth;maximum radius loading nose =4times specimen depth.FIG.1Allowable Range of Loading Nose and Support RadiiTABLE 1Flexural StrengthMaterial Mean,103psiValues Expressed in Units of %of 103psi V r A V R B r C R D ABS9.99 1.59 6.05 4.4417.2DAP thermoset 14.3 6.58 6.5818.618.6Cast acrylic 16.3 1.6711.3 4.7332.0GR polyester19.5 1.43 2.14 4.05 6.08GR polycarbonate 21.0 5.16 6.0514.617.1SMC26.04.767.1913.520.4AV r =within-laboratory coefficient of variation for the indicated material.It is obtained by first pooling the within-laboratory standard deviations of the test results from all of the participating laboratories:Sr =[[(s 1)2+(s 2)2...+(s n )2]/n]1/2then V r =(S r divided by the overall average for the material)3100.BV r =between-laboratory reproducibility,expressed as the coefficient of varia-tion:S R ={S r 2+S L 2}1/2where S L is the standard deviation of laboratory means.Then:V R =(S R divided by the overall average for the material)3100.Cr =within-laboratory critical interval between two test results =2.83V r .DR =between-laboratory critical interval between two test results =2.83V R.27.Test Specimens7.1The specimens may be cut from sheets,plates,or molded shapes,or may be molded to the desiredfinished dimensions.The actual dimensions used in Section4.2,Cal-culation,shall be measured in accordance with Test Methods D5947.N OTE3—Any necessary polishing of specimens shall be done only in the lengthwise direction of the specimen.7.2Sheet Materials(Except Laminated Thermosetting Ma-terials and Certain Materials Used for Electrical Insulation, Including Vulcanized Fiber and Glass Bonded Mica):7.2.1Materials1.6mm[1⁄16in.]or Greater in Thickness—Forflatwise tests,the depth of the specimen shall be the thickness of the material.For edgewise tests,the width of the specimen shall be the thickness of the sheet,and the depth shall not exceed the width(see Notes4and5).For all tests,the support span shall be16(tolerance61)times the depth of the beam.Specimen width shall not exceed one fourth of the support span for specimens greater than3.2mm[1⁄8in.]in depth.Specimens3.2mm or less in depth shall be12.7mm[1⁄2 in.]in width.The specimen shall be long enough to allow for overhanging on each end of at least10%of the support span, but in no case less than6.4mm[1⁄4in.]on each end.Overhang shall be sufficient to prevent the specimen from slipping through the supports.N OTE4—Whenever possible,the original surface of the sheet shall be unaltered.However,where testing machine limitations make it impossible to follow the above criterion on the unaltered sheet,one or both surfaces shall be machined to provide the desired dimensions,and the location of the specimens with reference to the total depth shall be noted.The value obtained on specimens with machined surfaces may differ from those obtained on specimens with original surfaces.Consequently,any specifi-cations forflexural properties on thicker sheets must state whether the original surfaces are to be retained or not.When only one surface was machined,it must be stated whether the machined surface was on the tension or compression side of the beam.N OTE5—Edgewise tests are not applicable for sheets that are so thin that specimens meeting these requirements cannot be cut.If specimen depth exceeds the width,buckling may occur.7.2.2Materials Less than1.6mm[1⁄16in.]in Thickness—The specimen shall be50.8mm[2in.]long by12.7mm[1⁄2in.] wide,testedflatwise on a25.4-mm[1-in.]support span.N OTE6—Use of the formulas for simple beams cited in these test methods for calculating results presumes that beam width is small in comparison with the support span.Therefore,the formulas do not apply rigorously to these dimensions.N OTE7—Where machine sensitivity is such that specimens of these dimensions cannot be measured,wider specimens or shorter support spans,or both,may be used,provided the support span-to-depth ratio is at least14to1.All dimensions must be stated in the report(see also Note6).7.3Laminated Thermosetting Materials and Sheet and Plate Materials Used for Electrical Insulation,Including Vulcanized Fiber and Glass-Bonded Mica—For paper-base and fabric-base grades over25.4mm[1in.]in nominal thickness,the specimens shall be machined on both surfaces to a depth of25.4mm.For glass-base and nylon-base grades, specimens over12.7mm[1⁄2in.]in nominal depth shall be machined on both surfaces to a depth of12.7mm.The support span-to-depth ratio shall be chosen such that failures occur in the outerfibers of the specimens,due only to the bending moment(see Note8).Therefore,a ratio larger than16:1may be necessary(32:1or40:1are recommended).When laminated materials exhibit low compressive strength perpendicular to the laminations,they shall be loaded with a large radius loading nose(up to four times the specimen depth to prevent premature damage to the outerfibers.7.4Molding Materials(Thermoplastics and Thermosets)—The recommended specimen for molding materials is127by 12.7by3.2mm[5by1⁄2by1⁄8in.]testedflatwise on a support span,resulting in a support span-to-depth ratio of16(tolerance 61).Thicker specimens should be avoided if they exhibit significant shrink marks or bubbles when molded.7.5High-Strength Reinforced Composites,Including Highly Orthotropic Laminates—The span-to-depth ratio shall be cho-sen such that failure occurs in the outerfibers of the specimens and is due only to the bending moment(see Note8).A span-to-depth ratio larger than16:1may be necessary(32:1or 40:1are recommended).For some highly anisotropic compos-ites,shear deformation can significantly influence modulus measurements,even at span-to-depth ratios as high as40:1. Hence,for these materials,an increase in the span-to-depth ratio to60:1is recommended to eliminate shear effects when modulus data are required,it should also be noted that the flexural modulus of highly anisotropic laminates is a strong function of ply-stacking sequence and will not necessarily correlate with tensile modulus,which is not stacking-sequence dependent.N OTE8—As a general rule,support span-to-depth ratios of16:1are satisfactory when the ratio of the tensile strength to shear strength is less than8to1,but the support span-to-depth ratio must be increased for composite laminates having relatively low shear strength in the plane of the laminate and relatively high tensile strength parallel to the support span.8.Number of Test Specimens8.1Test at leastfive specimens for each sample in the case of isotropic materials or molded specimens.8.2For each sample of anisotropic material in sheet form, test at leastfive specimens for each of the following conditions. Recommended conditions areflatwise and edgewise tests on specimens cut in lengthwise and crosswise directions of the sheet.For the purposes of this test,“lengthwise”designates the principal axis of anisotropy and shall be interpreted to mean the direction of the sheet known to be stronger inflexure.“Cross-wise”indicates the sheet direction known to be the weaker in flexure and shall be at90°to the lengthwise direction.9.Conditioning9.1Conditioning—Condition the test specimens at236 2°C[73.463.6°F]and5065%relative humidity for not less than40h prior to test in accordance with Procedure A of Practice D618unless otherwise specified by contract or the relevant ASTM material specification.Reference pre-test con-ditioning,to settle disagreements,shall apply tolerances of 61°C[1.8°F]and62%relative humidity.9.2Test Conditions—Conduct the tests at2362°C[73.46 3.6°F]and5065%relative humidity unlessotherwise 3specified by contract or the relevant ASTM material specifica-tion.Reference testing conditions,to settle disagreements, shall apply tolerances of61°C[1.8°F]and62%relative humidity.10.Procedure10.1Procedure A:10.1.1Use an untested specimen for each measurement. Measure the width and depth of the specimen to the nearest 0.03mm[0.001in.]at the center of the support span.For specimens less than2.54mm[0.100in.]in depth,measure the depth to the nearest0.003mm[0.0005in.].These measure-ments shall be made in accordance with Test Methods D5947.10.1.2Determine the support span to be used as described in Section7and set the support span to within1%of the determined value.10.1.3Forflexuralfixtures that have continuously adjust-able spans,measure the span accurately to the nearest0.1mm [0.004in.]for spans less than63mm[2.5in.]and to the nearest 0.3mm[0.012in.]for spans greater than or equal to63mm [2.5in.].Use the actual measured span for all calculations.For flexuralfixtures that havefixed machined span positions,verify the span distance the same as for adjustable spans at each machined position.This distance becomes the span for that position and is used for calculations applicable to all subse-quent tests conducted at that position.See Annex A2for information on the determination of and setting of the span.10.1.4Calculate the rate of crosshead motion as follows and set the machine for the rate of crosshead motion as calculated by Eq1:R5ZL2/6d(1) where:R=rate of crosshead motion,mm[in.]/min,L=support span,mm[in.],d=depth of beam,mm[in.],andZ=rate of straining of the outerfiber,mm/mm/min[in./ in./min].Z shall be equal to0.01.In no case shall the actual crosshead rate differ from that calculated using Eq1,by more than610%.10.1.5Align the loading nose and supports so that the axes of the cylindrical surfaces are parallel and the loading nose is midway between the supports.The parallelism of the apparatus may be checked by means of a plate with parallel grooves into which the loading nose and supports willfit when properly aligned(see A2.3).Center the specimen on the supports,with the long axis of the specimen perpendicular to the loading nose and supports.10.1.6Apply the load to the specimen at the specified crosshead rate,and take simultaneous load-deflection data. Measure deflection either by a gage under the specimen in contact with it at the center of the support span,the gage being mounted stationary relative to the specimen supports,or by measurement of the motion of the loading nose relative to the supports.Load-deflection curves may be plotted to determine theflexural strength,chord or secant modulus or the tangent modulus of elasticity,and the total work as measured by the area under the load-deflection curve.Perform the necessary toe compensation(see Annex A1)to correct for seating and indentation of the specimen and deflections in the machine.10.1.7Terminate the test when the maximum strain in the outer surface of the test specimen has reached0.05mm/mm [in./in.]or at break if break occurs prior to reaching the maximum strain(Notes9and10).The deflection at which this strain will occur may be calculated by letting r equal0.05 mm/mm[in./in.]in Eq2:D5rL2/6d(2) where:D=midspan deflection,mm[in.],r=strain,mm/mm[in./in.],L=support span,mm[in.],andd=depth of beam,mm[in.].N OTE9—For some materials that do not yield or break within the5% strain limit when tested by Procedure A,the increased strain rate allowed by Procedure B(see10.2)may induce the specimen to yield or break,or both,within the required5%strain limit.N OTE10—Beyond5%strain,this test method is not applicable.Some other mechanical property might be more relevant to characterize mate-rials that neither yield nor break by either Procedure A or Procedure B within the5%strain limit(for example,Test Method D638may be considered).10.2Procedure B:10.2.1Use an untested specimen for each measurement.10.2.2Test conditions shall be identical to those described in10.1,except that the rate of straining of the outer surface of the test specimen shall be0.10mm/mm[in./in.]/min.10.2.3If no break has occurred in the specimen by the time the maximum strain in the outer surface of the test specimen has reached0.05mm/mm[in./in.],discontinue the test(see Note10).11.Retests11.1Values for properties at rupture shall not be calculated for any specimen that breaks at some obvious,fortuitousflaw, unless suchflaws constitute a variable being studied.Retests shall be made for any specimen on which values are not calculated.12.Calculation12.1Toe compensation shall be made in accordance with Annex A1unless it can be shown that the toe region of the curve is not due to the take-up of slack,seating of the specimen,or other artifact,but rather is an authentic material response.12.2Flexural Stress(s f)—When a homogeneous elastic material is tested inflexure as a simple beam supported at two points and loaded at the midpoint,the maximum stress in the outer surface of the test specimen occurs at the midpoint.This stress may be calculated for any point on the load-deflection curve by means of the following equation(see Notes11-13):s f53PL/2bd2(3)where:s=stress in the outerfibers at midpoint,MPa[psi], 4P=load at a given point on the load-deflection curve,N [lbf],L=support span,mm[in.],b=width of beam tested,mm[in.],andd=depth of beam tested,mm[in.].N OTE11—Eq3applies strictly to materials for which stress is linearly proportional to strain up to the point of rupture and for which the strains are small.Since this is not always the case,a slight error will be introduced if Eq3is used to calculate stress for materials that are not true Hookean materials.The equation is valid for obtaining comparison data and for specification purposes,but only up to a maximumfiber strain of 5%in the outer surface of the test specimen for specimens tested by the procedures described herein.N OTE12—When testing highly orthotropic laminates,the maximum stress may not always occur in the outer surface of the test specimen.3 Laminated beam theory must be applied to determine the maximum tensile stress at failure.If Eq3is used to calculate stress,it will yield an apparent strength based on homogeneous beam theory.This apparent strength is highly dependent on the ply-stacking sequence of highly orthotropic laminates.N OTE13—The preceding calculation is not valid if the specimen slips excessively between the supports.12.3Flexural Stress for Beams Tested at Large Support Spans(s f)—If support span-to-depth ratios greater than16to 1are used such that deflections in excess of10%of the support span occur,the stress in the outer surface of the specimen for a simple beam can be reasonably approximated with the following equation(see Note14):s f5~3PL/2bd2!@116~D/L!224~d/L!~D/L!#(4) where:s f,P,L,b,and d are the same as for Eq3,andD=deflection of the centerline of the specimen at the middle of the support span,mm[in.].N OTE14—When large support span-to-depth ratios are used,significant end forces are developed at the support noses which will affect the moment in a simple supported beam.Eq4includes additional terms that are an approximate correction factor for the influence of these end forces in large support span-to-depth ratio beams where relatively large deflec-tions exist.12.4Flexural Strength(s fM)—Maximumflexural stress sustained by the test specimen(see Note12)during a bending test.It is calculated according to Eq3or Eq4.Some materials that do not break at strains of up to5%may give a load deflection curve that shows a point at which the load does not increase with an increase in strain,that is,a yield point(Fig.2, Curve B),Y.Theflexural strength may be calculated for these materials by letting P(in Eq3or Eq4)equal this point,Y.12.5Flexural Offset Yield Strength—Offset yield strength is the stress at which the stress-strain curve deviates by a given strain(offset)from the tangent to the initial straight line portion of the stress-strain curve.The value of the offset must be given whenever this property is calculated.N OTE15—This value may differ fromflexural strength defined in12.4.Both methods of calculation are described in the annex to Test Method D638.12.6Flexural Stress at Break(s fB)—Flexural stress at break of the test specimen during a bending test.It is calculated according to Eq3or Eq4.Some materials may give a load deflection curve that shows a break point,B,without a yield point(Fig.2,Curve a)in which case s fB=s fM.Other materials may give a yield deflection curve with both a yield and a break point,B(Fig.2,Curve b).Theflexural stress at break may be calculated for these materials by letting P(in Eq 3or Eq4)equal this point,B.12.7Stress at a Given Strain—The stress in the outer surface of a test specimen at a given strain may be calculated in accordance with Eq3or Eq4by letting P equal the load read from the load-deflection curve at the deflection corresponding to the desired strain(for highly orthotropic laminates,see Note 12).12.8Flexural Strain,e f—Nominal fractional change in the length of an element of the outer surface of the test specimen at midspan,where the maximum strain occurs.It may be calculated for any deflection using Eq5:e f56Dd/L2(5) where:e f=strain in the outer surface,mm/mm[in./in.],D=maximum deflection of the center of the beam,mm [in.],L=support span,mm[in.],and3For a discussion of these effects,see Zweben,C.,Smith,W.S.,and Wardle,M. W.,“Test Methods for Fiber Tensile Strength,Composite Flexural Modulus and Properties of Fabric-Reinforced Laminates,“Composite Materials:Testing and Design(Fifth Conference),ASTM STP674,1979,pp.228–262.N OTE—Curve a:Specimen that breaks before yielding.Curve b:Specimen that yields and then breaks before the5%strain limit.Curve c:Specimen that neither yields nor breaks before the5%strain limit.FIG.2Typical Curves of Flexural Stress(ßf)Versus FlexuralStrain(ef)5d =depth,mm [in.].12.9Modulus of Elasticity :12.9.1Tangent Modulus of Elasticity —The tangent modu-lus of elasticity,often called the “modulus of elasticity,”is the ratio,within the elastic limit,of stress to corresponding strain.It is calculated by drawing a tangent to the steepest initial straight-line portion of the load-deflection curve and using Eq 6(for highly anisotropic composites,see Note 16).E B 5L 3m /4bd3(6)where:E B =modulus of elasticity in bending,MPa [psi],L =support span,mm [in.],b =width of beam tested,mm [in.],d =depth of beam tested,mm [in.],andm =slope of the tangent to the initial straight-line portion of the load-deflection curve,N/mm [lbf/in.]of deflec-tion.N OTE 16—Shear deflections can seriously reduce the apparent modulus of highly anisotropic composites when they are tested at low span-to-depth ratios.3For this reason,a span-to-depth ratio of 60to 1is recommended for flexural modulus determinations on these composites.Flexural strength should be determined on a separate set of replicate specimens at a lower span-to-depth ratio that induces tensile failure in the outer fibers of the beam along its lower face.Since the flexural modulus of highly anisotropic laminates is a critical function of ply-stacking sequence,it will not necessarily correlate with tensile modulus,which is not stacking-sequence dependent.12.9.2Secant Modulus —The secant modulus is the ratio ofstress to corresponding strain at any selected point on the stress-strain curve,that is,the slope of the straight line that joins the origin and a selected point on the actual stress-strain curve.It shall be expressed in megapascals [pounds per square inch].The selected point is chosen at a prespecified stress or strain in accordance with the appropriate material specification or by customer contract.It is calculated in accordance with Eq 6by letting m equal the slope of the secant to the load-deflection curve.The chosen stress or strain point used for the determination of the secant shall be reported.12.9.3Chord Modulus (E f )—The chord modulus may be calculated from two discrete points on the load deflectioncurve.The selected points are to be chosen at two prespecified stress or strain points in accordance with the appropriate material specification or by customer contract.The chosen stress or strain points used for the determination of the chord modulus shall be reported.Calculate the chord modulus,E f using the following equation:E f 5~s f 22s f 1!/~e f 22e f 1!(7)where:s f 2and s f 1are the flexural stresses,calculated from Eq 3or Eq 4and measured at the predefined points on the load deflection curve,and e f 2ande f 1are the flexural strain values,calculated from Eq 5and measured at the predetermined points on the load deflection curve.12.10Arithmetic Mean —For each series of tests,the arithmetic mean of all values obtained shall be calculated to three significant figures and reported as the “average value”for the particular property in question.12.11Standard Deviation —The standard deviation (esti-mated)shall be calculated as follows and be reported to two significant figures:s 5=~(X 22nX¯2!/~n 21!(8)where:s =estimated standard deviation,X =value of single observation,n =number of observations,andX¯=arithmetic mean of the set of observations.13.Report13.1Report the following information:13.1.1Complete identification of the material tested,includ-ing type,source,manufacturer’s code number,form,principal dimensions,and previous history (for laminated materials,ply-stacking sequence shall be reported),13.1.2Direction of cutting and loading specimens,when appropriate,13.1.3Conditioning procedure,13.1.4Depth and width of specimen,13.1.5Procedure used (A or B),13.1.6Support span length,13.1.7Support span-to-depth ratio if different than 16:1,13.1.8Radius of supports and loading noses if different than 5mm,13.1.9Rate of crosshead motion,13.1.10Flexural strain at any given stress,average value and standard deviation,13.1.11If a specimen is rejected,reason(s)for rejection,13.1.12Tangent,secant,or chord modulus in bending,average value,standard deviation,and the strain level(s)used if secant or chord modulus,13.1.13Flexural strength (if desired),average value,and standard deviation,13.1.14Stress at any given strain up to and including 5%(if desired),with strain used,average value,and standard devia-tion,TABLE 2Flexural ModulusMaterial Mean,103psiValues Expressed in units of %of 103psi V r A V R B r C R D ABS338 4.797.6913.621.8DAP thermoset 485 2.897.188.1520.4Cast acrylic 81013.716.138.845.4GR polyester816 3.49 4.209.9111.9GR polycarbonate 1790 5.52 5.5215.615.6SMC195010.913.830.839.1AV r =within-laboratory coefficient of variation for the indicated material.It is obtained by first pooling the within-laboratory standard deviations of the test results from all of the participating laboratories:Sr =[[(s 1)2+(s 2)2...+(s n )2]/n ]1/2then V r =(S r divided by the overall average for the material)3100.BV r =between-laboratory reproducibility,expressed as the coefficient of varia-tion:S R ={S r 2+S L 2}1/2where S L is the standard deviation of laboratory means.Then:V R =(S R divided by the overall average for the material)3100.Cr =within-laboratory critical interval between two test results =2.83V r .DR =between-laboratory critical interval between two test results =2.83V R.6。
斯仑贝谢所有测井曲线英文名称解释
斯仑贝谢所有测井曲线英文名称解释OCEAN DRILLING PROGRAMACRONYMS USED FOR WIRELINE SCHLUMBERGER TOOLS ACT Aluminum Clay ToolAMS Auxiliary Measurement SondeAPS Accelerator Porosity SondeARI Azimuthal Resistivity ImagerASI Array Sonic ImagerBGKT Vertical Seismic Profile ToolBHC Borehole Compensated Sonic ToolBHTV Borehole TeleviewerCBL Casing Bond LogCNT Compensated Neutron ToolDIT Dual Induction ToolDLL Dual LaterologDSI Dipole Sonic ImagerFMS Formation MicroScannerGHMT Geologic High Resolution Magnetic ToolGPIT General Purpose Inclinometer ToolGR Natural Gamma RayGST Induced Gamma Ray Spectrometry ToolHLDS Hostile Environment Lithodensity SondeHLDT Hostile Environment Lithodensity ToolHNGS Hostile Environment Gamma Ray SondeLDT Lithodensity ToolLSS Long Spacing Sonic ToolMCD Mechanical Caliper DeviceNGT Natural Gamma Ray Spectrometry ToolNMRT Nuclear Resonance Magnetic ToolQSST Inline Checkshot ToolSDT Digital Sonic ToolSGT Scintillation Gamma Ray ToolSUMT Susceptibility Magnetic ToolUBI Ultrasonic Borehole ImagerVSI Vertical Seismic ImagerWST Well Seismic ToolWST-3 3-Components Well Seismic ToolOCEAN DRILLING PROGRAMACRONYMS USED FOR LWD SCHLUMBERGER TOOLSADN Azimuthal Density-NeutronCDN Compensated Density-NeutronCDR Compensated Dual ResistivityISONIC Ideal Sonic-While-DrillingNMR Nuclear Magnetic ResonanceRAB Resistivity-at-the-BitOCEAN DRILLING PROGRAMACRONYMS USED FOR NON-SCHLUMBERGER SPECIALTY TOOLSMCS Multichannel Sonic ToolMGT Multisensor Gamma ToolSST Shear Sonic ToolTAP Temperature-Acceleration-Pressure ToolTLT Temperature Logging ToolOCEAN DRILLING PROGRAMACRONYMS AND UNITS USED FOR WIRELINE SCHLUMBERGER LOGSAFEC APS Far Detector Counts (cps)ANEC APS Near Detector Counts (cps)AX Acceleration X Axis (ft/s2)AY Acceleration Y Axis (ft/s2)AZ Acceleration Z Axis (ft/s2)AZIM Constant Azimuth for Deviation Correction (deg)APLC APS Near/Array Limestone Porosity Corrected (%)C1 FMS Caliper 1 (in)C2 FMS Caliper 2 (in)CALI Caliper (in)CFEC Corrected Far Epithermal Counts (cps)CFTC Corrected Far Thermal Counts (cps)CGR Computed (Th+K) Gamma Ray (API units)CHR2 Peak Coherence, Receiver Array, Upper DipoleCHRP Compressional Peak Coherence, Receiver Array, P&SCHRS Shear Peak Coherence, Receiver Array, P&SCHTP Compressional Peak Coherence, Transmitter Array, P&SCHTS Shear Peak Coherence, Transmitter Array, P&SCNEC Corrected Near Epithermal Counts (cps)CNTC Corrected Near Thermal Counts (cps)CS Cable Speed (m/hr)CVEL Compressional Velocity (km/s)DATN Discriminated Attenuation (db/m)DBI Discriminated Bond IndexDEVI Hole Deviation (degrees)DF Drilling Force (lbf)DIFF Difference Between MEAN and MEDIAN in Delta-Time Proc. (microsec/ft) DRH HLDS Bulk Density Correction (g/cm3)DRHO Bulk Density Correction (g/cm3)DT Short Spacing Delta-Time (10'-8' spacing; microsec/ft)DT1 Delta-Time Shear, Lower Dipole (microsec/ft)DT2 Delta-Time Shear, Upper Dipole (microsec/ft)DT4P Delta- Time Compressional, P&S (microsec/ft)DT4S Delta- Time Shear, P&S (microsec/ft))DT1R Delta- Time Shear, Receiver Array, Lower Dipole (microsec/ft)DT2R Delta- Time Shear, Receiver Array, Upper Dipole (microsec/ft)DT1T Delta-Time Shear, Transmitter Array, Lower Dipole (microsec/ft)DT2T Delta-Time Shear, Transmitter Array, Upper Dipole (microsec/ft)DTCO Delta- Time Compressional (microsec/ft)DTL Long Spacing Delta-Time (12'-10' spacing; microsec/ft)DTLF Long Spacing Delta-Time (12'-10' spacing; microsec/ft)DTLN Short Spacing Delta-Time (10'-8' spacing; microsec/ftDTRP Delta-Time Compressional, Receiver Array, P&S (microsec/ft)DTRS Delta-Time Shear, Receiver Array, P&S (microsec/ft)DTSM Delta-Time Shear (microsec/ft)DTST Delta-Time Stoneley (microsec/ft)DTTP Delta-Time Compressional, Transmitter Array, P&S (microsec/ft)DTTS Delta-Time Shear, Transmitter Array, P&S (microsec/ft)ECGR Environmentally Corrected Gamma Ray (API units)EHGR Environmentally Corrected High Resolution Gamma Ray (API units) ENPH Epithermal Neutron Porosity (%)ENRA Epithermal Neutron RatioETIM Elapsed Time (sec)FINC Magnetic Field Inclination (degrees)FNOR Magnetic Field Total Moment (oersted)FX Magnetic Field on X Axis (oersted)FY Magnetic Field on Y Axis (oersted)FZ Magnetic Field on Z Axis (oersted)GR Natural Gamma Ray (API units)HALC High Res. Near/Array Limestone Porosity Corrected (%)HAZI Hole Azimuth (degrees)HBDC High Res. Bulk Density Correction (g/cm3)HBHK HNGS Borehole Potassium (%)HCFT High Resolution Corrected Far Thermal Counts (cps)HCGR HNGS Computed Gamma Ray (API units)HCNT High Resolution Corrected Near Thermal Counts (cps)HDEB High Res. Enhanced Bulk Density (g/cm3)HDRH High Resolution Density Correction (g/cm3)HFEC High Res. Far Detector Counts (cps)HFK HNGS Formation Potassium (%)HFLC High Res. Near/Far Limestone Porosity Corrected (%)HEGR Environmentally Corrected High Resolution Natural Gamma Ray (API units) HGR High Resolution Natural Gamma Ray (API units)HLCA High Res. Caliper (inHLEF High Res. Long-spaced Photoelectric Effect (barns/e-)HNEC High Res. Near Detector Counts (cps)HNPO High Resolution Enhanced Thermal Nutron Porosity (%)HNRH High Resolution Bulk Density (g/cm3)HPEF High Resolution Photoelectric Effect (barns/e-)HRHO High Resolution Bulk Density (g/cm3)HROM High Res. Corrected Bulk Density (g/cm3)HSGR HNGS Standard (total) Gamma Ray (API units)HSIG High Res. Formation Capture Cross Section (capture units) HSTO High Res. Computed Standoff (in)HTHO HNGS Thorium (ppm)HTNP High Resolution Thermal Neutron Porosity (%)HURA HNGS Uranium (ppm)IDPH Phasor Deep Induction (ohmm)IIR Iron Indicator Ratio [CFE/(CCA+CSI)]ILD Deep Resistivity (ohmm)ILM Medium Resistivity (ohmm)IMPH Phasor Medium Induction (ohmm)ITT Integrated Transit Time (s)LCAL HLDS Caliper (in)LIR Lithology Indicator Ratio [CSI/(CCA+CSI)]LLD Laterolog Deep (ohmm)LLS Laterolog Shallow (ohmm)LTT1 Transit Time (10'; microsec)LTT2 Transit Time (8'; microsec)LTT3 Transit Time (12'; microsec)LTT4 Transit Time (10'; microsec)MAGB Earth's Magnetic Field (nTes)MAGC Earth Conductivity (ppm)MAGS Magnetic Susceptibility (ppm)MEDIAN Median Delta-T Recomputed (microsec/ft)MEAN Mean Delta-T Recomputed (microsec/ft)NATN Near Pseudo-Attenuation (db/m)NMST Magnetometer Temperature (degC)NMSV Magnetometer Signal Level (V)NPHI Neutron Porosity (%)NRHB LDS Bulk Density (g/cm3)P1AZ Pad 1 Azimuth (degrees)PEF Photoelectric Effect (barns/e-)PEFL LDS Long-spaced Photoelectric Effect (barns/e-)PIR Porosity Indicator Ratio [CHY/(CCA+CSI)]POTA Potassium (%)RB Pad 1 Relative Bearing (degrees)RHL LDS Long-spaced Bulk Density (g/cm3)RHOB Bulk Density (g/cm3)RHOM HLDS Corrected Bulk Density (g/cm3)RMGS Low Resolution Susceptibility (ppm)SFLU Spherically Focused Log (ohmm)SGR Total Gamma Ray (API units)SIGF APS Formation Capture Cross Section (capture units)SP Spontaneous Potential (mV)STOF APS Computed Standoff (in)SURT Receiver Coil Temperature (degC)SVEL Shear Velocity (km/s)SXRT NMRS differential Temperature (degC)TENS Tension (lb)THOR Thorium (ppm)TNRA Thermal Neutron RatioTT1 Transit Time (10' spacing; microsec)TT2 Transit Time (8' spacing; microsec)TT3 Transit Time (12' spacing; microsec)TT4 Transit Time (10' spacing; microsec)URAN Uranium (ppm)V4P Compressional Velocity, from DT4P (P&S; km/s)V4S Shear Velocity, from DT4S (P&S; km/s)VELP Compressional Velocity (processed from waveforms; km/s)VELS Shear Velocity (processed from waveforms; km/s)VP1 Compressional Velocity, from DT, DTLN, or MEAN (km/s)VP2 Compressional Velocity, from DTL, DTLF, or MEDIAN (km/s)VCO Compressional Velocity, from DTCO (km/s)VS Shear Velocity, from DTSM (km/s)VST Stonely Velocity, from DTST km/s)VS1 Shear Velocity, from DT1 (Lower Dipole; km/s)VS2 Shear Velocity, from DT2 (Upper Dipole; km/s)VRP Compressional Velocity, from DTRP (Receiver Array, P&S; km/s) VRS Shear Velocity, from DTRS (Receiver Array, P&S; km/s)VS1R Shear Velocity, from DT1R (Receiver Array, Lower Dipole; km/s) VS2R Shear Velocity, from DT2R (Receiver Array, Upper Dipole; km/s) VS1T Shear Velocity, from DT1T (Transmitter Array, Lower Dipole; km/s) VS2T Shear Velocity, from DT2T (Transmitter Array, Upper Dipole; km/s) VTP Compressional Velocity, from DTTP (Transmitter Array, P&S; km/s) VTS Shear Velocity, from DTTS (Transmitter Array, P&S; km/s)#POINTS Number of Transmitter-Receiver Pairs Used in Sonic Processing W1NG NGT Window 1 counts (cps)W2NG NGT Window 2 counts (cps)W3NG NGT Window 3 counts (cps)W4NG NGT Window 4 counts (cps)W5NG NGT Window 5 counts (cps)OCEAN DRILLING PROGRAMACRONYMS AND UNITS USED FOR LWD SCHLUMBERGER LOGSAT1F Attenuation Resistivity (1 ft resolution; ohmm)AT3F Attenuation Resistivity (3 ft resolution; ohmm)AT4F Attenuation Resistivity (4 ft resolution; ohmm)AT5F Attenuation Resistivity (5 ft resolution; ohmm)ATR Attenuation Resistivity (deep; ohmm)BFV Bound Fluid Volume (%)B1TM RAB Shallow Resistivity Time after Bit (s)B2TM RAB Medium Resistivity Time after Bit (s)B3TM RAB Deep Resistivity Time after Bit (s)BDAV Deep Resistivity Average (ohmm)BMAV Medium Resistivity Average (ohmm)BSAV Shallow Resistivity Average (ohmm)CGR Computed (Th+K) Gamma Ray (API units)DCAL Differential Caliper (in)DROR Correction for CDN rotational density (g/cm3).DRRT Correction for ADN rotational density (g/cm3).DTAB AND or CDN Density Time after Bit (hr)FFV Free Fluid Volume (%)GR Gamma Ray (API Units)GR7 Sum Gamma Ray Windows GRW7+GRW8+GRW9-Equivalent to Wireline NGT window 5 (cps) GRW3 Gamma Ray Window 3 counts (cps)-Equivalent to Wireline NGT window 1GRW4 Gamma Ray Window 4 counts (cps)-Equivalent to Wireline NGT window 2GRW5 Gamma Ray Window 5 counts (cps)-Equivalent to Wireline NGT window 3GRW6 Gamma Ray Window 6 counts (cps)-Equivalent to Wireline NGT window 4GRW7 Gamma Ray Window 7 counts (cps)GRW8 Gamma Ray Window 8 counts (cps)GRW9 Gamma Ray Window 9 counts (cps)GTIM CDR Gamma Ray Time after Bit (s)GRTK RAB Gamma Ray Time after Bit (s)HEF1 Far He Bank 1 counts (cps)HEF2 Far He Bank 2 counts (cps)HEF3 Far He Bank 3 counts (cps)HEF4 Far He Bank 4 counts (cps)HEN1 Near He Bank 1 counts (cps)HEN2 Near He Bank 2 counts (cps)HEN3 Near He Bank 3 counts (cps)HEN4 Near He Bank 4 counts (cps)MRP Magnetic Resonance PorosityNTAB ADN or CDN Neutron Time after Bit (hr)PEF Photoelectric Effect (barns/e-)POTA Potassium (%) ROPE Rate of Penetration (ft/hr)PS1F Phase Shift Resistivity (1 ft resolution; ohmm)PS2F Phase Shift Resistivity (2 ft resolution; ohmm)PS3F Phase Shift Resistivity (3 ft resolution; ohmm)PS5F Phase Shift Resistivity (5 ft resolution; ohmm)PSR Phase Shift Resistivity (shallow; ohmm)RBIT Bit Resistivity (ohmm)RBTM RAB Resistivity Time After Bit (s)RING Ring Resistivity (ohmm)ROMT Max. Density Total (g/cm3) from rotational processing ROP Rate of Penetration (m/hr)ROP1 Rate of Penetration, average over last 1 ft (m/hr).ROP5 Rate of Penetration, average over last 5 ft (m/hr)ROPE Rate of Penetration, averaged over last 5 ft (ft/hr)RPM RAB Tool Rotation Speed (rpm)RTIM CDR or RAB Resistivity Time after Bit (hr)SGR Total Gamma Ray (API units)T2 T2 Distribution (%)T2LM T2 Logarithmic Mean (ms)THOR Thorium (ppm)TNPH Thermal Neutron Porosity (%)TNRA Thermal RatioURAN Uranium (ppm)OCEAN DRILLING PROGRAMADDITIONAL ACRONYMS AND UNITS(PROCESSED LOGS FROM GEOCHEMICAL TOOL STRING)AL2O3 Computed Al2O3 (dry weight %)AL2O3MIN Computed Al2O3 Standard Deviation (dry weight %) AL2O3MAX Computed Al2O3 Standard Deviation (dry weight %) CAO Computed CaO (dry weight %)CAOMIN Computed CaO Standard Deviation (dry weight %) CAOMAX Computed CaO Standard Deviation (dry weight %) CACO3 Computed CaCO3 (dry weight %)CACO3MIN Computed CaCO3 Standard Deviation (dry weight %) CACO3MAX Computed CaCO3 Standard Deviation (dry weight %) CCA Calcium Yield (decimal fraction)CCHL Chlorine Yield (decimal fraction)CFE Iron Yield (decimal fraction)CGD Gadolinium Yield (decimal fraction)CHY Hydrogen Yield (decimal fraction)CK Potassium Yield (decimal fraction)CSI Silicon Yield (decimal fraction)CSIG Capture Cross Section (capture units)CSUL Sulfur Yield (decimal fraction)CTB Background Yield (decimal fraction)CTI Titanium Yield (decimal fraction)FACT Quality Control CurveFEO Computed FeO (dry weight %)FEOMIN Computed FeO Standard Deviation (dry weight %) FEOMAX Computed FeO Standard Deviation (dry weight %) FEO* Computed FeO* (dry weight %)FEO*MIN Computed FeO* Standard Deviation (dry weight %) FEO*MAX Computed FeO* Standard Deviation (dry weight %) FE2O3 Computed Fe2O3 (dry weight %)FE2O3MIN Computed Fe2O3 Standard Deviation (dry weight %) FE2O3MAX Computed Fe2O3 Standard Deviation (dry weight %) GD Computed Gadolinium (dry weight %)GDMIN Computed Gadolinium Standard Deviation (dry weight %) GDMAX Computed Gadolinium Standard Deviation (dry weight %) K2O Computed K2O (dry weight %)K2OMIN Computed K2O Standard Deviation (dry weight %)K2OMAX Computed K2O Standard Deviation (dry weight %) MGO Computed MgO (dry weight %)MGOMIN Computed MgO Standard Deviation (dry weight %) MGOMAX Computed MgO Standard Deviation (dry weight %)S Computed Sulfur (dry weight %)SMIN Computed Sulfur Standard Deviation (dry weight %) SMAX Computed Sulfur Standard Deviation (dry weight %)SIO2 Computed SiO2 (dry weight %)SIO2MIN Computed SiO2 Standard Deviation (dry weight %) SIO2MAX Computed SiO2 Standard Deviation (dry weight %) THORMIN Computed Thorium Standard Deviation (ppm) THORMAX Computed Thorium Standard Deviation (ppm)TIO2 Computed TiO2 (dry weight %)TIO2MIN Computed TiO2 Standard Deviation (dry weight %) TIO2MAX Computed TiO2 Standard Deviation (dry weight %) URANMIN Computed Uranium Standard Deviation (ppm) URANMAX Computed Uranium Standard Deviation (ppm) VARCA Variable CaCO3/CaO calcium carbonate/oxide factor。
原位直剪试验测试强风化岩体强度参数的数值模拟
原位直剪试验测试强风化岩体强度参数的数值模拟唐雪峰1,2(1.福建省地质工程勘察院福建福州350002;2.中国地质大学(北京)北京100083)[摘要]简述了某强风化岩的原位直剪试验,并采用数值模拟手段对试验进行模拟还原。
结果表明,模拟得到的土体强度参数与试验值较为接近,在一定程度上证明了数值计算方法的准确性。
而后对试样的应力变形特性进行了分析,试样剪应力云图大体呈现工字型分布,也即试样两端的剪应力较大,而中部的剪应力相对较小,试样在约束刚度较大的位置(如靠近铁质剪切盒)或具有一定凹角的接触面上(如剪切盒的边角处)存在明显的应力集中现象。
通过数值模拟计算,一方面可以更为全面地展示原位直剪试验结果,揭示在试验中所无法获取的信息,另一方面,模拟结论也能够跟试验成果互为佐证,以便将其可靠地推广应用到滑坡的防治研究中。
[关键词]原位直剪试验;强风化岩体;数值模拟;应力变形特性Numerical simulation of in -situ direct shear test on the strength parameters of strong -weathered rockAbstract :The in -situ direct shear test of a strongly weathered rock is briefly described ,and the tests are reproduced by means of numeri-cal simulation.The results show that the simulated strength parameters are close to the test values ,which proves the accuracy of the numer-ical method to some extent.Then the stress and deformation characteristics of the specimen were analyzed ,the shear stress exhibits an"H"pattern ,that is ,the shear stress at the ends of the specimen is larger ,and shear stress in the central part of the specimen is relatively smal-ler.Obvious stress concentration can be observed where the constraint stiffness is larger (such as near the iron box )or near the contact sur-face with a concave angle.Through numerical simulation ,on the one hand ,the direct shear test can be displayed more comprehensively so as to reveal the information that cannot be obtained in the test ;on the other hand ,the simulation results can also be mutually confirmed with the test results ,which helps to apply them to the research of landslide control more reliably.Key words :field direct shear tests ,strong -weathered rock ,numerical simulation ,stress and deformation properties 基金项目:福建省科技重大专项(2016YZ0002-1),福建省科技创新平台建设(2014Y2007)作者简介:唐雪峰(1987-),女,福建莆田人,硕士,工程师,主要从事岩土工程勘察设计工作。
Geomechanics Aspects of Multiple
M.Y. Soliman, Loyd East, and David Adams, Halliburton Energy Services
Summary
z = h − 2 ͑H − v͒. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (3)
For H<v,
r = pi, . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (4)
pb = 3H − v . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . (8)
It has been observed in the laboratory (Soliman 1990; El Rabaa 1989) that Hubert and Willis’ failure criterion underestimates the breakdown pressure for a transverse fracture. This is because this failure criterion assumes the creation of an axial fracture because of a tensile failure of the rock. This criterion is valid for a vertical well or a horizontal well where the fracture is longitudinal. However, it does not fit the situation where the fracture is transverse.
机械翻译词汇
CheckBox1金属切削metal cutting 机床machine tool 金属工艺学technology of metals刀具cutter摩擦friction 联结link传动drive/transmission 轴shaft弹性elasticity频率特性frequency characteristic误差error 响应response定位allocation 机床夹具jig动力学dynamic 运动学kinematic静力学static 分析力学analyse mechanics拉伸pulling压缩hitting剪切shear 扭转twist弯曲应力bending stress 强度intensity三相交流电three-phase AC 磁路magnetic circles变压器transformer 异步电动机asynchronous motor几何形状geometrical 精度precision正弦形的sinusoid交流电路AC circuit机械加工余量machining allowance 变形力deforming force变形deformation应力stress硬度rigidity热处理heat treatment退火anneal正火normalizing脱碳decarburization 渗碳carburization电路circuit 半导体元件semiconductor element反馈feedback发生器generator直流电源DC electrical source 门电路gate circuit逻辑代数logic algebra外圆磨削external grinding内圆磨削internal grinding 面磨削plane grinding变速箱gearbox 离合器clutch绞孔fraising 绞刀reamer螺纹加工thread processing螺钉screw铣削mill 铣刀milling cutter功率power 工件workpiece齿轮加工gear mechining 齿轮gear主运动main movement 主运动方向direction of main movement 进给方向direction of feed 进给运动feed movement合成进给运动resultant movement of feed 合成切削运动resultant movement of cutting 合成切削运动方向direction of resultant movement of cutting切削深度cutting depth前刀面rake face刀尖nose of tool前角rake angle后角clearance angle 龙门刨削planing主轴spindle 主轴箱headstock卡盘chuck 加工中心machining center车刀lathe tool车床lathe钻削镗削bore车削turning磨床grinder 基准benchmark钳工locksmith锻forge压模stamping焊weld拉床broaching machine 拉孔broaching装配assembling 铸造found流体动力学fluid dynamics流体力学fluid mechanics加工machining 液压hydraulic pressure切线tangent 气压air pressure pneumatic pressure机电一体化mechanotronics mechanical-electrical integration稳定性stability 介质medium液压驱动泵fluid clutch 液压泵hydraulic pump阀门valve 失效invalidation强度intensity 载荷load应力stress 安全系数safty factor可靠性reliability 螺纹thread螺旋helix键spline销pin 滚动轴承rolling bearing滑动轴承sliding bearing 弹簧spring制动器arrester brake 十字结联轴节crosshead联轴器coupling 链chain皮带strap 精加工finish machining粗加工rough machining 变速箱体gearbox casing腐蚀rust 氧化oxidation磨损wear 耐用度durability随机信号random signal 离散信号discrete signal超声传感器ultrasonic sensor 集成电路integrate circuit挡板orifice plate 残余应力residual stress套筒sleeve 扭力torsion冷加工cold machining 电动机electromotor汽缸cylinder 过盈配合interference fit热加工hotwork 摄像头CCD camera倒角rounding chamfer 优化设计optimal design工业造型设计industrial moulding design 有限元finite element滚齿hobbing 插齿gear shaping伺服电机actuating motor铣床milling machine钻床drill machine 镗床boring machine步进电机stepper motor 丝杠screw rod导轨lead rail 组件subassembly可编程序逻辑控制器Programmable Logic Controller PLC 电火花加工electric spark machinin g电火花线切割加工electrical discharge wire - cutting相图phase diagram热处理heat treatment 固态相变solid state phase changes有色金属nonferrous metal 陶瓷ceramics合成纤维synthetic fibre 电化学腐蚀electrochemical corrosion车架automotive chassis悬架suspension转向器redirector变速器speed changer板料冲压sheet metal parts孔加工spot facing machining车间workshop 工程技术人员engineer气动夹紧pneuma lock 数学模型mathematical model画法几何descriptive geometry机械制图Mechanical drawing投影projection 视图view剖视图profile chart 标准件standard component零件图part drawing装配图assembly drawing尺寸标注size marking 技术要求technical requirements刚度rigidity 内力internal force位移displacement 截面section疲劳极限fatigue limit断裂fracture塑性变形plastic distortion脆性材料brittleness material刚度准则rigidity criterion 垫圈washer垫片spacer 直齿圆柱齿轮straight toothed spur gear斜齿圆柱齿轮helical-spur gear 直齿锥齿轮straight bevel gear运动简图kinematic sketch齿轮齿条pinion and rack蜗杆蜗轮worm and worm gear虚约束passive constraint曲柄crank 摇杆racker凸轮cams 共轭曲线conjugate curve范成法generation method 定义域definitional domain值域range 导数\\微分differential coefficient求导derivation定积分definite integral不定积分indefinite integral 曲率curvature偏微分partial differential 毛坯rough游标卡尺slide caliper 千分尺micrometer calipers攻丝tap 二阶行列式second order determinant逆矩阵inverse matrix 线性方程组linear equations概率probability 随机变量random variable排列组合permutation and combination 气体状态方程equation of state of gas动能kinetic energy 势能potential energy机械能守恒conservation of mechanical energy 动量momentum桁架truss 轴线axes余子式cofactor 逻辑电路logic circuit触发器flip-flop脉冲波形pulse shape数模digital analogy 液压传动机构fluid drive mechanism机械零件mechanical parts 淬火冷却quench淬火hardening 回火tempering调质hardening and tempering 磨粒abrasive grain结合剂bonding agent砂轮grinding wheel卷板机Bending Machine坡口机Groove Machine型钢电动煨弯机Bending steel electrical machine硅整流焊机Silicon welder直流弧焊机DC arc welding machines半自动切割机Semi-automatic cutting machine远红外线烘干箱Far infrared drying box焊条保温筒Insulation cylinder electrode电动角向磨光机Electrical angle Angle grinder手电钻Hand electro drill碳弧气刨Carbon arc gouging喷砂设备Sandblasting equipment空气压缩机(电动)Air Compressor (electric)液压顶升系统Hydraulic jacking system试压用水泵Pump pressure test内工胀专用装置Expansion work at specialized devicesX光射线探伤机X-ray detection machine测厚仪Thickness Gauge电气、仪表调试仪器Electrical and instrument equipment debugging经纬仪Theodolite水准仪water level水准仪water level铟钢尺Indium steel ruler钢卷尺Steel Tape对讲机Walkie-talkie继电保护 relay protectionaccess arm 磁头臂,存取臂octet 八位位组,八位字节information 信息access time 存取时间operator 操作员inline processing 内处理adder 加法器optical character reader 光符阅读机input 输入address 地址optical scanner 光扫描器inquiry 询问alphanumeric 字母数字的output 输出instruction 指令analog computer 模拟计算机overflow 溢出,上溢integrated circuit 集成电路analyst 分析员panel 平板to interpret 解释area 区域parameter 参数,参量item 项目,项array 数组,阵列perforator 穿孔机jump 转移assembler 汇编程序peripheral equipment 外围设备,外部设备key 键,关键码automation 自动化personal computer 个人计算机keyboard 键盘band 区printed circuit 印制电路latency time 等待时间batch processing 成批处理printer 打印机library 库,程序库binary code 二进制码printout 打印输出linkage 连接binary digit 二进制位,二进制数字to process 处理to load 装入,寄存,写入,加载bit 比特,二进制的一位processing unit 处理部件location 存储单元branch 分支,支线program 程序logger 登记器,记录器brush 电刷to program 程序编制loop 循环buffer storage 缓冲存储器programmer 程序设计员machine language 机器语言calculator 计算器programming 程序设计,程序编制magnetic storage 磁存储器pulse 脉冲ma gnetic tape 磁带card punch 卡片穿孔机punch 穿孔matrix 矩阵card reader 卡片阅读机,读卡机to punch 穿孔memory 存储器cell 单元punched card, punch card 穿孔卡片message 信息,报文channel 通道,信道punched tape, punch tape 穿孔纸带microcomputer 微型计算机character 字符punch hole 孔,穿孔module 组件,模块check digit 校验数位random access 随机存取monitor 监视器,监督程序,管程circuit 电路,线路to read 读nanosecond 毫微秒to clear 清除,清零reader 阅读程序network 网络,网clock 时钟reading 阅读numeric, numerical 数字的,数值的code 代码real time 实时simulator 模拟器,模拟程序to code 编码record, register 记录software 软件,软设备coder 编码员,编码器redundancy 冗余sort 分类,排序command 指令,命令routine 例行程序sorter 分类人员,分类机,分类程序,排序程序compiler 编译程序selector 选择器,选择符storage 存储器computer language 计算机语言sentinel 标记time sharing 分时console 控制台sequence 序列,顺序timing 定时control unit 控制部件,控制器sequential 顺序的track 磁道core storage, core store 磁心存储器serial 串行的.连续的transducer 传感器,翻译机counter 计数器shift 移位,移数translator 翻译程序,翻译器cybernetics 控制论signal 信号to update 更新cycle 循环simulation 模拟Winchester disk drive 温彻斯特磁盘机,硬盘机data 数据to store 存储working storage 工作存储器data processing 数据处理subroutine, subprogram 子程序debugging 调试switch 开关teleprinter 电传打字机decision 制定symbol 符号terminal 终端digit 数字,数位,位symbolic language 符号语言terminal unit 终端设备digital computer 数字计算机system 系统timer 时钟,精密计时器disc, disk 磁盘tabulator 制表机frame 帧display unit 显示装置feedback 反馈hardware 硬件drum 磁鼓field 字段,信息组,域identifier 标识符to edit 编辑file 文件index 索引electronics 电子学floppy disk 软磁盘to erase 擦除,清洗,抹除emitter 发射器floppy disk drive 软磁盘机feed 馈送,供给to encode 编码flow chart 流程图to feed 馈送,供给3--Jaws indexing spacers 三爪、分割工具头A.T.C.system 加工中心机刀库Aluminum continuous melting & holding furnaces 连续溶解保温炉Balancing equipment 平衡设备Bayonet 卡口Bearing fittings 轴承配件Bearing processing equipment 轴承加工机Bearings 轴承Belt drive 带传动Bending machines 弯曲机Blades 刀片Blades,saw 锯片Bolts,screws & nuts 螺栓,螺帽及螺丝Boring heads 搪孔头Boring machines 镗床Cable making tools 造线机Casting,aluminium 铸铝Casting,copper 铸铜Casting,gray iron 铸灰口铁Casting,malleable iron 可锻铸铁Casting,other 其他铸造Casting,steel 铸钢Chain drive 链传动Chain making tools 造链机Chamfer machines 倒角机Chucks 夹盘Clamping/holding systems 夹具/支持系统CNC bending presses 电脑数控弯折机CNC boring machines 电脑数控镗床CNC drilling machines 电脑数控钻床CNC EDM wire-cutting machines 电脑数控电火花线切削机CNC electric discharge machines 电脑数控电火花机CNC engraving machines 电脑数控雕刻机CNC grinding machines 电脑数控磨床CNC lathes 电脑数控车床CNC machine tool fittings 电脑数控机床配件CNC milling machines 电脑数控铣床CNC shearing machines 电脑数控剪切机CNC toolings CNC刀杆CNC wire-cutting machines 电脑数控线切削机Conveying chains 输送链Coolers 冷却机Coupling 联轴器Crimping tools 卷边工具Cutters 刀具Cutting-off machines 切断机Diamond cutters 钻石刀具Dicing saws 晶圆切割机Die casting dies 压铸冲模Die casting machines 压铸机Dies-progressive 连续冲模Disposable toolholder bits 舍弃式刀头Drawing machines 拔丝机Drilling machines 钻床Drilling machines bench 钻床工作台Drilling machines,high-speed 高速钻床Drilling machines,multi-spindle 多轴钻床Drilling machines,radial 摇臂钻床Drilling machines,vertical 立式钻床drills 钻头Electric discharge machines(EDM) 电火花机Electric power tools 电动刀具Engraving machines 雕刻机Engraving machines,laser 激光雕刻机Etching machines 蚀刻机Finishing machines 修整机Fixture 夹具Forging dies 锻模Forging,aluminium 锻铝Forging,cold 冷锻Forging,copper 铜锻Forging,other 其他锻造Forging,steel 钢锻Foundry equipment 铸造设备Gear cutting machines 齿轮切削机Gears 齿轮Gravity casting machines 重力铸造机Grinder bench 磨床工作台Grinders,thread 螺纹磨床Grinders,tools & cutters 工具磨床Grinders,ultrasonic 超声波打磨机Grinding machines 磨床Grinding machines,centerless 无心磨床Grinding machines,cylindrical 外圆磨床Grinding machines,universal 万能磨床Grinding tools 磨削工具Grinding wheels 磨轮Hand tools 手工具Hard/soft and free expansion sheet making plant 硬(软)板(片)材及自由发泡板机组Heat preserving furnaces 保温炉Heating treatment funaces 熔热处理炉Honing machines 搪磨机Hydraulic components 液压元件Hydraulic power tools 液压工具Hydraulic power units 液压动力元件Hydraulic rotary cylinders 液压回转缸Jigs 钻模Lapping machines 精研机Lapping machines,centerless 无心精研机Laser cutting 激光切割Laser cutting for SMT stensil 激光钢板切割机Lathe bench 车床工作台Lathes,automatic 自动车床Lathes,heavy-duty 重型车床Lathes,high-speed 高速车床Lathes,turret 六角车床Lathes,vertical 立式车床Lubricants 润滑液Lubrication Systems 润滑系统Lubricators 注油机Machining centers,general 通用加工中心Machining centers,horizontal 卧式加工中心Machining centers,horizontal & vertical 卧式及立式加工中心Machining centers,vertical 立式加工中心Machining centers,vertical double-column type 立式双柱加工中心Magnetic tools 磁性工具Manifolds 集合管Milling heads 铣头Milling machines 铣床Milling machines,bed type 床身式铣床Milling machines,duplicating 仿形铣床Milling machines,horizontal 卧式铣床Milling machines,turret vertical 六角立式铣床Milling machines,universal 万能铣床Milling machines,vertical 立式铣床Milling machines,vertical & horizontal 立式及卧式铣床Mold & die components 模具单元Mold changing systems 换模系统Mold core 模芯Mold heaters/chillers 模具加热器/冷却器Mold polishing/texturing 模具打磨/磨纹Mold repair 模具维修Molds 模具Nail making machines 造钉机Oil coolers 油冷却器Overflow cutting machines for aluminium wheels 铝轮冒口切断机P type PVC waterproof rolled sheet making plant P型PVC高分子防水PCB fine piecing systems 印刷电器板油压冲孔脱料系统Pipe & tube making machines 管筒制造机Planing machines 刨床Planing machines vertical 立式刨床Pneumatic hydraulic clamps 气油压虎钳Pneumatic power tools 气动工具Powder metallurgic forming machines 粉末冶金成型机Presses,cold forging 冷锻冲压机presses,crank 曲柄压力机Presses,eccentric 离心压力机Presses,forging 锻压机Presses,hydraulic 液压冲床Presses,knuckle joint 肘杆式压力机Presses,pneumatic 气动冲床Presses,servo 伺服冲床Presses,transfer 自动压力机Pressing dies 压模Punch formers 冲子研磨器Quick die change systems 速换模系统Quick mold change systems 快速换模系统Reverberatory furnaces 反射炉Rollers 滚筒Rolling machines 辗压机Rotary tables 转台Sawing machines 锯床Sawing machines,band 带锯床Saws,band 带锯Saws,hack 弓锯Saws,horizontal band 卧式带锯Saws,vertical band 立式带锯shafts 轴Shapers 牛头刨床Shearing machines 剪切机Sheet metal forming machines 金属板成型机Sheet metal working machines 金属板加工机Slotting machines 插床spindles 主轴Stamping parts 冲压机Straightening machines 矫直机Switches & buttons 开关及按钮Tapping machines 攻螺丝机Transmitted chains 传动链Tube bending machines 弯管机Vertical hydraulic broaching machine 立式油压拉床Vises 虎钳Vises,tool-maker 精密平口钳Wheel dressers 砂轮修整器Woven-Cutting machines 织麦激光切割机Wrenches 扳手。
平板计算公式
Chapter 6Design FormulasStress FormulasStrength of MaterialsBeam Formulas, Bending Moments Properties of Sections, Moments of Inertia Flat Plate FormulasDesigning for Equal Stiffness Designing for Impact Resistance Designing for Thermal StressWhether you are designing in metals or plastics, it is necessary to choose the specific structural property values for use in stan-dard design equations. With metals, such property values are relatively constant over a wide range of temperatures and time. But for plastics, the appropriate values are dependent on temperature, stress level, and life expectancy of the part.As far as design practices are involved, the principles defined in many good engi-neering handbooks are applicable. However, the nature of high polymer materials requires even more attention to appropriate safety factors.The information and formulas provided in this chapter can help you solve many of the design problems commonly met in the structural design of plastic parts. However, it is important that designers and design engineers understand that the formulas and the data expressed in this brochure are given only as guides. They may not be pertinent to the design of a particular part, with its own special require-ments and end-use environments. Generally, the symbols used in this man-ual’s various figures, formulas, and text have the definitions shown in the boxed column on this page.Our customers can expect efficient design assistance and aid from the technical sup-port services at Dow Plastics. We invite you to discuss your needs with us.Above all, there is an aspect of profes-sional and competent design engineering that holds true throughout. That is the fact that, after all the science, mathematics, and experience have been properly used in “solving” the design needs of a part, it is strongly recommended that prototype parts be produced and thoroughly tested in the expected end-use conditions and environ-ments before committing the design tofull-scale production.Partial list of engineering symbols and letters used, and meanings.=AngleA=Area . . . cross-sectional␣=Coefficient of linear thermal expansion y=Deflection of cantilever; height ofundercut=DensityD=DiameterMD=Diameter, majorPD=Diameter, pitchc=Distance from neutral axis to outerfiber, centroidz=Distance from q to neutral axisP=Force . . . P = deflection force=Friction, coefficienta,b,h,t=Height or thicknessI=Inertia, moment of (neutral axis)=Length⌬ =Length, changeE=Modulus (Young’s)q=Point within a beam or internalpressureR=Radiusr=RadiusEs=Secant modulusM=Sectional bending momentτ=Shear stress=Strain=StressTCF=Thickness conversion factorT=Temperature⌬T=Temperature, changev=Poisson’s ratio=Velocity, constant angular,radius/secondbo=Width at basea=Width . . . wall thicknessStress FormulasTensile or Compressive StressTensile or compressive stress is the force carried per unit of area and is expressed by the equation: = P = PA a b Where:=stress P =forceA =cross-sectional area a =width b=heightThe force (P) produces stresses normal (i.e., perpendicular) to the cross section of the part. If the stress tends to lengthen the part, it is called tensile stress. If the stress tends to shorten the part, it is called com-pressive stress. (For compression loading,the part should be relatively short, or it must be constrained against lateral bucking.)StrainStrain is the ratio of the change in the part’s length, over the original length. It is expressed as the percentage of change in length, or percent elongation.In direct tension and compression loading,the force is assumed to act along a line through the center of gravity of members having uniform cross-sections, called centroids.Within the elastic limits of the materials,design formulas developed for metals can also be applied to plastics. Stress levels are determined only by load and part geometry,so standard equations can be used. Deflec-tion is determined by two other material property values: the elastic, or Young’s modulus (E); and Poisson’s ratio (v). Since the modulus of a plastic material varies with temperature and duration of the stress, this modulus may need replacement in deflec-tion equations by the appropriate creep modulus. It may be helpful to review vari-ous sections of Chapter 4 for assistance in choosing modulus values appropriate to the specific stress level, temperature, and design life of the part.Poisson’s ratio varies with temperature,strain level, and strain rate. These differ-ences are too small to significantly affect a calculation. For example, Poisson’s ratio at room temperature for CALIBRE polycarbon-ate resin is 0.37, and it ranges from 0.35 to 0.40 over the operational temperature range.By selecting the correct modulus and assum-ing the value of Poisson’s ratio to be constant,standard equations can be used to design a part for fabrication in thermoplastics.Stress Acting at an AngleThe standard stress equation is valid when the cross-section being considered isperpendicular to the force. However, when the cross-section is at an angle other than 90° to the force, as shown in Figure 57, the equation must be adapted. These stresses are always less than the standard case, i.e.,maximum normal stress occurs when = 0.Shear StressIn addition to the normal stress calculated in the previous section, a plane at an angle to the force has a shear stress component.Here, unlike tensile and compressive stress,the force produces stress in the plane of the cross-section, i.e., the shear stresses are perpendicular to tensile or compressive stresses. The equations for calculating planar shear stress, based on Figure 58 are:τ = P sin cos AMax =P2A (when = 45° or 135°)Torsional StressWhen a stress acts to twist a component, it produces torsional stress. If a solid circular shaft, or shaft-like component, is subject to a twisting moment, or torsion, the resulting shear stress (q) is calculated by:G rwhere:q = shear stressG = modulus of rigidity(see Chapter 4, page 35)= angle of twist, in radians r = radius of shaft = length of shaftThe torque (T) carried by the shaft is given byG where I P is the polar second moment of d 432A useful rearrangement of the formula isT GI PFigure 57 – Diagram of Stress Acting at an Angle Figure 58 – Representation of Shear Stressq =T = I Parea = =Strength of MaterialsBeamsWhen a straight beam of uniform cross-sectional area is subjected to a perpendicular load, the beam bends. If shear is negligible, the vertical deflection is largely due to bend-ing. Fibers on the convex side of the beam lengthen, and fibers on the concave side compress.There is a neutral surface within any beam that contains the centroids of all sections and is perpendicular to the plane of the load for such deflections. In a uniform, symmetri-cal beam, the neutral axis of the beam is the horizontal, central axis. Tensile or compres-sive stress and strain on the neutral axis are essentially zero. At all other points within the beam, the stress is a tensile stress if the point lies between the neutral axis and convex surfaces of the beam, and is a compressive stress if the point lies between the neutral axis and concave surfaces of the beam, see Figure 59.The fiber stress for any point (q) within the beam is calculated using the equation: = MzIwhere:M =bending moment of the section containing q (values can be taken from the appro-priate beam formula, Figures 60 to 68).z =the distance from q to the neutral axisI =the moment of inertia with respect to theneutral axis (values can be taken fromthe appropriate cross-sectional areaformula, Figures 69 to 91).The maximum fiber stress in any section occurs at the points farthest from the neu-tral surface and at the section of greatest bending moment, i.e., when z = Max z, and M = Max M. Maximum fiber stress is given by the equation:Max = McIwhere:c =the distance from the neutral axis to theextreme outermost fiber.Such equations are valid if:•The beam is of homogeneous material,so that it has the same modulus ofelasticity in tension and compression.•Plane sections remain planar.If several loads are applied at the same time,the total stress and deflection at any pointare found by superimposition. Compute thestress and deflection for each load actingon the point, and add them together. Figure 59 – Bending of a BeamFigure 60 – Cantilever Beam, concen-trated load at free endBeam Formulas, Bending MomentsFigure 63 – Simple Beam, concentrated load off centerFigure 61 – Cantilever Beam, uniformload, w per unit length, total load W Figure 62 – Simple Beam, concentrated load at centerFigure 64 – Simple Beam, two equal, concentrated loads, symmetrically placed Figure 66 – Beam fixed at both ends, concentrated load at centerFigure 67 – Beam fixed at both ends, concentrated load at any pointProperties of Sections, Moments of InertiaFigure 71Figure 74Figure 77Figure 79Figure 81Figure 84Figure 87Figure 89Figure 918384Flat PlatesA flat plate of uniform thickness is used in many designs to support a load perpendicu-lar to the plate. Figures 92 to 95 give stress and deflection equations for several com-mon plate configurations. Again, these equations are valid when working with a homogeneous, isotropic material, and when deflection is less than about one-half of the plate thickness.Where:a=radius of circularplateD=Eh312 ( - 2)flexural rigidityof plateE=apparent modulus of elasticityh=plate thicknessv=Poisson’s ratioq=uniform load perunit area Figure 92 – Rectangular plate, all edges fixed, uniform loadFlat Plate FormulasFigure 94 – Circular plate, fixed edges,uniformly distributed loadThin-Walled TubingFigure 96 and the equations provided can be used to calculate the stress and defor-mation of thin-walled tubing under internal pressure when neither end of the tubing is closed. This also applies to fairly long tubes, or in situations remote from the tube ends. As long as the wall thickness is less than about one-tenth of the radius, the circumfer-ential or hoop stress (2) is practically uni-form throughout the thickness of the wall,and the radial stress (3) is negligible. Asusual, the appropriate time- and tempera-ture-dependent modulus must be calculated for specific applications. Significant error can result if the thin-wall equations are used in calculations that involve thick walls.1=qr2t1 = 0, if longitudinal pressure is zero or isexternally balanced2=qrt⌬r = qrEtSee Figure 96 for definitions.Figure 96 – Thin Walled Tubing8586Thick-Walled Pressure Vessels Equations for design of thin-walled pressure vessels can be used to design thick-walled pressure vessels to be fabricated from thermo-plastics. However, several guidelines need to be considered. First, include generous safety factors in the design to allow for the geometrical differences at the joint of the end-plate and the cylinder. These differ-ences can cause maximum stresses, many times the nominal hoop stress, depending on the plate-to-wall joint design. Also, the ratio of wall thickness to mean radius should not exceed approximately 1:10 to avoid a triaxial stress state – with stresses acting in three directions – which can reduce the ductility of plastics and most other materi-als. And, of course, the modulus must be selected carefully.Remember always that design analysis and calculations cannot take into consideration such factors as weld lines, the effect of gate location, orientation of the polymer, or vari-ations in polymer density. Therefore, the design should always be verified by fabricat-ing and testing prototypes. For example, a typical pressure vessel evaluation would include fatigue testing (cyclic pressuriza-tion) and hydrostatic burst testing. (For more information on the effect of weld lines and gate location, see page 66.) For the equations appropriate to a specific situation,consult your general engineering handbook.† = 1 x 2(3 + v)R2 +R2 + R2R2– (1 + 3v)r28 386.4r2Rotating DisksBecause of their high strength-to-weight ratio, dimensional stability, resistance to creep and relaxation, and their impact strength, engineering thermoplastics are excellent materials for rotating disks, such as impellers.The total stress on an impeller is calculated by adding:•Bending stresses due to the pressure differential.•Localized bending stresses due to the attachment of a blade.•Inertial stresses due to high-speed rotation.Make sure that the total stress is within the design limits based on service conditions. Bending stresses are calculated using standard stress and deflection equations. The inertial stresses developed by high-speed rotation can be estimated by using the following flat-disk equations. In all of the equations, v is Poisson’s ratio, which is defined on page 40.Rotating Disk EquationsA. For a solid, homogeneous, circular diskof uniform thickness, having radius R(mm) and density r (g/cm3), rotatingabout its centroidal axis with a constant angular velocity, v (rad/sec):1.Radial tensile inertia stress (sr ) at apoint which is distance r from the center, is given as:r = 1 x 2 (3 + v)(R2 - r2)8 386.42.Tangential tensile inertia stress †) isgiven as†= 1 x 2 (3 + v)R2 - (1 + 3v)r28 386.43.Maximum radial and maximumtangential stresses are equal andoccur at the center (r = 0).Max r= Max †= 1 x 2 (3 + v)R28 386.4B.For a homogeneous, annular disk ofuniform thickness with an outer radiusR (mm), a central hole of radius Ro(mm),and density r (g/cm3), rotating about itscentroidal axis with a constant angularvelocity v (rad/sec):1.At any point a distance r from thecenter radial tensile stress (r) isgiven asr= 3 + v x 2 (R2 + R2 - R2R2 - r2)8 386.4 r22.Tangential tensile inertia stress (†)is given as3.Maximum radial stress (Max r)occurs at r = ߛRRand is given asMax r= 3 + v x 2 (R - R2)28 386.44.Maximum tangential stress (Max †)occurs at the perimeter of the holeand is given asMax †= 1 x 2 (3 + v )R2 +(1 - v)R24 386.48788Equivalent ThicknessWhen a thermoplastic is specified asreplacement for another material (a metal,for example) the new part often needs tohave the same stiffness as the old one.Essentially, that means making sure thatthe new part, when subjected to the sameload, will have the same deflection as theold part.Deflection in bending is proportional 1/EI(E = modulus and I = moment of inertia),and I is proportional to t3 (t = thickness).Thus, the equivalent thickness of a plain,flat part to be made from a thermoplasticcan be calculated by the following equation:t2= t1E1E2where:E1=flexural modulus of material beingreplacedE2=flexural modulus or creep modulus ofreplacement thermoplastict1=thickness of old materialt2=required thickness of thermoplasticA thickness conversion factor (TCF) can becalculated on the basis of the cube root ofthe ratio of the moduli of the two materials.Table 17 lists the thickness conversionfactors for several common structuralmaterials relative to steel. These factors arebased on the short-term, room temperaturemodulus values. Conversion factors basedon the long-term and/or high temperaturemodulus (that is, the creep modulus) willbe different from those shown here.For example, to find what thickness of athermoplastic component is required forequal stiffness relative to steel, multiplythe thickness of the steel component bythe conversion factor, TCF, in Table 17:t2= t1x TCFwhere:TCF = E1ES Tand EST= flexural modulus or creepmodulus of steel.To determine the thickness of material (Y)required for a thermoplastic part that willgive the same stiffness as when the part ismade with a material (Z) other than steel,multiply the thickness of the part inmaterial (Z) by the TCF (from Table 17 )for the thermoplastic relative to steel, andthen divide by the TCF for the material(Y) relative to steel.33Designing for Equal StiffnessTable 17 – Thickness Conversion Factors for Common Structural Materials Relative To SteelFlexural Modulus Thickness Replacement S.I.English Metric ConversionMaterial GPa ksi kg/cm2FactorABS 2.6 3.8 x 105 2.7 x 104 4.29Acrylic 3.0 4.4 x 105 3.1 x 104 4.12Aluminum, cast71.0 1.0 x 1077.2 x 105 1.43Brass96.5 1.4 x 1079.9 x 105 1.29Ceramics (A203)344.8 5.0 x 107 3.5 x 1060.84Glass69.0 1.0 x 1077.0 x 105 1.44 PC 2.4 3.5 x 105 2.5 x 104 4.41 PP 1.2 1.7 x 105 1.2 x 104 5.63 PS 3.3 4.8 x 105 3.4 x 104 3.97 Polysulfone 2.5 3.6 x 105 2.6 x 104 4.37 Steel206.9 3.0 x 107 2.1 x 106 1.00 Timber (average of a variety of structural timbers)11.7 1.7 x 106 1.2 x 105 2.60 SAN 3.6 5.2 x 105 3.7 x 104 3.88 Zinc, die cast44.8 6.5 x 106 4.6 x 105 1.6689RibsOccasionally, the calculations for an equiva-lent thickness of a thermoplastic to a plain,flat plate can give results that would be too thick to be economical or practical. As the moment of inertia is proportional to thick-ness cubed, the addition of ribs to a rela-tively thin plate is an effective way to increase the stiffness.Figure 97 shows four cross-sections of equal stiffness. The straight conversion factor for polycarbonate is bulky, uneconom-mical and inappropriate. The use of ribs in the part made with polycarbonate will allow a thinner overall wall thickness. By allowing thinner walls, ribbing also reduces molding cycle time and cross-sectional area, and reduces material usage and product weight without sacrificing physical properties. You may wish to consider other methods of stiffening such as corrugating and doming.Figure 97 – Calculations for Equal Stiffness, Ribbing with Polycarbonate ResinsThe following calculations illustrate both methods of finding equivalent thickness when redesigning in polycarbonate.To calculate the thickness of a part that,when made in polycarbonate, will have the same deflection as a 0.75 mm thick alumi-num part at 73°F (23°C).ing the moduli of the two materials:E 1 = modulus of aluminum at 73°F (23°C)= 7.2 x 104 MPaE 2 = modulus of polycarbonate at 73°F (23°C)= 2.41 x 103 MPa t 1 = 0.75t 2 = ?t 2 = t 1E 1E 2= 0.7571,000 2,410= 2.3 mming the thickness conversion factors from Table 17:TCF AL/ST = TCF for aluminum relative to steel= 1.43TCF PC/ST = TCF for polycarbonate relativeto steel= 4.41TCV PC/AL = TCF for polycarbonate relativeto aluminum= TCV PC/STTCF AL/ST= 4.411.43= 3.08Therefore: t 2 = 0.75 x 3.08= 2.3 mmRemember that stiffness is proportional to thickness cubed (t 3). This means an increase in thickness of only 26% will double part stiffness.3390The impact resistance exhibited by anactual part depends on the design of thepart, the material used, and the conditionsof fabrication.Designing for impact is complex. Theshape and stiffness of the striking body, theshape of the part, the inertia of both, andend-use conditions can all affect impactstrength. The following section gives yougeneral design guidelines for improvingimpact strength. These guidelines comprisea sound approach to the design challenge,but are not a substitute for production ofand testing for prototype parts in the actualconditions of use.Part Design for Impact ResistanceBecause the part must be able to absorb theenergy of impact, part design is probablythe greatest single factor – other thanproper material selection – in determiningimpact strength. Part design will improvethe impact resistance when you take care to:•Provide walls that flex rather thanrigidly resist impact loading.•Use rounded corners so that they cangive with the impact and provide asmoother transfer of energy. (See thediscussion on corner radius in “ProductDesign” page 56.)•Avoid any abrupt changes in stiffness(due to changes in wall thickness orstructural reinforcement), which tend toconcentrate impact loading. This includessuch features as ribs, holes, and machinedareas. (See Chapter 5, page 56 for designguidelines on wall thickness, transitionzones and ribs.)Mold DesignImpact strength can also be improved bygood mold design. In this:•Position gates away from high impactareas. (See page 66 for more informa-tion on gate location.)•Place weld lines, whenever possible,away from high impact areas. (See page66 for more information on weld lines.)•Core-out thick sections to reduce pack-ing stresses and improve flexibility.AssemblyThe method of assembly can also affect apart’s impact strength. Rigid joints cancause abrupt transitions in energy flow,which can break the joint. Joints, like wallsand corners, should be flexible. Assemblytechniques are discussed in Chapter 7.Designing for Impact ResistanceDesigning for Thermal StressThermal expansion and contraction areimportant considerations in plastics design,and are often overlooked. Expansion-contraction problems often arise when twoor more parts made of materials havingdifferent coefficients of thermal expansionare assembled at a temperature other thanthat of the end-use environment. When theassembled parts go into service in the end-useenvironment, the two materials react differ-ently, and the resultant thermal stressescan cause unexpected part failure.So, you must consider the effects of ther-mal expansion and/or contraction early inthe design of parts that involve close fits,molded-in inserts, and mechanical fastenings.Coefficients of thermal expansion for somecommon materials are given in Table 18.Thermal stress can be calculated byusing the following equation:t = (␣1-␣2)E⌬Tor =(␣1-␣2)⌬TWhere:␣1=coefficient of thermal expansion of one material␣2=coefficient of thermal expansion of second materialE=modulus⌬T=change in temperature, °F (°C) =strain, mm/mm=constant (roughly 1.0 for most conditions)The following calculations illustrate the use of thermal stress equations: Calculate the strain ( ) on a part made of polycarbonate and close fitting onto a steel bracket. The parts are assembled at a room temperature of 73°F (23°C) and operated at an environmental temperature of 180°F (82°C).A.Select values of coefficients from Table 18:a1= coefficient of polycarbonate= 6.8 x 10-5a2= coefficient for steel= 1.2 x 10-5B.Calculate the change in temperature:DT = 180°F (82°C) - 73°F (23°C) = 138°F (59°C) C.Choose the appropriate thermal stress equationand insert values:e = (a1-a2) DT= (6.8 x 10-5 - 1.2 x 10-5 mm/mm/°C) x 59°C= 0.0033 mm/mm (0.33%)Because the steel bracket restrains the expansion of the polycarbonate part, a strain of 0.33% is induced in the part.Table 18 Coefficients of Thermal Expansion of Various Structural MaterialsCoefficient of Thermal ExpansionMaterial S.I.English Metricmm/mm/°C in/in/°F mm/mm/°C ABS9.5 x 10–5 5.3 x 10–59.5 x 10–5 Aluminum 2.2 x 10–5 1.2 x 10–5 2.2 x 10–5 Brass 1.8 x 10–5 1.0 x 10–5 1.8 x 10–5 Nylon8.1 x 10–5 4.5 x 10–58.1 x 10–5 PBT7.4 x 10–5 4.1 x 10–57.4 x 10–5PC 6.8 x 10–5 3.8 x 10–5 6.8 x 10–5PE12.0 x 10–5 6.7 x 10–512.0 x 10–5PP 5.8 x 10–5 3.2 x 10–5 5.8 x 10–5PS8.1 x 10–5 4.5 x 10–58.1 x 10–5 SAN 6.7 x 10–5 3.7 x 10–5 6.7 x 10–5 Steel 1.1 x 10–50.6 x 10–5 1.1 x 10–59192NOTICE: Dow believes the information and recommendations contained herein to be accurate and reliable as of March 2001. However, since any assistance furni shed by Dow wi th reference to the proper use and di sposal of i ts products i s provi ded wi thout charge, and si nce use condi ti ons and di sposal are not within its control, Dow assumes no obligation or liability for such assistance and does not guarantee results from use of such products or other infor-mation contained herein. No warranty, express or implied, is given nor is freedom from any patent owned by Dow or others to be inferred. Information contained herei n concerni ng laws and regulati ons i s based on U.S. federal laws and regulati ons except where speci fi c reference i s made to those of other juri sdi cti ons. Si nce use condi ti ons and governmental regulati ons may di ffer from one locati on to another and may change wi th ti me, i t i s the Buyer’s responsi bi li ty to determi ne whether Dow’s products are appropri ate for Buyer’s use, and to assure Buyer’s workplace and di sposal practi ces are i n compliance with laws, regulations, ordinances, and other governmental enactments applicable in the jurisdiction(s) having authority over Buyer’s operations.。
1999-Stuart Crampin-Calculable fluid-rock interactions
1994). Similar shear-wave splitting, with very similar characteristics, is seen in the lower crust and in the Earth’s mantle, but here we shall refer only to splitting in the uppermost 15–20 km of the Earth’s crust. Since first positively identified (Crampin et al. 1980), stressaligned shear-wave splitting in the Earth’s crust has been attributed to the stress-aligned distributions of the fluidsaturated intergranular microcracks and pores existing in almost all rocks. The fluid may sometimes be oil or gas, but is usually a liquid (at depth often super-critical) water-based salt solution. These distributions of aligned fluid-filled voids are known as extensive-dilatancy anisotropy or EDA (q.v.) and the individual voids as EDA-cracks (Crampin et al. 1984). Shear-wave splitting in EDA-cracks is illustrated schematically in Fig. 1. Although the origin and the ray path may be imperfectly known, the time-delays (usually normalized to ms/km) between the two split shear-waves and the azimuth of polarization of the faster split shear-wave, are comparatively stable and can be easily estimated from polarization diagrams. The recent advance reported in this introduction is the development of a model of anisotropic poro-elasticity, known as APE, that allows the evolution of stressed fluid-saturated rock to be calculated (Zatsepin & Crampin 1995, 1997; Crampin & Zatsepin 1995, 1997a). APE-modelling is highly constrained yet matches with considerable accuracy an increasing range of both field and laboratory observations over a wide range of wavelengths. This agreement confirms the earlier hypothesis that stress-aligned intergranular microcracks are the cause of the shear-wave splitting observed in the crust. This paper reviews these developments, which are believed to provide a new understanding of the nature of in situ rock. In particular, the ability to numerically model and predict the response of rock to changing conditions appears to have implications and applications over a wide range of academic and industrial Earth Science. Some essential terminology for seismic anisotropy is listed in Table 1.
岩石力学课件(英文版)第七章
Figure7-2 influence of surface configuration on in situ stress (a) irregular surface configuration
(b) linearisation of earth surface adumbration
(c) V alveole
Chapter 7 In situ stresses
Section 1
1. Basic concept
In situ stresses is the original amount of the Earth stress before the process of drilling and oil gas production.
2. Residual stress Because of the nonhomogeneity cooling of rock or the different coefficient of thermal expansion of rock unit although the rock is uniform cooled, residual stress will generate in the interior rock. Various local variation of mineral in the rock can also cause residual stress. The process of local recrystallization in the rock will generate bulk strain. Change about water content in the mineral aggregate will also bring about strain and residual stress. It is impossible to master the thermodynamics history of rock stratum component part and tiny geology evolution process. So the problem of residual stress can’t be resolved yet. Basic mechanics theory and exhaustive geologic examination can not predict the stress state.
中英文无损检测名词S
Safelight 安全灯Sampling probe 取样探头Saturation 饱和Saturation,magnetic 磁饱和Saturation level 饱和电平Scan on grid lines 格⼦线扫查Scan pitch 扫查间距Scanning 扫查Scanning index 扫查标记Scanning directly on the weld 焊缝上扫查Scanning path 扫查轨迹Scanning sensitivity 扫查灵敏度Scanning speed 扫查速度Scanning zone 扫查区域Scattared energy 散射能量Scatter unsharpness 散射不清晰度Scattered neutrons 散射中⼦Scattered radiation 散射辐射Scattering 散射Schlieren system 施利伦系统Scintillation counter 闪烁计数器Scintillator and scintillating crystals 闪烁器和闪烁晶体Screen 屏Screen unsharpness 荧光增感屏不清晰度Screen-type film 荧光增感型胶⽚SE probe SE探头Search-gas 探测⽓体Second critical angle 第⼆临界⾓Secondary radiation ⼆次射线Secondary coil ⼆次线圈Secondary radiation 次级辐射Selectivity 选择性Semi-conductor detector 半导体探测器Sensitirity va1ue 灵敏度值Sensitivity 灵敏度Sensitivity of leak test 泄漏检测灵敏度Sensitivity control 灵敏度控制Shear wave 切变波Shear wave probe 横波探头Shear wave technique 横波法Shim 薄垫⽚Shot 冲击通电Side lobe 副瓣Side wall 侧⾯Sievert(Sv) 希(沃特)Signal 信号Signal gradient 信号梯度Signal over load point 信号过载点Signal overload level 信号过载电平Signal to noise ratio 信噪⽐Single crystal probe 单晶⽚探头Single probe technique 单探头法Single traverse technique ⼀次波法Sizing technique 定量法Skin depth 集肤深度Skin effect 集肤效应Skip distance 跨距Skip point 跨距点Sky shine(air scatter) 空中散射效应Sniffing probe 嗅吸探头Soft X-rays 软X射线Soft-faced probe 软膜探头Solarization 负感作⽤Solenoid 螺线管Soluble developer 可溶显像剂Solvent remover 溶剂去除剂Solvent cleaners 溶剂清除剂Solvent developer 溶剂显像剂Solvent remover 溶剂洗净剂Solvent-removal penetrant 溶剂去除型渗透剂Sorption 吸着Sound diffraction 声绕射Sound insulating layer 隔声层Sound intensity 声强Sound intensity level 声强级Sound pressure 声压Sound scattering 声散射Sound transparent layer 透声层Sound velocity 声速Source 源Source data label 放射源数据标签Source location 源定位Source size 源尺⼨Source-film distance 射线源-胶⽚距离Spacial frequency 空间频率Spark coil leak detector 电⽕花线圈检漏仪Specific activity 放射性⽐度Specified sensitivity 规定灵敏度Standard 标准Standard 标准试样Standard leak rate 标准泄漏率Standard leak 标准泄漏孔Standard tast block 标准试块Standardization instrument 设备标准化Standing wave; stationary wave 驻波Step wedge 阶梯楔块Step- wadge calibration film 阶梯楔块校准底⽚Step- wadge comparison film 阶梯楔块⽐较底⽚Step wedge 阶梯楔块Step-wedge calibration film 阶梯-楔块校准⽚Step-wedge comparison film 阶梯-楔块⽐较⽚Stereo-radiography ⽴体射线透照术Subject contrast 被检体对⽐度Subsurface discontinuity 近表⾯不连续性Suppression 抑制Surface echo 表⾯回波Surface field 表⾯磁场Surface noise 表⾯噪声Surface wave 表⾯波Surface wave probe 表⾯波探头Surface wave technique 表⾯波法Surge magnetization 脉动磁化Surplus sensitivity 灵敏度余量Suspension 磁悬液Sweep 扫描Sweep range 扫描范围Sweep speed 扫描速度Swept gain 扫描增益Swivel scan 环绕扫查System exanlillatien threshold 系统检验阈值System inclacel artifacts 系统感⽣物System noise 系统噪声。
工艺参数中英文对照
工艺参数中英文对照在工艺参数中,英文和中文之间的对照是非常重要的,特别是在国际合作和交流中。
以下是一些常见的工艺参数中英文对照:1. 温度 - Temperature摄氏度 - Celsius华氏度 - Fahrenheit2. 压力 - Pressure巴 - Pascal磅力/平方英寸 - Pound per square inch (PSI)3. 流量 - Flow rate立方米/小时 - Cubic meters per hour (m³/h)升/分钟 - Liters per minute (L/min)4. 时间 - Time秒 - Second (s)分钟 - Minute (min)小时 - Hour (hr)5. 浓度 - Concentration摩尔/升 - Mole per liter (mol/L)百分比 - Percentage (%)6. 粘度 - Viscosity帕斯卡秒 - Pascal second (Pa·s)斯托克 - Stokes (St)7. 强度 - Strength兆帕 - Megapascal (MPa)千磅/英寸2 - Kilopound per square inch (ksi)8. 相对湿度 - Relative humidity百分比 - Percentage (%)重量比 - Weight ratio9. 电导率 - Conductivity10. 清洁度 - Cleanliness微克/立方米 - Micrograms per cubic meter (µg/m³)颗粒/升 - Particles per liter (p/L)11. 电流 - Current安培 - Ampere (A)毫安 - Milliampere (mA)12. 功率 - Power瓦特 - Watt (W)千瓦 - Kilowatt (kW)13. 电压 - Voltage伏特 - Volt (V)千伏 - Kilovolt (kV)14. 频率 - Frequency赫兹 - Hertz (Hz)千赫兹 - Kilohertz (kHz)15. 质量 - Mass克 - Gram (g)千克 - Kilogram (kg)16. 声音 - Sound分贝 - Decibel (dB)毫帕斯卡 - Millipascal (mPa)17. 测量精度 - Measurement accuracy百分之 - Percentage (%)小数点后几位 - Decimal places这只是一些常见的工艺参数中英文对照,根据不同的行业和背景,可能还有其他的对照。
侧缝撕裂强度测试的英文
侧缝撕裂强度测试的英文Side Seam Tear Strength Testing.Side seam tear strength testing is a crucial aspect of evaluating the durability and quality of clothing, particularly garments that are prone to tear or ripping along the seams. This testing ensures that the seams can withstand normal wear and tear, thus maintaining the garment's structural integrity and aesthetic value.The process of side seam tear strength testingtypically involves applying a controlled force to the seam, either manually or through the use of specialized equipment. This force is gradually increased until the seam gives way, tearing along the stitch line. The amount of force required to cause the tear provides a quantifiable measure of the seam's tear strength.There are several factors that can influence the tear strength of a seam, including the type of thread used, thestitch density, and the material of the garment itself. For example, thicker and stronger threads are generally more resistant to tearing, while a higher stitch density provides more support and stability to the seam. Additionally, fabrics with a tight weave and fewer imperfections are typically stronger and less prone to tearing.During the testing process, it's important to simulate real-world conditions as accurately as possible. This includes applying the force in a controlled manner, at a constant speed, and along a straight line parallel to the seam. It's also crucial to use a testing machine that is calibrated and maintained regularly to ensure accurate results.The results of side seam tear strength testing are often used by manufacturers to assess the quality of their products and make necessary adjustments to improve durability. For example, if a particular seam fails to meet the required tear strength standards, manufacturers may consider using stronger thread, increasing the stitchdensity, or switching to a different fabric to improve the garment's overall strength.In addition to ensuring product quality, side seam tear strength testing is also crucial for consumer safety. Garments that fail to meet minimum tear strength requirements may pose a safety hazard to the wearer, as they may rip or tear unexpectedly, causing accidents or injuries. Therefore, it's essential for manufacturers to conduct thorough testing to ensure that their products meet or exceed these standards.Overall, side seam tear strength testing is a critical component of quality control in the clothing industry. It helps manufacturers identify weaknesses in their products and make necessary improvements to ensure durability and consumer safety. By investing in this testing, manufacturers can gain valuable insights into their products' performance and use this information to create stronger, more reliable garments that meet the needs and expectations of their customers.。
构造水平应力 英语
构造水平应力英语Constructing Horizontal Stress: A Guide for Engineering ProfessionalsIntroduction:Horizontal stress plays a significant role in many engineering projects, including tunneling, mining, and geotechnical engineering. Understanding and manipulating horizontal stress is crucial for the successful completion of such projects. In this article, we will discuss how to construct horizontal stress and some essential aspects to consider.1. Definition of Horizontal Stress:Horizontal stress is the force that acts parallel to the surface of the earth's crust. It is perpendicular to the vertical stress and can cause potential stability problems in soil and rock masses subjected to excavation or construction.2. Methods to Construct Horizontal Stress:There are various methods used to create horizontal stress, including:a. Pre-Stressing: Pre-stressing is a technique that entails applying a load to the rock or soil mass before excavation or construction. The load can be applied using hydraulic jacks or explosives.b. Grouting: Grouting is the process of injecting amaterial, usually cement or other mixtures, under pressure into the soil or rock mass to consolidate and strengthen the ground conditions. This process is used to create ahorizontal stress in the soil or rock mass.c. Mechanical Anchors: Mechanical anchors are devices inserted into the rock or soil mass to create a pre-defined stress condition. These anchors can be traditional mechanical anchors or modern equipment that generates tension forces.3. Implications of Horizontal Stress:Horizontal stress has implications for the stability of a construction site. These implications can be positive, and horizontal stress can be utilized to provide support to the excavation or construction site. Alternatively, horizontal stress can also cause instability and failure of the site. It is important to understand the impact of horizontal stress on the site and consider appropriate measures to remedy adverse effects.Conclusion:In summary, creating a generous stress condition for construction is an essential consideration for engineering professionals. It affects the stability and safety of thesite and, if not monitored effectively, can lead toinstability and failure. The techniques mentioned in this article are just a few examples of how to constructhorizontal stress. However, the design and construction of the pre-defined stress condition should be based on a carefulconsideration of the geological and geographical conditions of the site, as well as the specific needs of each project.。
经椎旁肌间隙入路椎弓根螺钉固定与保守治疗轻中度中青年胸腰椎骨折的疗效比较
中华创伤骨科杂志2021 年 1月第 23 卷第 1期Chin J Orthop Trauma, January 2021. Vol. 23, No. 1• 39 •经椎旁肌间隙入路椎弓根螺钉固定与保守治疗轻中度中青年胸腰椎骨折的疗效比较赵轶波赵晓峰范志峰周润田关海山山西医科大学第二医院骨科,太原 030001通信作者:关海山,Email:ff860808@ 126. com【摘要】目的比较胸腰椎损伤分类及损伤程度评分系统(TUCS)评分矣4分的中青年胸腰椎骨折患者行经椎旁肌间隙人路椎弓根螺钉内固定治疗与保守治疗的疗效。
方法回顾性分析2014年1月至2018年12月山西医科大学第二医院骨科收治且获得随访的219例TLICS评分矣4分的胸腰椎骨折中青年患者资料。
根据治疗方法不同分为手术组(126例,行经椎旁肌间隙椎弓根螺钉内固定术)和保守组(93例,保守治疗)。
手术组:男65例,女61例;年龄18 ~37岁;TLICS评分:1分38例,2 ~4分88例。
保守组:男48例,女45例;年龄19 ~ 38岁;TLICS评分:丨分29例,2 ~4分64例。
两组患者在治疗前均进行胸腰椎X线、C T及MRI检查,治疗后均定期复查胸腰椎X线。
分别计算两组患者治疗后的下腰痛视觉模拟评分(VAS)较术前的改善情况,比较两组患者治疗前、治疗后1个月、末次随访时的VAS、伤椎前缘高度及后凸cobb角。
结果手术组和保守组患者治疗前一般资料比较差异均无统计学意义(P>〇. 05),具有可比性。
手术组随访24~72个月;治疗后1个月、末次随访时的VAS评分[(2. 5 ±1.2)分、(2. 3 ±0.8分)]较术前[(6.8±2. 1)分]显著改善,差异均有统计学意义(尸<0.05);治疗后未发生严重的手术并发症。
保守组随访30~65个月;治疗后1个月、末次随访时的VAS评分[(3. 9 ±1.9)分、(3. 5 ±0.9分)]较术前[(6. 2 ±2.0)分J M著改善,差异均有统计学意义(尸<0. 05);出现下肢神经症状3例,发生褥疮4例,肺部感染4例,并发症发生率为11. 8% (11/93)。
estimating the gradient threshold in the perona-malik equation
Applications of segmentation and noise reduction using a scale-sp efficient improvement in that treats an image not just as a two-dimensional (2-D) the classical scale-space analysis was proset of pixels but as one sample of a continuous range of posed by Perona and Malik in [7] where scaled images. Images at other scales are obtained by they describe the diffusion process known simple blurring operations. In general, there is not a prias the Perona–Malik (PM) equation. Despite the illori information on how to choose the appropriate scales posed nature of the PM equation, many of its applifor a given data set, and then the only reasonable cations could be carried with success in the signal approach is to represent the input data at multiple scales. This means that the original signal, by iterative processing field. On the other hand Weickert has processes, is embedded into a one-parameter family of proved the regularization of the PM equation derived signals, in which fine-scale structures are succesdescribing and analyzing a model on a semidiscrete sively suppressed. A necessystem [11]. Francesco Voci, Shigeru Eiho, sar y requirement is that In this article we presstructures at coarse scales ent a regularized model of Naozo Sugimoto, must represent simplificathe PM diffusion equation and Hiroyuki Sekiguchi tions of corresponding for image segmentation. structures at finer scales. The coarser scale structures We start from the hypothesis of well-posedness in should not be accidental results originated by the filterthe discrete space and the stability conditions. We will ing for suppressing fine-scale structures. show two methods for automatic setting of the gradiIt was first observed by Koenderink [1] that the ent threshold k , which is changed for each iteration generating equation of a linear scale-space is the linear of the partial differential equation (PDE) integration heat diffusion equation: The convolution of the origisteps. Experimental segmentations are implemented for noise reduction of generic digital images and for nal image with a Gaussian kernel is equivalent to the segmentation of microcalcifications on X-ray biomedsolution of the linear heat diffusion with an unitary ical images. constant diffusion c . The scale-space approach proposed by Koenderink has been based on the solution of the following linear Introduction heat diffusion equation: Today, the scale-space theory is an important area in image processing and in particular in visual operations. Significant methods and development were described by ∂I Koenderink [1], [2], Lindeberg [3], and Yuille and (1) = c ∇ 2I = c ∇ · ∇ I = c I x x + c I y y ∂t Poggio [4]. Scale space is a powerful theory of vision
海洋深水钻井
?随着世界各国对能源需求的增加及陆上和海水浅水区发现难度的增大,深水油气勘探不断升温。
在深水水平井钻井过程中井控技术是深水油气开发的核心技术之一,环空多相流流动规律研究则是井控理论的重要组成部分。
由于深水的存在使得环空多相流的流动特征与陆上相比更加复杂。
因此,进行深水水平井井控技术研究,对深水安全钻井具有重要意义。
????本文以传热学和热力学理论为基础,推导了深水钻井及压井过程温度分布模型,计算了深水井井筒温度场随井深和时间的变化关系;以气体分别在水中和油中的溶解度模型为基础,建立了气体在钻井液中的溶解度计算模型,计算得到了不同温度、压力下气体在钻井液中的溶解度。
在深入研究国内外多相流理论基础上,基于质量守恒、动量守恒原理,建立了适合于深水水平井的地层——井筒——隔水管——地面系统压力传递数学模型,并给出相应的边界条件,应用有限差分方法进行了数值求解,编制了模拟深水水平井溢流发生及压井分析的软件,分析了出气量、钻井液排量和钻井液体系等对环空压力和持液率等参数的影响规律。
考虑井底压差对地层渗流过程的影响,模拟计算了溢流发生过程中井底压力随时间变化关系,对影响溢流的敏感性因素及其影响规律进行了模拟分析。
对比分析了深水与陆上水平井压井过程,分析了节流管线长度、节流管内径和水平段长度对压井过程中立管压力和节流阀压力的影响,得到了立管压力和节流阀压力随时间的变化关系。
????模拟计算表明:出气量、排量和钻井液体系等因素对环空流动参数影响较大。
深水水平井的水平段越长井底压力降低越快,当气体快到井口时,井底压力几乎呈直线下降。
通过模拟深水水平井压井过程发现:节流管线越长,节流管内径越小,节流阀压力越大;水平段长度对深水水平井压井过程中立管压力和节流阀压力影响不大。
????本文研究成果可用于预测深水水平井环空循环温度场分布,气体在钻井液中的溶解度,结合上述模型可得到深水水平井溢流发展过程,为制定合理的压井施工措施提供理论支持。
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Horizontal stress contrast in the shallow marine sediments of the Gulf of Mexico sites Walker Ridge 313and Atwater Valley 13and 14e Geological observations,effects on wellbore stability,and implications for drillingRichard Birchwood *,Sheila NoethSchlumberger,1325South Dairy Ashford Road,Houston,TX 77077,USAa r t i c l e i n f oArticle history:Received 15August 2011Received in revised form 12January 2012Accepted 17January 2012Available online 25January 2012Keywords:Wellbore stability Geomechanics DrillingGas hydrateMethane hydrate AnisotropyHorizontal stress Backreaminga b s t r a c tSigni ficant horizontal stress anisotropy was encountered in three blocks in the Gulf of Mexico drilled by the Gulf of Mexico gas hydrates Joint Industry Project,namely,Atwater Valley 13,Atwater Valley 14,and Walker Ridge 313.The geological factors responsible for this state of stress and the implications for wellbore stability and drilling operations are explored.In Atwater Valley 13and 14,stresses at the well sites were perturbed by the underlying salt.In Walker Ridge 313,a combination of thrusting by adjacent salt and material anisotropy associated with the regional minibasin structure caused the maximum horizontal stress to rotate with depth.Horizontal stress anisotropy combined with a lack of heavy mud caused breakouts to form in the well Walker Ridge 313-G (WR313-G).A simple formula to predict the depth at which wells drilled with seawater are prone to breakouts is derived.Evidence is presented that the breakouts in WR313-G produced heavy cavings which were mainly responsible for the tight hole conditions encountered while drilling this well.However,it is shown that bottom hole assembly (BHA)design and drilling practices such as backreaming may have exacerbated these problems.Modi fications to drilling practices based on the experience gained from drilling WR313-G helped to improve the quality of the neighboring borehole WR313-H.Ó2012Elsevier Ltd.All rights reserved.1.IntroductionA frequently made assumption when modeling shallow marine sediments in the Gulf of Mexico is that the horizontal principal stresses are equal or close to equal (Ozkale,2006;Wojtanowicz et al.,2000).This paper discusses recent evidence of strong hori-zontal stress contrast from two drilling expeditions of the Gulf of Mexico Gas Hydrate Joint Industry Project (JIP).During the Leg I campaign in April and May of 2005,the JIP drilled and cored a series of riserless vertical wells at potential gas hydrate sites located at Atwater Valley and Keathley Canyon in the Gulf of Mexico.In Atwater Valley,two wells were drilled with conventional rotary bits (AT13#1and AT14#1)and three were drilled with corers (AT13#2,ATM #1,ATM #2).In Keathley Canyon,one well was drilled with a conventional rotary bit (KC151#2)and one was cored (KC151#3).The expedition was focused on drilling,logging,and coring operations for evaluation of gas hydrate related hazards associated with drilling through clay-dominatedsediments that are typical of the shallow sub-sea floor in the deepwater Gulf of Mexico (Ruppel et al.,2008).In 2009the Leg II expedition of the JIP aimed at evaluating gas-hydrate occurrences in coarser-grained sediments.The JIP conducted logging-while-drilling operations that included drilling and logging seven wells in three blocks:Green Canyon 955,Walker Ridge 313,and Alaminos Canyon 21(Boswell et al.,2012;Collett et al.,2011;Shedd et al.,2012).The locations of these blocks are shown in Figure 1.A constant challenge during the drilling campaign was to get optimal data quality by maintaining borehole stability in shallow unconsolidated sediments.According to Collett et al.(2009)many of the encountered drilling hazards were not gas hydrate-related.Issues such as borehole instability,drill cuttings removal,in fluxes of free gas and an apparent shallow water flow were among the problems faced during the two expeditions.In spite of these problems,most wells successfully reached their targets.Insights into optimizing drilling strategies for marine riserless drilling programs were gained.In this paper we analyze and review the stress field and stress directions as determined from features indicative of mechanical failure of the wellbore wall observed in logging-while-drilling images and caliper data from the Atwater Valley 13and 14sites*Corresponding author.E-mail address:rbirchwood@ (R.Birchwood).Contents lists available at SciVerse ScienceDirectMarine and Petroleum Geologyjournal ho mep age:www.elsevier.co m/lo cate/marpetgeo0264-8172/$e see front matter Ó2012Elsevier Ltd.All rights reserved.doi:10.1016/j.marpetgeo.2012.01.008Marine and Petroleum Geology 34(2012)186e 208(Leg I)and the Walker Ridge 313site (Leg II).Two types of failure modes are most commonly observed in wellbores,namely “breakouts ”,a form of compressive failure and “drilling-induced fractures ”,a form of tensile failure.Both types of failures can provide information about stress orientations.Drilling-induced compressive rock failure leading to breakouts occurs where the maximum hoop stress is higher than the rock strength (Zoback,2007).In a well drilled parallel to the vertical principal stress Sv,borehole breakouts tend to be aligned with the azimuth of the minimum horizontal stress.On the other hand,drilling-induced tensile fractures develop along the azimuth where the hoop stress is most likely to go into tension.These fractures tend to be aligned with the azimuth of the maximum horizontal stress.Both breakouts and fractures can be identi fied from resistivity images.Tensile fractures look like cracks along the wellbore wall,while breakouts usually cover a bigger area of the wellbore and the edges are not so well de fined.In vertical wells,both features tend to be aligned with the well axis and occur as conjugate pairs separated by 180 .Hence they can be distinguished from natural fractures or failure of the borehole wall caused by hydraulic erosion or mechanical wear.Since tensile fractures observable on wellbore images occur when the wellbore pressure exceeds the fracture gradient,this mode of failure can frequently be correlated with the existence of high wellbore pressure or ECD.1Zoback and Zoback (1980)used breakout information as well as earthquake focal mechanisms to build regional stress maps.Borehole breakouts as stress indicators are also described by Bell and Gough (1979),Plumb and Cox (1987),Plumb and Hickman (1985),Yassir and Zerwer (1997),and others.Examples ofdrilling-induced tensile fractures as stress indicators are shown in Castillo et al.(2000),Wiprut and Zoback (2000),and Zoback (2007).The Gulf of Mexico is considered to be a passive margin basin in a plate tectonic context with an extensional stress regime (Stein et al.,1989),but it is actively deforming because of the interplay of salt tectonics and sedimentary loading (Peel et al.,1995).The magnitude of the horizontal stresses in the Gulf of Mexico is not expected to be larger than that of the vertical stress.Rapid depo-sition at the shelf edge causes slumping,which results in some stress anisotropy.However,horizontal stresses near the seabed are sometimes assumed to be equal to the vertical stress due to their plastic nature (Wojtanowicz et al.,2000).In such circumstances,drilling-induced fractures and breakouts should not exhibit a preferred orientation.However in this paper,evidence of consistently oriented wellbore damage features in sediments located less than 300feet below the sea floor is presented for sites in Atwater Valley 13,Atwater Valley 14,and Walker Ridge 313.In the next section,the geological settings of the wells in Atwater Valley and Walker Ridge are described.In Section 3,image logs showing evidence of signi ficant horizontal stress contrast at both sites are presented.In Section 4,possible geological factors that could explain the observed horizontal stress anisotropy are considered.In Section 5,the implications of high horizontal stress contrast for wellbore stability and drilling operations are explored for the Walker Ridge sites.2.Geologic frameworkThe present-day Gulf of Mexico is characterized by a complex interaction of salt tectonics and sedimentary loading.The rifting during the Middle Jurassic created deep graben and elevated horst structures whose topography very probably in fluenced the post-rift deposition of the Upper Jurassic Louann Salt (Peel et al.,1995).Due to deposition of a high volume of Cretaceous e Cenozoic clastic sedi-ments,the shelf margin prograded several hundredkilometersFigure 1.Location map of the northern Gulf of Mexico showing the different JIP sites.JIP Leg I sites are displayed by green dots.The red stars indicate locations drilled during Leg II.Note:The site in AC818was not drilled since it revealed evidence of overpressures (figure modi fied from Boswell et al.,2009).(For interpretation of the references to color in this figure legend,the reader is referred to the web version of this article.)1ECD stands for “Equivalent Circulating Density ”.It is the density of a static column of drilling fluid required to generate the pressure at a given location in the borehole during mud circulation.The pressure developed during mud circulation is higher than the pressure exerted by a static mud column of the same density due to frictional effects.R.Birchwood,S.Noeth /Marine and Petroleum Geology 34(2012)186e 208187and the underlying Jurassic salt began to mobilize as diapirs and salt canopies driven by differential loading of the prograding clastic wedge.Salt-withdrawal minibasins withflanking salt bodies and ridges as well as slumps and debrisflows can occur as isolated systems or as components of salt-based detachment systems and are characteristic and very well documented(Diegel et al.,1995;Nelson, 1991;Prather et al.,1998).The Sigsbee salt canopy comprises more than100salt sheets and stocks that coalesced to cover more than 137,000km2on the lower continental slope of the northern Gulf of Mexico.The canopy is advancing along thrust systems with the leading edge of the canopy thrusts following the base of the Sigsbee Escarpment,a bathymetric step of about1250m(Hudec et al.,2009). Detachment faults soling into salt have created salt-cored foldbelts in sediments near the Sigsbee Escarpment,such as the Perdido Foldbelt in the western Gulf and the Mississippi Fan Foldbelt in the east(Fiduk et al.,1999;Hutchinson et al.,2008;Rowan et al.,2000). Salt-withdrawal minibasins in the shelf and upper slope are gener-allyfilled while those in the lower slope are still beingfilled(Winker and Booth,2000).The highly variable deposition rates in the minibasins depend on varyingfluvial input and slope debris.During the late Oligocene e Miocene the main depocenter moved eastwards to the present-day location of the Mississippi River.Fluid and gas migration pathways are usually located along the crests of the ridges, at the edges of the minibasins and near slope failures with faults that extend to the seafloor.These permeability pathways contribute to a seafloor morphology with hydrocarbon vents and pockmarks, chemosynthetic communities,authigenic carbonate outcrops, seafloor mud volcanoes and gas hydrate mounds(Lorensen et al., 2002).In the following sections,the drilled sites in Atwater Valley and in Walker Ridge are described in more detail.2.1.Atwater ValleyThe Atwater Valley area,with water depths of1300m,is located within the Mississippi Valley channel complex,with a thick sedi-mentary layer covering the underlying salt.The Pleistocene sedi-ments are complex and indicate multiple channel levee and slope fan systems.The massive deposits of the Pleistocene slope fan containing sands and shales show slumping and channeling. Subsequently,sands and shales were deposited in channel-levee systems(Dai et al.,2004).Mobile salt resulted in formation of the northwest-southeast trending fault system,which provides permeable pathways for gas migration and formation of gas hydrates.This fault system is possibly active today and enables migration to the series of mounds found in this area.2.2.Walker RidgeThe Walker Ridge313site is located in the tabular salt and mini-basin province of the Gulf of Mexico below about6500ft of water approximately90km north of the Sigsbee Escarpment in the Terrebonne mini-basin.The mini-basin is bounded to the south, east and west by large allochthonous salt bodies that can crop out locally at the seafloor(McConnell et al.,2009).Thus the basin architecture represents a closed low with a sand-delivery fairway (Frye et al.,2012).A result of uplift of the bounding ridges is a reversal of the depositional gradient and deposition of“ponded”sheet sands(Beaubouef and Friedmann,2000).According to Frye et al.(2012)recent uplift and extension have occurred at a north-south trending salt diapir at the northeast end of the salt wall, but the minibasin has also undergone recent compression, indicated by the morphologic expression of thrust faults in the seafloor(McConnell and Kendall,2002).The compression and fault morphologies indicate recent northwest-to-southeast salt move-ment on the northern side of the minibasin.3.Analysis of borehole images in Atwater Valley and Walker Ridge3.1.Introduction to resistivity imagesHigh-resolution electrical images of the near-wellbore region were analyzed in both the Atwater Valley and Walker Ridge wells. These images were produced while drilling by taking continuous 360 oriented measurements of downhole resistivity.The GVR6 tool(GeoVision*)has two transmitter coils and several electrodes that enable the tool to focus current at three different depths of investigation.The resulting GVR6button images have an azimuthal resolution of about6 (Bonner et al.,1996).The GVR6data are plotted as a planar,“unwrapped”,360 resistivity image of the borehole with depth.The image orientation is referenced to north. Orientation is measured by the magnetometers inside the tool. Horizontal features appear horizontal on the images,whereas planar,dipping features are sinusoidal in aspect.Since the tool is generally located close to the bit,measurements are made shortly after the bit passes a given depth.This minimizes the effect of hole degradation on the measurement.In water-based mud,borehole breakouts are identified on the GVR6image because of tool standoff from the elongated sides of the borehole ellipse which results in lower resistivity in the direction of the breakouts(Goldberg and Janik,2006;McNeill et al., 2004).Drilling-induced fractures are revealed as linear,low-resistivity features since they contain drillingfluid(Rezmer-Cooper et al.,2000).3.2.Resistivity images in Atwater ValleyFigure2shows resistivity images from AT13#1and AT14#1. Both wells exhibited pervasive drilling-induced fractures that are mostly oriented in an east-west direction.The fractures were caused by the ECD in the wellbore exceeding the fracture gradient. High ECD developed in these wells because boreholes were sealed off from the seafloor by either creep or a solids influx accompanying a shallow waterflow.A more detailed description of these events can be found in Birchwood et al.(2007).The consistent orientation of the hydraulic fractures in these boreholes suggests that there is a strong horizontal stress contrast in the Atwater Valley area.Although the hydraulic fractures in AT13#1and AT14#1were directed mostly east-west,this was not uniformly the case.Figure3 shows a close-up view of the hydraulic fracture in the shallow section of AT13#1.Between4400and4410ft RKB2(123e133fbsf), the hydraulic fracture appears to be directed northeast-southwest.A change in the direction of the fracture occurs between4410and 4412ft RKB(133e135fbsf).For the rest of the logged interval the fracture is consistently oriented in an east e west direction.The apparent change in orientation is indicative of a change in the stress direction at this depth and may have been caused by the presence of a fault(see Section4.1).3.3.Resistivity images in Walker RidgeThe wells drilled in Walker Ridge(WR313-G and WR313-H)are located at the edge of a salt withdrawal basin,about800m apart. *Mark of Schlumberger.2RKB is short for rotary kelly bushing.The RKB is a steel housing located on a drilling platform used to transmit torque from the rotary table to the drillstring. The RKB constitutes a standard reference for measuring depth in a borehole.In AT13#1the RKB was located4277ft above the seafloor.In AT14#1,WR313-G, WR313-H the corresponding distances were4309,6614,and6501ft.All logs shown in this paper with MD in the depth track are referenced to RKB.R.Birchwood,S.Noeth/Marine and Petroleum Geology34(2012)186e208 188Breakouts were observed in both boreholes.However,the break-outs in WR313-G were far more pervasive than those in WR313-H.Through examination of breakouts and a drilling-induced fracture in WR313-G,subtle changes in stress direction can be observed.Figure 4shows two sets of drilling-induced fractures in the WR313-G well.These fractures constituted the shallowest indica-tors of the stress direction in this well and are oriented northwest e southeast.This suggests a maximum horizontal stress with the same orientation at this depth.However this stress direction appears to rotate clockwise with increasing depth.Figure 5shows a set of breakouts in a deeper section of the well between 7100and 7200ft RKB.These are oriented east e west suggesting that the maximum horizontal stress is directed north e south.However,breakouts occurring in the deepest sections of the well tended to be oriented west-northwest e east-southeast suggesting that the maximum horizontal stress was oriented north-northeast e south-southwest.Figure 6shows an example of these deeper breakouts.Note that in contrast to the breakouts shown in Figure 5,the breakouts in Figure 6appear as resistive rather than conductive features.The paradox of resistive breakouts was described by Cook (2010)who suggested that gas hydrate may have formed inside these breakouts.Evidence supporting Cook ’s hypothesis will be presented shortly.The stress indicators shown in Figures 4e 6suggest that the maximum horizontal stress rotates from northwest e southeast at the surface to north-northeast e south-southwest deeper in the well.The breakouts in WR313-H are identi fied only for depths between 9165ft and 9175ft RKB.Over this interval (Fig.7)they show a northwest-southeast direction,indicating a maximum horizontal stress direction of northeast-southwest.This is in general agreement with stress direction of N40 E stated by Cook (2010)based on gas hydrate filled fractures in WR 313H.As previously stated,many of the breakouts observed in WR313-G were strikingly resistive relative to the surrounding formation (Fig.6).This suggests that gas hydrates were present at the location of these breakouts.Two possible explanations can be cited.The first is that the wellbore penetrated gas hydrate zones and that for some reason,gas hydrate was preserved only at the location of the breakouts.However as Cook (2010)pointed out,logging-while-drilling measurements indicated that wellbore temperatures were generally maintained well below the methane hydrate phase transition temperature.It is therefore unlikely that drilling would have caused gas hydrates to preferentially dissociate outside the breakouts.The second possible explanation is that gas hydrates formed within the breakouts during drilling.Support for this explanation can be seen in Figure 8which provides evidence that the gas hydrates in breakouts were localized borehole features that were distinct from the formations that were drilled.The figure shows some of the shallowest resistive breakouts recorded in the hole.Two resistivity logs,one a deep-reading 40-inch attenuation resistivity log and the other a relatively shallow buttonresistivityFigure 2.Well logs in (a)the well Atwater Valley 13#1and (b)the well Atwater Valley 14#1.Figures (a)and (b)both feature the difference between the bit size and the density caliper (blue shading,left track)and an image log derived from the GVR6tool (right track).(For interpretation of the references to color in this figure legend,the reader is referred to the web version of this article.)R.Birchwood,S.Noeth /Marine and Petroleum Geology 34(2012)186e 208189log,are shown.The shallow resistivity log shows spikes whenever gas hydrates are present in breakouts.However,at most of these spikes (shown by blue arrows)the deep-reading log does not show a signi ficant increase in resistivity.This suggests that the hydrates in the resistive breakouts are con fined to the near-wellbore region.Therefore the more plausible of the two possible explanations is that hydrates formed inside the breakouts during drilling.However,the time-span available for hydrate formation would have been very short.The time between opening of the hole and the pass of the GVR tool would have been anywhere between 1and 5min,depending on the rate of penetration (ROP).Why would hydrates form inside the breakouts?Possible explanations include:1.Enhanced surface roughness inside the breakouts is conducive to gas hydrate nucleation or accumulation.Surface roughness is thought to aid the nucleation of gas hydrates (Ceccotti,1966;Lee,2007).An additional effect of surface roughness may be to impede re-entrainment of deposited gas hydrate crystals intothe flow stream.The effect of surface roughness on detachment of particles from a surface by hydrodynamic forces is described in Vaidyanathan and Tien (1988)and Das et al.(1994).2.The presence of breakouts could alter the flow pattern to produce conditions more favorable to gas hydrate formation and/or deposition.When fluid flows over a cavity,the pressure inside a cavity can be reduced relative to that in the undis-turbed flow and velocity reversal can occur (Sinha et al.,1981;Zdanski et al.,2003).Such conditions may aid formation and deposition of gas hydrate crystals.The fact that the annulus between the BHA and the borehole wall was narrow 3should have enhanced the effect of breakouts on the flow regime.3.Gas hydrates tend to form everywhere but they are constantly removed from the borehole wall as a result ofmechanicalFigure 3.Image log derived from GVR6tool in Atwater Valley 13#1.Hole diameter (blue curve),gamma ray (green curve),and hydrate saturation derived from resistivity (shaded)shown in leftmost track along with measured depth.Image derived from shallow resistivity reading shown in Track 2.Hydraulic fractures appear as conductive features running parallel to the vertical borehole.(For interpretation of the references to color in this figure legend,the reader is referred to the web version of this article.)3The average annular gap between the GVR6tool and the in-gauge borehole wall was approximately 0.9in.R.Birchwood,S.Noeth /Marine and Petroleum Geology 34(2012)186e 208190agitation of the fluid by the rotating drill pipe.Gas hydrates inside breakouts are relatively protected from these effects due to their increased distance from the drill pipe.It is obvious that more rigorous studies of this phenomenon need to be carried out.4.Geological origins of stress anisotropyBorehole breakouts and drilling-induced fractures at both Atwater Valley and Walker Ridge are indicative of a difference in the magnitudes of the maximum and minimum horizontal stresses.The apparent maximum stress direction in the Atwater Valley sites is approximately east e west,while the direction in the Walker Ridge drilling site rotates from northwest e southeast at the surface to north-northeast e south-southwest deeper in the subsurface.It will be shown that the stress state in Atwater Valley is quite complex and possibly non-uniform.To gain insight into the controls on stress direction in both areas,bathymetric maps and seismic cross-sections were examined.Yassir and Zerwer (1997)observed that the maximum horizontal stress in the Gulf of Mexico is frequently aligned with bathymetric contours that describe the prograding sedimentary wedge of the Gulf of Mexico (Yassir and Zerwer,1997).However,they caution that topographic features by themselves are unlikely to exercise much control over stresses except very near to the surface.Simulations of stresses in a uniform half-space suggest that the in fluence of typical surface topographical features on horizontal stresses dies out within a few hundred meters of the surface (Evans et al.,1989).Caution is therefore warranted in interpreting stress orientations in the JIP wells based solely on surface topography.Stress orientations derived from surface features are more likely to be indicative ofstresses at depth to the extent that they represent the overall geometry of deeper structural features.The shape of the sedimentary wedge in the Gulf of Mexico allows for the extensional stress regime on the continental slope with typical listric normal faulting,gravity spreading and gravity gliding,and a compressional stress regime at the toe of the wedge on the lower slope with reverse or thrust faults (Galloway,1986).In such a geotectonic setting,the direction of maximum horizontal stress would be parallel to the strike of the normal faults (Anderson,1951).This means that on a regional scale the maximum horizontal stress is oriented in a general northeast-southwest direction.Examples are shown in studies by Yassir and Zerwer (1997)and recently by Cook et al.(2008)for Keathley Canyon and by Cook (2010)for the Walker Ridge sites.However Cook (2010)treated the stress direction in WR313-G to be uniform and did not consider the subtle expressions of stress rotation with depth in this well.It will be shown that such rotations are probably caused by the interplay between the structure of the salt minibasin penetrated by WR313-G and the compressional forces exerted by the surrounding salt.4.1.Atwater ValleyFigure 9shows a bathymetric map of the Atwater Valley area with the direction of maximum horizontal stress as can be inter-preted from the drilling-induced fractures in AT13#1and AT14#1.The interpreted stress direction is not aligned with bathymetric contours and is therefore at variance with the trend observed by Yassir and Zerwer (1997)in the Gulf of Mexico.One possible cause could be salt-induced stress rotation.Figure 10shows seismic cross-sections through the trajectory of the well AT13#1.A series of faults extend upwards to the sea floor from the salt body.In general the area is characterizedbyFigure 4.Image logs revealing drilling-induced fractures in WR313-G.R.Birchwood,S.Noeth /Marine and Petroleum Geology 34(2012)186e 208191northwest e southeast trending faults that provide pathways for gas to migrate to the surface.Many of these faults intersect the mudline 4and appear to be active.Salt migration in the underlying northwest e southeast-trending salt ridge caused faulting and warping of the overlying sediments,resulting in steeply dipping beds (see Fig.10).Both AT13#1(Fig.10)and AT14#1intersected a major northeast-dipping fault that is in contact with the underlying salt,indicating that possibly,the stresses at these locations are in flu-enced by the salt body in the subsurface (Fig.10).Salt introduces a complex set of stress perturbations into the surrounding sedi-ments including enhanced horizontal stress anisotropy (Dusseault et al.,2004;Fredrich et al.,2003).The northwest e southeast-striking normal faults with northeast dip indicate maximumhorizontal stresses in a northwest-southeast direction;however,the drilling-induced fractures observed in the wells indicate an east e west direction.The faults extend all the way to the seabed and should thus provide a good indication of the present-day stress state.To understand the discrepancy,a detailed numerical model of stress perturbations around salt and faults is required.Such a study lies beyond the scope of the present paper.4.2.Walker RidgeFigure 11shows an east-west cross section of the minibasin in which the Walker Ridge wells were drilled.The different maximum horizontal stress directions,i.e.,northwest e southeast shallow,north e south from 7030to 7300ft RKB,and north-northeast e south-southwest in the deeper sections are described in Section 3.3.Thrust faults outcropping at the surface and associated with recent salt movement (Hutchinson et al.,2009;McConnell and Kendall,2002)indicate a direction of maximum horizontal stress consistentwithFigure 5.Drilling-induced breakouts in the well WR313-G recorded by the GVR6tool.Tracks 2,3,and 4show resistivity images at shallow,medium,and deep depths of inves-tigation,respectively.Borehole breakouts appear as conductive (dark)features running parallel to the vertical borehole and are consistently oriented in an east e west direction,indicating a maximum stress direction of north e south.Connection points at 7113and 7178ft RKB are shown.Note persistence of breakouts at all three depths of investigation.4The term “mudline ”refers to the boundary between the earth and a body of water.In marine settings the mudline coincides with the sea bed.R.Birchwood,S.Noeth /Marine and Petroleum Geology 34(2012)186e 208192。