Speeding-up Fault Injection Campaigns in VHDL models
奇思妙想高速发射器英语作文
奇思妙想高速发射器英语作文English Answer:The Whirling Wonder High Velocity Launcher (WW-HVL) isa groundbreaking engineering marvel that combines the principles of centrifugal force, electromagnetic propulsion, and aerodynamic design to achieve unparalleled projectile velocities. It epitomizes the pinnacle of human ingenuity and innovation in the realm of projectile launch systems.The WW-HVL harnesses the centripetal force generated by a rotating arm to propel projectiles with exceptional speed and accuracy. The arm, powered by an advanced magnetic levitation system, spins at astonishing speeds, creating a centrifugal force that propels the projectile outward. This centrifugal force is precisely controlled and calibrated to ensure optimal projectile acceleration and velocity.In addition to the centrifugal force, the WW-HVL incorporates electromagnetic induction technology tofurther enhance projectile speed. A series of electromagnetic coils strategically positioned along the launch path generate a powerful magnetic field thatinteracts with the projectile's conductive material. This interaction creates an electromagnetic force that propelsthe projectile forward, complementing the centrifugal force.Aerodynamic design plays a pivotal role in maximizingthe WW-HVL's performance. The projectiles are meticulously engineered with streamlined bodies that minimize air resistance and optimize airflow. The launcher's trajectoryis precisely calculated to leverage the laws of aerodynamics, ensuring that the projectile follows a parabolic path with minimal deviation.The WW-HVL boasts an impressive array of features that make it an unparalleled projectile launch system. Its high velocity capability enables projectiles to reach speeds exceeding Mach 10, providing scientists and researcherswith unprecedented opportunities for studying hypersonic phenomena. Its precision firing mechanism ensures pinpoint accuracy, making it ideal for applications where precisetarget engagement is paramount.Furthermore, the WW-HVL is highly versatile and can accommodate projectiles of varying sizes and weights. This versatility makes it suitable for a wide range of applications, including research and development, military defense, and space exploration. Its modular design allows for easy customization and reconfiguration, enabling scientists and engineers to tailor the launcher to specific experimental or operational requirements.The WW-HVL stands as a testament to human ingenuity and the tireless pursuit of scientific advancement. Its unique combination of centrifugal force, electromagnetic propulsion, and aerodynamic design provides unmatched projectile velocities and precision, opening up new frontiers in research, defense, and space exploration.中文回答:旋风奇想高速发射器。
海员机工考试英语试题及答案
海员机工考试英语试题及答案一、选择题(每题2分,共20分)1. Which of the following is the correct way to spell the word "maintenance"?A. MaintananceB. MaintenenceC. MaintenenceD. Maintenance答案:D2. The term "deadweight" refers to:A. The maximum weight a ship can carryB. The weight of the ship without cargoC. The weight of the cargo onlyD. The total weight of the ship including cargo答案:A3. What does the abbreviation "SOLAS" stand for?A. Society of Load and Load AfloatB. Safety of Life at SeaC. Standard Operating Load and Load AfloatD. Ship Operations and Load Afloat答案:B4. Which of the following is not a type of marine fuel?A. Heavy fuel oilB. Marine gas oilC. Liquefied natural gasD. Unleaded gasoline答案:D5. The International Maritime Organization (IMO) is responsible for:A. Regulating the global shipping industryB. Providing maritime educationC. Conducting marine researchD. All of the above答案:A6. What is the primary function of a lifebuoy?A. To provide a source of lightB. To be used as a signaling deviceC. To assist in rescuing a person overboardD. To store emergency rations答案:C7. The term "GMDSS" stands for:A. Global Maritime Data SystemB. Global Maritime Distress and Safety SystemC. Global Maritime Development SystemD. Global Maritime Delivery System答案:B8. What is the purpose of a bilge pump on a ship?A. To pump water from the bilges to maintain the ship's stabilityB. To cool the ship's engineC. To clean the ship's deckD. To transfer fuel between tanks答案:A9. The term "LOA" when referring to a ship, stands for:A. Length of ArrivalB. Length of AgreementC. Length Over AllD. Length of Approval答案:C10. Which of the following is not a navigational aid?A. BuoyB. LighthouseC. RadarD. Compass答案:C二、填空题(每题2分,共20分)1. The _______ is the part of the ship's hull that is in contact with the water.答案:hull2. The term "draft" refers to the _______ of a ship's hull that is submerged in water.答案:depth3. A _______ is a device used to measure the depth of water. 答案:sounder4. The _______ is the highest point of a ship's structure above the waterline.答案:mast5. The _______ is a device used to measure the speed of a ship through the water.答案:log6. The _______ is the area on a ship where cargo is loaded and unloaded.答案:cargo hold7. A _______ is a rope used to secure a ship to a dock or another ship.答案:hawser8. The _______ is the part of the ship's deck where the crew works.答案:forecastle9. The _______ is a device used to communicate with other ships and shore stations.答案:radio10. The _______ is a type of knot used to secure a rope to a fixed object.答案:cleat hitch三、简答题(每题10分,共40分)1. What are the main functions of a ship's engine room?答案:The main functions of a ship's engine room include generating power for propulsion, providing mechanical energy for various onboard systems, and maintaining the ship's operational efficiency.2. Explain the importance of regular maintenance of a ship's hull.答案:Regular maintenance of a ship's hull is crucial for preventing corrosion, minimizing biofouling, ensuring the structural integrity of the vessel, and maintaining its hydrodynamic efficiency, which in turn affects fuel consumption and overall performance.3. What are the key components of a ship's navigation system? 答案:Key components of a ship's navigation system include the compass, radar, GPS, chart plotter, autopilot, and communication equipment such as VHF radios and satellite communication systems.4. Describe the role of a ship's life-saving equipment in emergency situations.答案:In emergency situations, a ship's life-saving equipment plays a critical role in ensuring the safety of the crew and passengers. This equipment includes lifeboats, life rafts, lifebuoys, lifejackets, and emergency signaling devices, which are designed to facilitate rescue operations and provide temporary survival support until help arrives.。
六年级英语交通工具功能单选题60题
六年级英语交通工具功能单选题60题1. If you want to travel long distances quickly, which transportation do you choose?A. CarB. BikeC. PlaneD. Train答案:C。
本题考查不同交通工具的特点。
A 选项“Car”( 汽车)速度较快,但长途旅行不如飞机高效。
B 选项“Bike”(自行车)适合短距离出行。
C 选项“Plane”( 飞机)能快速长途旅行。
D 选项“Train” 火车)速度比飞机慢。
所以选C。
2. When you go to school nearby, which one is the best choice?A. BusB. SubwayC. BikeD. Ship答案:C。
这道题考查距离较近时的交通工具选择。
A 选项“Bus” 公交车)通常用于较长距离的公共交通。
B 选项“Subway”( 地铁)适用于城市中较长距离的出行。
C 选项“Bike”(自行车)适合短距离且灵活方便。
D 选项“Ship”(轮船)一般用于水上长途运输。
所以选C。
3. You need to carry a lot of goods. Which transportation is suitable?A. TaxiB. TruckC. MotorcycleD. Helicopter答案:B。
此题涉及运输大量货物的交通工具。
A 选项“Taxi”( 出租车)主要载人。
B 选项“Truck” 卡车)能承载大量货物。
C 选项“Motorcycle”( 摩托车)载货能力有限。
D 选项“Helicopter”( 直升机)多用于特殊情况,载货不是其主要功能。
所以选B。
4. If you want to enjoy the scenery during the journey, which transportation is better?A. PlaneB. TrainC. ShipD. Subway答案:B。
fault running gear workshop! 翻译
fault running gear workshop! 翻译翻译:故障运行设备修理店说明用法:该短语指向进行设备维修和修理的商店或工作坊。
在这种类型的工作坊中,技术人员可以对各类设备进行维修,包括机械设备、汽车部件、电子设备等。
10句双语例句:1. My car broke down, so I had to take it to the nearest running gear workshop.我的车坏了,所以我不得不把它带到最近的运行设备修理店。
2. The running gear workshop managed to fix my bicycle tire within a day.运行设备修理店在一天之内修好了我的自行车轮胎。
3. The technician at the running gear workshop repaired my laptop charger quickly and efficiently.运行设备修理店的技术人员迅速而高效地修好了我的笔记本电脑充电器。
4. We need to find a running gear workshop that specializes in repairing industrial machinery.我们需要找一家专门修理工业机械的运行设备修理店。
5. The running gear workshop is known for their expertise in fixing engine faults.这家运行设备修理店以修复发动机故障技术而闻名。
6. I contacted the running gear workshop to schedule an appointment for my broken generator repair.我联系了运行设备修理店,为我坏了的发电机预约维修。
7. The running gear workshop offers a warranty for all the repairs they do.运行设备修理店对他们所做的维修提供保修。
卷11-备战2022年高考英语【名校地市好题必刷】全真模拟卷(新高考专用)第三辑(原卷版)
第一模拟(本卷共3部分,满分120分,考试用时90分钟)注意事项:1. 答卷前,考生务必将自己的姓名、准考证号填写在答题卡上。
2. 回答选择题时,选出每小题答案后,用铅笔把答题卡上对应题目的答案标号涂黑。
如需改动,用橡皮擦干净后, 再选涂其他答案标号。
回答非选择题时,将答案写在答题卡上,写在本试卷上无效。
3. 考试结束后,将本试卷和答题卡一并交回。
第一部分阅读(共两节, 满分50分)第一节(共15小题;每小题2.5分, 满分37.5分)阅读下列短文,从每题所给的A、B、C、D四个选项中选出最佳选项。
(2021·百校联盟2022届高三11月质量监测英语试题)AThese Kids Books Written by Famous People Are Perfect for Your Little KidsKelly Clarkson Wrote a Book Inspired By Her DaughterWhen Kelly Clarkson wrote River Rose and the Magical Lullaby, she named the main character after her young daughter. The story follows Rose, who finds herself in a magical dreamworld, led by the voice of her mother. At the end of the book, there’s a link to a lullaby (摇篮曲)performed by Clarkson. She’s even said that writing the book was harder than any song she’sever written, but she felt like she had to try.Jim Carrey Is on a Roll With This BookJim Carrey’s new show, Kidding, on Showtime, is decidedly not for kids. His 2013 book, How Roland Rolls, however, is very much for the little ones. How Roland Rolls is about a wavewho worries about what will happen when he finally hits the beach. His fear disappears when herealizes he’s more than just a wave, he’s the entire ocean!备战2022年高考英语【名校地市好题必刷】全真模拟卷(新高考专用)Jamie Lee Curtis Has Been Writing Since The’90sYou might know her best from the Halloween film, but your kids know her best as the author of T his is Me: A Story of Who We Are and Where We Came From. This is Me is a story about immigration(移民). Curtis says “Every person has an immigrant story in their family, and we’re losing that. I thought it was important to connect that thread back to who we are.”Steve Martin’s Books Prove He’s a Comedian For All AgesThere’s a good chance that you grew up with Steve Martin. Now your kids can read his books, too. Since getting into children’s writing, Martin has written several books, including Late for School and The Alphabet From A to Y with Bonus Letter Z. Each letter of the alphabet is paired with a poem by Martin.1. What can you enjoy in Kelly Clarkson’s book?A. A beautiful baby song.B. Deep love from a mother.C. Experiences of her daughter.D. A story happening in the dream.2. What benefit can you probably get from the book How Roland Rolls?A. Learning language knowledge.B. Helping you find yourself.C. Appreciating the beauty of the ocean.D. Knowing your family members better.3. Which book tells about the family history?A. This is Me.B. River Rose.C. Late for School.D. How Roland Rolls.B(2022·河北高中2022届高三上学期12月份教学质量监测英语试卷)All Olympic medalists work incredibly hard to reach their goals, but Maria Andrejczyk went through someserious struggles before reaching the platform. The Polish javelin(标枪) thrower missed her chance at the 2016 Olympic Games by just 2 centimeters. Sidelined by a shoulder injury in 2017, she then learned she had bone cancer. Showing true fighting spirit, Maria powered through her recovery in time to qualify for the 2020 Games in Tokyo, Japan, All of her effort was worth it when she earned her first Olympic medal ever, a silver!Back at home, she heard about an 8- month-old baby named Miloszek Maysa, who desperately needed to go to the U.s. for a surgery that could save his life. Miloszek was born with a serious heart disease, which wasn’t detected in time to correct in the first weeks of his life. Baby Miloszek’s condition was too serious to be treated in his home country, but doctors at Stanford University Medical Center in California were able to take his case.Unfortunately, they required 80 percent of the payment up front, a sum the Maysa’s family simply could not afford. That’s when Maria stepped in to help! Just week after returning from Japan, the athlete shared a message on Facebook announcing that she would be auctioning off her silver medal to raise money for Miloszek’s surgery.Days later, a Polish convenience store called Zabka purchased the medal for $125,000, which was more than Maria had hoped to get. Not only that, but when her story broke, more people began donating to the fundraiser. In the end, they pulled in more than enough cash to cover Miloszek’s trip to America! And the goodwill doesn’t end there. Zabka announced that they would let Maria keep her medal after all!4. What can we know about Maria in Paragraph 1?A. She won a gold medal in 2020.B. She spent a miserable childhood.C. She beat his bone cancer in 2016.D. She kept fighting against the difficult life.5. Why did Miloszek have to go to the U.S. for a surgery?A. He was too young.B. His home condition was poor.C. His home country abandoned him.D. Doctors at Stanford University could treat him.6. What does the underlined phrase "auctioning off" in Paragraph 3 probably mean?A. Selling.B. Lending.C. Making.D. Returning.7. What is Zabka’s attitude to Maria’s behavior?A. Doubtful.B. Supportive.C. Ambiguous.D. Disapproving.C(2022·江苏南京一中2022届高三下学期开学检测英语试题)In gardens across Britain the grass has stopped growing, which is not drought-stricken. In fact, it is greener and cleaner than ever before. That is because the lawns are actually artificial substitutes.Britons are fascinated by lawns. Country estates (庄园) have long competed to have the most perfectly cut and polished grassland. “What you’re saying in big loud capital letters, is ‘I’m so terribly wealthy’,” says Fiona Davison of the RHS(皇家园林协会). With the coming ofgrass-cutting machines in 1830, the middle classes joined the fun.But now Britons have fallen in love with artificial grass. Evergreens UK, which sells the stuff, says it has seen a 120% rise in sales since 2015. Artificial grass is popular with families who have children or dogs and don’t want mud dragged through their houses. It has another charm factor, too—people now see gardens as “outside rooms”—pairing carpets of artificial grass with delicately decorated seating and hot containers.Not everyone is a fan. Artificial grass contains microplastics that ruin soil and risk flooding.A study finds earthworms gain 14% less body weight when operating under rubber, a form of artificial grass, which might not be a problem for its fans, as wormholes are regular disgusting things, but it disappoints green types. Ms Davison says a group of wildlife-loving gardeners is blooming, many having caught the bug during COVID-19 lockdowns. For example, a landscape designer says they like things less neat and try “to capture that wild element”. These eco-gardeners are influenced by rewilding projects and are more likely to be environmentalists.While three written documents signed by many people have tried to stop artificial grass spreading, the government says regulating what people do in their backyards is wrong. The RHSis concerned about artificial grass, but prefers persuasion to laws. “We say ‘Let a hundred flowers bloom’,” says Ms Davison.8. What can be inferred from Davison’s remark in Paragraph 2?A. She is very rich.B. High-quality grassland is valued.C. Operating a cutting machine is fun.D. The gardening competition is fierce.9. What possibly contributes to the popularity of artificial grass?A. Messy grasslands.B. Gardens’ new function.C. Advertising campaigns.D. Ill-mannered children and dogs.10. What can replace the underlined phrase “caught the bug” in Paragraph 4?A. got infected.B. lost their temper.C. became depressed.D. develop the passion.11. Which of the following is a suitable title of the text?A. The Barrier of British GrasslandB. The Appeal of Grassland for BritonsC. The Fight to Define the Great British GardenD. The Competition to Become the Best GrasslandD(2022·山东济宁2022届高三上学期期末考试英语试题)A new study shows that increases in extreme winter weather in parts of the US are linked to quickened warming of the Arctic.Over the past four decades, warming in the Arctic has been far more definite than that in the rest of the world and has caused a rapid decrease of summer sea ice. Heating in the Arctic has ultimately disturbed the circular pattern of winds known as the polar vortex (旋涡). As a result, it got stretched out of shape and slid southward off the pole. Scientists believe this vortex stretching process led to the deadly Texas cold wave in February this year.“The polar vortex over the Arctic usually locks in cold air at the poles and does not easily move south. The stronger the winds, the more the air inside is kept, and the colder it gets,” explained lead researcher Dr. Judah Cohen, who’s a professor at the Massachusetts Institute of Technology (MIT). “Melting ice in the Arctic and rising temperatures can disturb the Arctic vortex, making cold air no longer locked in the Arctic? but move some farther south.”The researchers say that their findings are based on both observations and modelling and they show a physical link between climate change in the Arctic, the stretching of the polar vortex and the impacts on ground.The researchers believe their work could improve predictions about the beginning of extreme cold winter events. The research team also believes that their findings will help people understand that global warming is complex and perhaps let go of the idea that colder winters mean climate change isn’t happening. “In the past, these cold extremes over the US and Russia have been used to justify not reducing carbon, but there’s no longer any excuse to not start reducing emissions right away,’’ said Dr. Cohen.12. What is paragraph 2 mainly about?A. The efforts made by scientists.B. The definition of polar vortex.C. The decrease of summer sea ice.D. The formation of Texas cold wave.13. What is the function of polar vortex?A. Making the wind stronger.B. Helping cold air move freely.C. Speeding up the melting of ice.D. Keeping cold air from escaping.14. What can be inferred from the last paragraph?A. Global warming is just alarmist.B. Weather-gone-wild pattern is a fantasy.C. Reducing emissions is a pressing matter.D. Weather forecast has never been a perfect science.15. In which column of a website can the text probably be found?A. Environment.B. Travel.C. Education.D. Life.第二节(共5小题:每小题2. 5分, 满分12. 5分)阅读下面短文, 从短文后的选项中选出可以填入空白处的最佳选项。
ECMAScript Language Specification, 3rd Edition
Cache Size Selection for Performance,Energy and Reliability ofTime-Constrained SystemsYuan Cai,Marcus T.Schmitz,Alireza Ejlali,Bashir M.Al-Hashimi,Sudhakar M.Reddy Department of Electrical and Computer Engineering,University of IowaE-mail:yucai,reddy@School of Electronics and Computer Science,University of SouthamptonEmail:ms4,ae04v,bmah@Abstract—Improving performance,reducing energy con-sumption and enhancing reliability are three important objec-tives for embedded computing systems design.In this paper,we study the joint impact of cache size selection on these three objec-tives.For this purpose,we conduct extensive fault injection exper-iments onfive benchmark examples using a cycle-accurate pro-cessor simulator.Performance and reliability are analyzed using the performability metric.Overall,our experiments demonstrate the importance of a careful cache size selection when designing energy-efficient and reliable systems.Furthermore,the experi-mental results show the existence of optimal or Pareto-optimal cache size selection to optimize the three design objectives.I.I NTRODUCTIONCache memories are widely used in microprocessors to im-prove the system performance[1].As small,fast on-chip mem-ories,caches store frequently accessed instructions and data to avoid a large number of accesses to the slow,off-chip main memory.Depending on the way the cache blocks are mapped onto the main memory,we distinguish between direct-mapped caches(each main memory address is mapped to one and only one cache block)and-way set-associative caches(each main memory address can be mapped to possible cache blocks). As opposed to the slow dynamic main memory,cache mem-ories are implemented asflip-flops using static logic.Though cache memories can improve the system performance dramat-ically,they are responsible for a large portion of the overall system’s power dissipation[2].To reduce the energy dissi-pation,several approaches of dynamic cache reconfiguration have been reported.Zhang et al.[3]proposed a technique called way concatenation that tunes the cache ways between one(direct-mapped),two and four.Accordingly,at a reduced number of ways(1and2)the corresponding unused cache ways are disable.This is carried out under software control, i.e.,at application run-time.They report an average energy saving of40%compared to afixed four-way cache.Simi-larly,Dropsho et al.[4]introduced a cache design,called ac-counting cache based on the selective ways cache[5].The number of active ways is dynamically change under hardware control.Powell et al.[6]applied way-prediction and selec-tive direct-mapping to reduce the set-associative cache energy.This work is supported in part by the EPSRC,U.K.,under grant GR/S95770,EP/C512804This is achieved by predicting the matching way and access-ing only this matching one,instead of all ways.A dynamic online scheme that combines the processor voltage scaling and dynamic cache reconfiguration was proposed by Nacul et al.[7].Their online algorithm adapts the processor speed and the cache subsystem to the workload requirements of the appli-cation.In a similar fashion,Zhang et al.[2]introduced an online heuristic that dynamically adjusts the cache size in or-der to minimize the cache energy.Their experiments point out that among all configurable cache parameters,cache size has the largest impact on cache performance and energy consump-tion.Yang et al.[8]investigated different design choices for resizable caches and evaluated their efficiency in reducing the system’s energy dissipation.While these approaches are ef-fective in reducing the energy dissipation,they neglect another important factor,namely the cache reliability.Cache reliability is mainly threatened by transient faults, caused by strikes from alpha particles and energetic particles [9].When a memory cell(flip-flop)is hit by such a particle, though the circuit itself is not damaged,the stored bit value canflip and cause an error.This problem is becoming more and more serious due to the ever-shrinking feature size and re-duced supply voltage levels[10].Hardware approaches that are dedicated to improve the cache reliability have been pro-posed.Such approaches make use of spatial redundancy to cor-rect corrupted bits,for instance,data word parity[11]and Sin-gle Error Correct-Double Error Detect Error Correcting Codes (SEC-DED ECC)[12].Li et al.[10]studied the impact of two leakage energy reduction approaches on the cache reliability. They also used the word parity and SEC to detect and correct the corrupted bits.However,the impact of cache size selection was not considered.Clearly,the spacial redundancy requires additional hardware and decreases the performance,hence is likely to increase the cache energy consumption. Nevertheless,like cache energy and performance,the cache reliability is also affected by the cache size.The reason for this is threefold.Firstly,when the cache size is reduced(for instance,through disabling a portion of the cache),the proba-bility of particle-hits in the smaller active area is also reduced and particles hitting the disabled part of the cache will not man-ifest in errors.Secondly,the execution time of the application generally increases as the cache size decreases.The proba-bility of particle-hits during a longer execution time increases. Thirdly,if time redundancy techniques(e.g.rollback recovery)12(b) Cache size set to 128 lines (slack for one re−execution)128256641(a) Cache size set to 256 lines (slack for 2 re−executions)1128256641CacheTask execution(c) Cache size set to 64 lines (insufficient slack for re−execution)Fig.1.Affection of the cache size on reliabilityare used to correct faulty executions,the cache’s influence on the task execution times will also affect the number of possible re-executions,hence affecting the system’s reliability.For ex-ample,in Fig.1(a),if we reduce the cache size from 256lines to 128and 64lines (Fig.1(b)and (c)),the number of faults in the active cache area decrease from 3to 2and 1,respectively.However,the smaller cache sizes result in prolonged task ex-ecution times,which,in turn,change the amount of slack left for re-executions.The aim of this paper is to examine the combined effect of cache size selection on energy consumption,reliability and performance.To the best of our knowledge,this is the first investigation into the interaction between cache energy con-sumption and transient faults from an cache size perspective.We perform extensive fault inject simulations on five com-monly used benchmarks,using a cycle-accurate microproces-sor simulator.The experiments demonstrate that there exists a complex trade-off between the different objects.Ultimately,this trade-off can be exploited through dynamic cache resizing (enabling/disabling portions of the cache)at application run-time.The remainder of this paper is organized as follows.We in-troduce the models of the transient faults,the cache performa-bility and the cache energy in Section II.The simulation setup and results analysis are in Section III.Concluding remarks are given in Section IV.II.P RELIMINARIESA.Transient fault modelTransient faults within the cache are mainly caused by al-pha particles hitting the flip-flops of the cache [9,17].The physical procedure of the particle-hits causing faults is com-plex and the effect depends on many factors,like the energy transferred from the particle into the circuit,the transistor size,etc.[18].In this paper,however,we are not directly interested in the combined circuit and particle properties that can lead to transient faults,but rather in the effect of the transient faults within the cache on the task execution result with respect to performance,energy and reliability.Thus we will use the bit-flip as the transient fault model,i.e,when an alpha particle hits a flip-flop,the value stored in it changes its value from 1to 0or vice versa [19].The arrival process of the transient faults is typically modeled as a Poisson process with an average faultrate[13,14].With the arrival of a transient fault,each flip-flop in the cache has an equal probability to be hit since alpha particles are uniformly distributed over the circuit area.Of course,the transient faults can also occur in other parts of the processor (e.g.registers)and cause errors.However,the number of registers in modern microprocessor is far below the number of cache memory cells and it was pointed out in [21]that more than 90%of errors in a processor are originating from the transient faults in the cache.Therefore,we will focus throughout this paper on transient faults in the cache.When a transient fault occurs in the cache,though the value in a certain flip-flop is corrupted,this does not necessarily manifest in an error,that is,the computational result can still be correct.For example,when the transient fault happens in a tag array and the processor wants to read the corresponding cache line,the ef-fect may be just one read miss causing a read from the external memory.Nevertheless,the overall correctness of the computa-tion is not jeopardized.Even when a transient fault happens in a data array of the cache,it is possible that the corrupted value in the data array is overwritten due to a cache write from the processor or a data read from the memory to the cache before it is propagated into the data path of the processor so that the fault is masked.Hence,one important factor that characterizes the system’s vulnerability is the ratio between the errors and transient faults.We define the vulnerability factor (VF)as thisratio.Further,we define the error rateas the product of VF and the fault rate,i.e.,.The error rate will be used in Section II.B to compute the performa-bility of the cache.Though the fault rate is independent of the cache size (3faults appear in all cache configurations of Fig.1),we can find that VF is actually a function of the cache size from the simulation results (see Section III.B),so the er-ror rate as well as the performability both depend on the cache size.We will outline how to obtain VF through fault injection experiments in Section III.A.B.Performability modelFor real-time systems,the most important criterion of the system performance is whether the processor can finish execut-ing a task within a given deadline.More specifically,suppose the processor needs cycles to execute a task and the proces-sor frequency is ,if the deadline before which the task shouldcomplete is,then the performance requirement is.In the case that the taskfinishes execution before the deadline ,then there exists a slack.For example,Fig.1(b)shows the task execution for a cache size of128lines.As we canobserve,it takes cycles to execute the task,leaving a slack of.This slack time can be utilized to increase the system’s reliability against transient faults by performing roll-back recoveries(re-execution)when errors occur[14].That is, in the presents of an error,the task is re-executed with the aim to achieve a non-faulty run.Nevertheless,since re-executions require time,the number of possible re-executions is limited by the amount of slack.Accordingly,the number of possible re-executions is given by:(1)For instance,in Fig.1(a),the slack is large enough to per-form two re-executions(=2),when needed.The number of possible re-execution,however,decreases as the cache size is reduced.For instance,in Fig.1(b)and(c)the number of re-execution is and,respectively.Since the appearance of transient faults follows a Poisson distribution,the probability of at least one error during the ex-ecution of a task is[14]:(2) We use a combined metric called performability to measure the system performance and reliability together[13,14].Here,the performability is defined as the probability offinishing the task correctly within the deadline in the presence of faults[14]. Based on Eqs.(1)and2,the performability can be expressed by[14]:(3) The clock cycles that the processor needs to execute a task is heavily impacted by the cache size.The direct result is that ,the number of possible re-executions,will be different for different cache sizes.Also,as outlined in Section III.A,the error rate is a function of the cache size.As a result,the performability is fundamentally impacted by the cache size. As our experimental results indicate(Section III),a careful se-lection of the cache size is of utmost importance to achieve the required performance and reliability.C.Cache energy consumptionThe energy dissipated in the cache is comprised by a static and a dynamic component.Static energy is caused by leak-age currents in the CMOS circuit,while dynamic energy is mainly due to the charging and discharging of the load capac-itance which are driven by switching gates.Dynamic energy consumption consists of most of the total energy dissipation in level one caches[16],hence we only consider the dynamic energy of the cache here.Cache energy is dissipated during read as well as write accesses.Write accesses include the nor-mal write accesses and the cache line replacements after cache misses.Accordingly,the cache energy is given by:(4)Tag DataValid12L12MYX. . .. . .Fig.2.Position of fault injection:instruction cachewhere and are the numbers of the cache read access and write access respectively,while andare the energy consumed during one cache read access and one cache write access,respectively.Both and de-pend on the cache size since the cache hit rates are generally different for different cache sizes.Furthermore,the energy per access,as well as,is also cache size dependent. The main reason is that different memory wire lengths have different capacitances to be charged[23].III.S IMULATIONS AND EXPERIMENTAL RESULTSA.Simulation setupIn order to study the impacts of the cache size on performa-bility and cache energy,we use a simulation-based approach. The experimental platform is MPARM[24],a cycle-accurate simulator that includes an ARM7microprocessor model.The simulator reports detailed information regarding the number of clock cycles used to execute a benchmark as well as the energy consumed within the cache.The cache size of MPARM can be configured from32bytes up to1M bytes(10241024)with the constraint that the size must be a power of2.The cache line size isfixed to16bytes.In our simulation,we use separated data cache and instruction cache,and both have a maximum size of256K bytes(2561024).Cache memory accesses require one clock cycle,while accesses to the main DRAM memory are conservatively assumed to take100clock cycles [22].Two way set-associativity is used for the data cache.The instruction cache is direct-mapped.Although the associativity of the cache is configurable,we do not change the cache as-sociativity in our simulations,since our main focus is on the cache size.We conduct the fault injection experiments to determine the vulnerability factor(Section II.A)of different cache con-figuration forfive commonly used benchmark applications, namely,afixed point FFT(FPFFT)with a1024points dis-crete sinewave as input,a cyclic redundancy check(CRC)with 300ASCII characters as inputs,a88matrix multiplication (MM),a1212matrix addition(MA)and a100integer quick sort algorithm(QSORT).In order to obtain accurate vulnera-bility factors,we inject faults for each benchmarks.Each fault is injected in the following way:Two independent ran-dom variables and are used to decide the position of the fault injection in the cache,as illustrated in Fig.2.The ran-dom variable is uniformly distributed between1and,the number of lines in the cache.Accordingly,decides in which line the fault will be injected.The random variable is uni-(a)(b)(c) 01e+062e+063e+06 4e+06 5e+066e+064 6 8 10 12 14 16 18d a t a c a c he e n e r g y (p J )cache sizedata cache energy2e+064e+06 6e+068e+06 1e+07 1.2e+07 1.4e+071.6e+071.8e+074681012141618c l o c k c y c l e scache sizeclock cycles0.02 0.04 0.06 0.08 0.1 0.120.14 4 6 8 10 12 14 1618v u l n e r a b i l i t y f a c t o rcache sizevulnerability factorFig.3.FPFFT simulation results:data cacheformly distributed between 1and ,the number of bits in a line,to decide which bit in the line will flip its value.This de-termines if the flipped bit belongs to the valid bit,the tag array or the data array.Fig.2shows the case for the direct-mapped instruction cache,the fault position in the two way data cache is decided in a similar way,only that is uniformly distributed between 1and 2.When is less than ,the fault is within set 0;otherwise,the fault is within set 1.According to the val-ues ofand ,we check whether the selected memory cell falls within the disabled cache region.If so,the fault injection will definitely not cause an error and a simulation run is unnec-essary.On the other hand,if a memory cell within the enabled cache is selected,then the injected fault might manifest in an error,i.e.,the simulation has to be performed to observe the effect of the injected fault.Before the simulation is performed,we also randomly determine the clock cycle of the task ex-ecution during which the fault will be injected ().After a simulation has finished,we compare the outcome with the expected outcome to see if the injected fault resulted in an error.The number of errors is counted and divided by the num-ber of injected faults ()to obtain the vulnerability factor.B.Experimental resultsIn the first set of experiments,we concentrate on the data cache and the results obtained for the FPFFT benchmark.Fig.3shows the outcomes of the experiments.The three graphs give the energy dissipation,the number of clock cy-cles and the vulnerability factor as a function of the cache size.Note that the cache size in the figures is the logarithm of the true cache size,e.g.,cache size 10means the true cache sizeisbytes.As we can observe from Fig.3(a),the optimal cache energy consumption for the FPFFT benchmarkis obtained for a cache size ofbytes.It is interesting to see that the cache energy increases for smaller sizes.The main rea-son for this behavior is the high miss rate for smaller caches,which consequently results in a large number of cache line replacements.This increases the number of cache accesses (read/write accesses +replacement accesses).Although the energy per cache access increases when the cache size gets larger,the number of cache accesses drops relatively faster and the overall effect is a decreasing energy consumption.Whenthe cache size is abovebytes,the number of the cache ac-cesses reduces slower and becomes fixed after the cache size isgreater thanbytes.However,the energy per cache access continuously increases with the cache size increasing.This is mainly due to the fact that the address/data lines in the cache become longer and hence a larger capacitance has to beTABLE IPERFORMABILITY FORFPFFT:DATA CACHEcache sizenumber of 9’sdigits after 95689742667410676599748125299891669592102681057112652011122639275132634412142630301152648551162640212172627900182642730charged for the accesses.As a result,the energy curve of the cache rises after the cache size is larger than bytes.The processor clock cycles used to execute the benchmark is depicted in Fig.3(b).As we can see,with increasing cache size the miss rate drops and the clock cycles decrease quickly.Clearly,less cache misses cause less time-consuming main memory accesses so that the total clock cycles are reduced.Nevertheless,once the cache size is abovebytes,the clock cycles do not change any more.This is due to the fact that the application can not facilitate the extra cache and the increasing cache size will not further reduce the cache miss rate.Fig.3(c)shows the vulnerability factor (VF)as a function of the cache size.It shows an opposite trend when compared to the clock cycle curve of Fig.3(b).This can be explained as follows.If the active cache portion is increasing,also an increasing number of the uniformly distributed transient faults will hit this active area,hence causing more errors.However,when the cache size has exceededbytes,the FPFFT bench-mark does not take advantage of additional cache and the pro-cessor will not access the additional cache lines.Hence,as the cache becomes larger and larger,although more and more tran-sient faults fall into the cache,the number of those hitting the accessed lines of the cache does not change significantly.As a result,the VF curve becomes saturate when the cache sizeexceedsbytes.Having obtained the clock cycles and vulnerability factor,we can now use Eq.3to compute the performability for each cache size.The deadline for the FPFFT benchmark is 80.9ms,which is the execution time of the benchmark when the cache size is minimum (bytes).The performability results are given in Table I.Note that the performability is actually a prob-ability,with a desired value of as close as possible to 1.To ease the comparison we report the results by the number of 9s af-ter the decimal point (Column 2)and five more digits after the(a)(b)(c) 0 5000001e+06 1.5e+06 2e+06 2.5e+06 3e+06 3.5e+06 4e+064.5e+06 4681012141618d a t a c a c he e n e r g y (p J )cache size data cache energy 02e+064e+06 6e+06 8e+06 1e+071.2e+07 1.4e+074681012141618c l o c k c y c l e scache sizeclock cycles 00.050.10.150.20.250.34 6 8 10 12 14 1618v u l n e r a b i l i t y f a c t o rcache sizevulnerability factorFig.4.CRC simulation results:data cache(b)(a)(c) 05e+061e+071.5e+07 2e+072.5e+07 3e+073.5e+074e+074.5e+074 6 8 10 12 14 1618c l o c k c y c l e scache sizeclock cycles 05e+061e+071.5e+072e+072.5e+074 6 8 10 12 14 1618i n s t r u c t i o n c a c h e e n e r g y (p J )cache sizeinst. cache energy 00.010.020.030.040.050.064 6 8 10 12 14 1618v u l n e r a b i l i t y f a c t o rcache sizevulnerability factorFig.5.FPFFT simulation results:instruction cachelast 9(Column 3).As we can observe,when the cache size is smaller than bytes,though the VF value is small (Fig.3(c)),the execution time is relatively long due to the large number of clock cycles (Fig.3(b)).As a result,there is not enough slack for the re-execution so that the performability becomes low.With increasing cache size,the execution time reduces and there is more slack left for re-executions,even though the VF value increases,the performability still improves.This il-lustrates that compared to VF,slack time is more important to improve the performability for this benchmark.After the sizereachesbytes,the difference between each performability value is marginal and the number of 9s remains the same.FromTable I,it can be found that with the cache size ofbytes,we can achieve the best performability.Taking the energy curve of Fig.3(a)into consideration,we can find that selecting a cachesize larger thanis not a good choice because it is not energy efficient and the performability will not be improved.Clearly,for the FPFFT benchmark,bytes is the optimal cache size with which the cache energy is minimal and the performability is maximal.The next set of experiments is concerned with the CRC benchmark,for which we performed the same evaluations as for the FPFFT benchmark.The deadline of the CRC bench-mark is at 69.4ms.Fig.4and Table II show the experimental results.When comparing Figs.3and 4as well as Tables I and II,we can notice similar trends,however,we should note some important difference.For CRC the cache energy is mini-mal when the cache size is bytes while the performability ismaximal when the cache size isbytes.That is,as opposed to FPFFT,there is a Pareto-optimal set of the cache sizes:,.The decision of the cache size selection can be made according to the system requirement.For safety-critical sys-tems,we should selectbytes to achieve the highest per-formability;for systems with tight energy budget,e.g.some battery powered systems,the cache size should be selected asTABLE IIPERFORMABILITY FORCRC:DATA CACHEcache sizenumber of 9’sdigits after 95733991667516076602768257814293175245103687705113683265123631894133587930143586913153589884163517656173589517183503286bytes.Due to space limitations,we do not report here the de-tailed results of the matrix multiplication (MM),matrix addi-tion (MA)and quick sort algorithm (QSORT).Nevertheless,the general trends of these benchmarks follow observations made for the FPFFT and CRC benchmarks.Overall these benchmarks have optimal data cache sizes for MM,MA andQSORT of,and ,respectively.Since the above given experimental results concentrated on the data cache,we have conducted additional experiments for the instruction cache.The results of the FPFFT benchmark are given in Fig.5and Table III.The energy curve reaches the lowest point at the cache size of bytes.In Table III,we can find the performability is maximum when the cache size is bytes.However,since the performability at size is very close to the maximum value and the number of 9s at size is the same as that of size ,we can choose and as the Pareto-optimal set of the cache size.The experimental results for the other four benchmarks on the instruction cache follow a similar trend and details are omitted due to space limitations.Nevertheless,for the MAand QSORT benchmarks,there are Pareto-optimal sets:,TABLE IIIPERFORMABILITY FOR FPFFT:INSTRUCTION CACHEcache size number of9’s digits after95548157648002374178008124591094019101106475657116479140126485160136486659146469409156483935166467832176480194186483067and,,respectively.For the MM and CRC bench-marks the optimal cache sizes are and,respectively. Summarizing,we can draw the following conclusion from the above experimental results.There exist optimal or Pareto-optimal cache size choices with respect to performability and energy consumption.Depending on the application require-ment a proper cache size should be selected to achieve the opti-mal energy and performability simultaneously or the best trade off.Furthermore,as the optimal cache sizes depend largely on the running application,dynamically changing the cache size to suit the particular application is not only beneficial from an energy point of view but also to improve the system’s per-formability.For instance,when running the FPFFT benchmark after the MA benchmark,the processor’s data cache should be adapted from to bytes and the instruction cache should be changed from to bytes.This adaption would reduce the data cache energy by2.6%and increasing the performa-bility from sixteen9s to twenty-six9s.The instruction cache would reduce its energy by8.8%and improve the performabil-ity from twelve9s to forty9s.IV.C ONCLUSIONSIn this paper,we studied the impact of the cache size se-lection on three important design objectives,namely,the sys-tem performance,the cache energy consumption and the cache reliability,which has not been addressed explicitly in previ-ous work.Performability has been defined to combine the analysis of the performance and the reliability.We have con-ducted extensive experiments to analyze the interplay between the three objects.These experiments were performed using cycle-accurate processor simulations and it was found that the cache size selection affects not only the energy but also the performability.The results indicate that a careful cache size selection is needed,in order to take advantage of the found optimal energy/performability trade-off points.R EFERENCES[1]J.L.Hennessy,D.A.Patterson,Computer Architecture:A QuantitativeApproach,2nd Edition,Morgan Kaufmann Publishing Co.1996[2] C.Zhang,F.Vahid and R.Lysecky,“A self-Tuning Cache Architecturefor Embedded Systems”,in Proc.of DATE,2004.[3] C.Zhang,F.Vahid,W.Najjar,“A Highly Configurable Cache Architec-ture for Embedded Systems”,in Proc.of International Symposium on Computer Architecture,2003.[4]S.Dropsho et al.,“Integrating Adaptive On-Chip Storage Structures forReduced Dynamic Power”,in Proc.of the International Conference on Parallel Architectures and Compilation Techniques,2002.[5] D.H.Albonesi,“Selective cache ways:On-demand cache resource allo-cation”,in Proc.of International Symposium on Microarchitecutre,1999.[6]M.Powell A.Agaewal,T.Vijaykumar,B.Falsafiand K.Roy,“ReducingSet-Associative Cache Energy via Way-Prediction and Selective Direct Mapping”,in Proc.of International Symposium on Microarchitecture, 2001.[7] A.C.Nacul and T.Givargis,“Dynamic V oltage and Cache Reconfigura-tion for Low Power”,in Proc.of DATE04,March,2004.[8]S.Yang,M.D.Powell, B.Falsafi,T.N.Vijaykumar,“ExploitingChoice in Resizable Cache Design to Optimize Deep-Submicron Pro-cessor Energy-Delay”,in Proc.of International Symposium on High-Performance Computer Architecture,2002.[9]G.Asadi,V.Sridharan,M.B.Tahoori,D.Kaeli,“Balancing Performa-cne and Reliability in the Memory Hierarchy”,in Proc.of International Symposium on Performance Analysis of Systems and Software,2005.[10]L.Li,V.Degalahal,N.Vijaykrishnan,M.Kandemir,M.J.Irwin,“SoftError and Energy Consumption interations:A Data Cache Perspective”, in Proc.of ISLPED04,Aug.2004.[11]S.Kim and A.K.Somani,“Area Efficient Architectures for InformationIntegrity in Cache Memories”,in Proc.of International Symposium on Computer Architecture,1999.[12]W.Zhang,S.Gurumurthi,M.Kandemir,A.Sivasubramaniam,“ICR:in-cache replication for enhancing data cache reliability”,in Proc.of In-ternational Conference on Dependable Systems and Networks,2003. 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船舶零配件英语
一.职位及工种(Titles and type of work) 1.船长 Captain 2.大副 Chief officer 3.二副 Second officer 4.三副 Third officer 5.四副 Fourth officer 6.水手长 Boatswain 7.水手 Sailor & Seaman 8.木匠 Carpenter 9.轮机长 Chief engineer 10.大管轮 Second engineer 11.二管轮 Third engineer 12.三管轮 Fourth engineer 13.机匠长 Chief motorman 15.机匠 Fitter 16.加油工 Oil man 17.大电 Chief electrician 18.电工 Electrician 19.车间主任 Workshop director 20.工长 Section chief 21.班长 22.钳工 23.主管工程师24.机务&船东 Superintendent &Super &Owner 25.助理工程师 Assistant engineer 26.验船师(机)Register 27.验船师(船)Surveyor 28.油漆工 Painter 29.焊工 Welder 30.大橱 Chief cook31.物料员 Store keeper 32.加油工 Oiler33.机工 Mechanic 34.甲板员 Deck man 35.电线工 Wireman 36.外包工 Laborer 37.铸工 Molder 38.管子工 Pipe fitter 39.起重工 Crane operator二、柴油机类(Words about diesel engine) 1.主机 Main engine2.二冲程柴油机 Two-stroke diesel engine 3.四冲程柴油机 Fore-stroke diesel engine 4.高速柴油机 High speed diesel engine 5.中速柴油机 Middle speed diesel engine 6.低速柴油机 Low speed diesel engine 7.气缸盖(缸头) Cylinder head 8.安全阀 Safety valve 9.释放阀 Relief valve 10.示功阀 Indicator valve 11.示功考克 Indicator cock 12.空气起动阀 Air starting valve13.起动空气分配器 Air starting distributor 14.油头(燃油喷射器) Fuel injector 15.排气阀 Exhaust valve 16.气缸套 Cylinder liner17.冷却水套 Cooling water jacket 18.气缸注油器 Cylinder lubricator 19.活塞 Piston20.活塞头 Piston crown21.活塞裙 Piston skirt22.活塞销 Piston gudgeon pin 24.活塞杆 Piston rod 25.活塞环 Piston ring26.活塞环槽 Piston ring groove 27.压缩环 (气环) Compression ring 28.刮油环 (油环) Oil scraper ring29.减磨令 Wear ring (copper ring) 30.伸缩管(水拉管) Telescopic pipe31.活塞冷却空间 Piston cooling space 32.填料箱(函) Stuffing box33.填料箱密封环Sealing ring for Stuffing box 34.填料箱压缩环 Pressure ring for Stuffing box 35.填料箱刮油环 Scraper ring for Stuffing box 36.扫气箱 Scavenging receiver 37.扫气口 Scavenging port 38.排气口 Exhaust port 39.十字头 Cross head 40.十字头销 Crosshead pin 41.十字头轴承 Crosshead bearing 42.十字头滑块 Crosshead slipper 43.滑块 Guide shoe44.十字头导板 Crosshead guide plate 45.连杆 Connecting rod 46.连杆大端轴承 Bid end bearing 47.连杆小端轴承 Small end bearing 48.曲柄轴承 Crank bearing 49.曲柄销 Crank pin 50.曲轴 Crank shaft 51.曲轴颈 Crank journal52.曲柄臂Crank web53.拐档差Crank deflection54.主轴承Main bearing55.主轴颈Main journal56.轴承瓦Bearing bush57.上轴瓦Upper bearing bush58.上轴瓦Upper half59.下轴瓦Lower bearing bush60.下轴瓦Lower half61.推力轴承Thrust bearing62.推力块Thrust pad63.推力盘Thrust disc64.推力轴Thrust shaft65.底座Bed plate66.机架Frame67.曲柄箱Crank case68.曲柄箱导门Crank case door69.曲柄箱防爆门Explosion-proof Crank case. 70.定时齿轮Timing gear71.飞轮Flying wheel72.凸轮Cam73.凸轮轴Cam shaft74.喷油凸轮Fuel injection cam75.链条Chain76.链条轮Chain wheel77.链条箱Chain box78.推杆Push rod79.摇臂Rocker arm80.排气阀Exhaust valve81.吸气阀Suction valve 82.排气总管Exhaust manifold83.进气总管Air inlet manifold84.高压燃油管High pressure fuel pipe85.活塞冷却水管Piston cooling water pipe86.法兰Flange87.贯穿螺栓Tie bolt (tie rod)88.端盖Side cover89.滑油泵Lubricating oil pump90.燃油泵Fuel oil pump91.滑油泵齿轮Gear for lubricating oil pump92.燃油泵齿轮Gear for fuel oil pump93.叶轮Impeller94.柱塞Plunger95.导杆Guide rod96.导套Sleeve97.滚动轴承Ball bearing98.滑动轴承Sliding bearing99.推力滚动轴承Thrust ball bearing100.推力面Thrust surface (thrust side)101.盘车机Turning gear102.增压器Turbocharger103.涡轮机(透平)Turbine104.涡轮Turbine wheel105.涡轮叶片Turbine blade106.喷嘴Nozzle107.废气叶轮Exhaust impeller108.废气叶轮片Exhaust blade109.废气端Exhaust side110.透平端Turbine side111.转子轴Rotor shaft112.油泵L.O. pump113.换向装置Reversing device114.换向伺服期Reversing servomotor115.压气机(鼓风机) Blower116.膨胀接Expansion joint117.调速器governor118.飞重Flying weight119.补偿阀Compensate valve120.针阀Needle valve121.开口销Cotter pin122.轴封Shaft seal123.机械密封Machinery seal124.配电盘Switchboard125.应急配电盘Emergency switchboard126.应急发电机Emergency generator127.滤器Filter128.细滤器Filter129.粗滤器Strainer130.滑油滤器L.O. filter131.燃油滤器 F.O. filter132.空气消音器Air intake silencer132.空气滤器Air intake filter133.空气瓶Air bottle (receiver)134.分油机Separator135.油水分离器Water-oil separator136.净油机Purifier137.燃油净化器 F.O. purifier138.二氧化碳CO2139.二氧化碳瓶CO2 bottle140.正时齿轮Timing gear141.导向棒装置Guide bar142.注油器驱动Lubricator driver143.链条张紧装置Chain tightener144.凸轮轴传动轮Chain wheel on cam shaft 145.中间链链传动轮Intermediate chain wheel 146.注油器驱动装置Lubricator drive147.链条张紧装置Chain tightener148.滚筒导座Roller guide housing 149.应急操纵台Emergency console150.力矩平衡器Moment compensator 151.主启动阀Main starting valve152.启动空气分配器Starting air distributor 153.喷油器Fuel valve154.扫气系统Scavenge air system 155.安全帽Safety cap156.机座Bed plate157.轴向振动减振器Axial vibration damper 158.贯穿螺栓Arrangement of stay bolt 159.示功器驱动装置Indicator driver160.端罩End shields161.气缸架Cylinder frame162.气阀传动装置Valve operating device 163.摇臂润滑油泵Rocker arm lubricating oil pump 164.摇臂润滑油柜Rocker arm lubricating tank 165.摇臂润滑滤器Rocker arm lubricating filter 三、船舶机械类(Words about marine machinery)1.船用锅炉Marine boiler2.废气锅炉Exhaust boiler3.辅锅炉Donkey boiler4.组合式锅炉Combined boiler5.火管Fire tube6.给水管Feed pipe7.炉膛Furnace8.炉墙Furnace wall9.火侧Fire side10.水侧Water side11.燃烧器Oil burner12.安全阀Safety valve13.上排污Upper drain14.下排污Lower drain15.锅炉皮阀Mounting valve16.水位计Water level gauge17.压力表Pressure gauge18.主汽门Main steam valve19.玻璃管Glass tube20.空调装置Air-conditioning plant21.制冷装置Refrigerating plant22.冰机Fridge. Machine23.空气压缩机Air compressor24.造水机Fresh water generator25.板式冷却器Plate type cooler26.机舱天车Engine room crane27.天车导轨Crane rail28.电磁阀Solenoid valve29.舵机Steering gear30.舵承Rudder bearing carrier31.液压缸Hydraulic cylinder32.废气涡轮增压器Exhaust gas turbocharger33.弹簧阀Spring loaded valve34.冷凝器Condenser35.分油器Oil separator36.轴带发电机Shaft generator37.焚烧炉Oil burner38.分油机Separator39.分离筒Separator bowl40.配水盘装置Paring disc device41.转数计Revolution counter42.控制阀Control valve43.辅机Auxiliary machinery44.制冷装置Refrigerating plant45.海水淡化装置Sea water desalting plant46.热交换器Heat exchanger47.船用气瓶Marine air bottle48.冷风机Cooler unit49.防水风门Fire damper50.气密挡板Gas tight damper51.排气风机Exhaust fan52.舱室通风机Cabin fan53.机舱通风机Engine room fan54.应急鼓风机Emergency blower四、阀门(Words about valve)1.吸气阀Suction valve2.排气阀Exhaust valve3.控制阀Control valve4.导阀Pilot valve5.单向阀Non-return valve6.口琴阀Flap valve7.调节阀Regulating valve 8.液压阀Hydraulic valve9.膨胀阀Expansion valve 10.给水阀Feed valve11.排水阀Discharge valve 12.截止阀Stop valve13.吹泄阀Blow-off valve 14.空气阀Air valve15.泄放阀Drain valve16.止回阀Check valve17.海底阀Sea valve18.回流阀Retune valve19.节流阀Throttle valve20.进气阀Inlet valve21.出气阀Outlet valve22.热力阀Thermal valve23.中央阀Center valve24.单向阀One way valve25.二通阀Two way valve 26.三通阀Triple valve27.旁通阀By-pass valve28.换向阀Change-over valve 29.减压阀Pressure-reducing valve 30.溢流阀Overflow valve 31.自闭阀Self-locking valve 32.针阀Needle valve33.平衡阀Balance valve34.循环阀Circulation valve 35.主阀Main valve36.滑阀Slide valve 37.蝶阀Butter-fly valve38.截止阀Shut-off valve39.闸板阀Gate valve40.通海阀Sea suction valve41.吹除阀Sea chest cleaning valve42.防浪阀Storm valve43.舱壁阀Bulkhead valve44.快关阀Emergency shut off valve45.呼吸阀Breather valve五、泵类(Words about pump)1.电动泵Motor-driven pump2.柱塞泵Plunger pump3.叶片泵Vane pump4.回转泵Rotary pump5.齿轮泵Gear pump6.往复泵Reciprocating pump7.离心泵Centrifugal pump1.电动泵Motor-driven pump2.柱塞泵Plunger pump3.叶片泵Vane pump4.回转泵Rotary pump5.齿轮泵Gear pump6.往复泵Reciprocating pump7.离心泵Centrifugal pump8.真空泵Vacuum pump9.螺杆泵Screw pump10.喷射泵Ejector pump11.冷却泵Cooling pump12.淡水泵Fresh water pump13.海水泵Sea water pump14.给水泵Feed water pump15.循环泵Circulating pump16.锅炉给水泵Boiler feed pump17.卫生水泵Sanitary pump18.压载泵Ballast pump19.舱底泵Bilge pump20.污水泵Sewage pump21.燃油泵Fuel pump22.高压油泵High pressure pump23.底压油泵Low pressure pump24.驳运泵Transfer pump25.增压泵Booster pump26.消防泵Fire pump27.通用泵G.S. pump28.旋涡泵Regenerative29.蜗壳泵V olute pump30.导叶泵Diffuser pump31.单联泵Simplex pump32.双联泵Duplex pump33.多联泵Multiplex pump34.活塞泵Piston pump35.减摇泵Anti-roll pump36.总用泵General service pump37.应急消防泵Emergency fire pump38.扫舱泵Stripping pump39.货油泵Cargo oil pump40.滑油泵Lubricating oil pump六、甲板机械类(Deck machinery)1.锚机Windlass2.锚机轴Windlass shaft3.刹车带Brake lining4.离合器Clutch5.锚链轮Anchor Chain wheel6.轴承瓦Bearing bush7.轴承盖Bearing cover8.绞揽机Capstan9.系揽绞车Mooring winch10.卷缆车Reel11.钢丝绳Wire rope12.卡环Shackle13.缆绳Mooring rope 14.滑轮Block15.刹车装置Brake device 16.制链器Anchor chain stopper 17.舱盖滚轮Hatch cover wheel 18.舱盖铰链Hatch cover hinge 19.液压油缸Hydraulic jack 20.起货机Cargo winch 21.可令吊Crane22.生活吊Accommodation crane 23.吊杆Derrick boom 24.桅杆Mast25.救生艇Lifeboat26.艇架Davit27.艇机Lifeboat capstan 28.救生筏Life raft29.救生衣Life jacket七、工具类(Word about tools) 1.车床Lathe2.刨床Planing machine 3.钻床Drill machine 4.砂轮机Grinding machine 5.磨床Grinder6.铣床Milling machine 7.镗床Boring machine 8.手锤Engineer’s hammer 9.冲击板手Impact wrench 10.板手Spanner11.活络板手Screw spanner12.梅花板手Ring spanner13.呆扳手Open spanner15.套筒板手Socket spanner16.管子钳Pipe spanner17.螺丝刀Screw driver18.钢丝钳Wire pliers19.尖嘴钳Long nose pliers20.钢锯Hack saw21.剪刀Scissors22.手电筒Torch23.扁铲(凿子) Chisel24.锉刀File25.丝攻Thread tap26.板牙Thread die27.绞刀Reamer28.刮刀Scraper29.油石Oil stone30.拔子(拉马) Puller31.沙布Emery cloth32.破布Rag33.卷尺Measuring tape34.空心冲Hole punch35.样冲Joint punch36.油壶Oil gun37.牛油枪Grease gun38.手电钻Handle drill39.钻头Drill40.液压千斤Hydraulic jack.41.塞尺Feeler gauge42.游标卡尺Vernier caliper43.外卡尺Outside calipers44.内卡尺Inside calipers45.螺纹量规Screw gauge46.桥规Bridge gauge47.电焊机Electrode welding machine48.气焊机Gas welding machine49.电焊钳Electric welding pliers50.气割枪Cutting touch51.电焊条Electric soldering iron52.电工刀Electrician knife53.电笔Test pen54.剥线钳Wire stripping pliers55.圆规Compass56.量表Gauge57.拐档表Crank deflection gauge58.深度规Depth gauge59.千分表Micrometer gauge60.台虎钳Table vice61.柴油Diesel oil62.滑油Lubricating oil63.液压油Hydraulic oil64.重油Heavy oil65.燃油Fuel oil66.黄油Grease67.螺栓Bolt68.螺帽Nut69.垫片Washer70.研磨沙Grinding sand71.研磨膏Grinding paste72.石棉板Asbestos plate73.青壳纸Fish paper74.盘根Packing75.细钢丝Thin steel wire76.密封圈Rubber seal ring77.塑料管Plastic pipe78.胶皮管Rubber hose79.电灯泡Electric bulb80.工作灯Working lamp81.插头Electric plug82.插座Electric socket.93.喷砂机Sand blaster outfit94.空气马达Air motor95.油柜清洁器Tank cleaning machine96.高压冲水机High pressure hose for hydraulic 97.真空泵Vacuum pump98.套筒扳手组Socket wrench set99.深头套筒Deep socket wrench 100.套筒扳手Box wrench101.单开口扳手Single open end wrench 102.双开口扳手Double open end wrench 103.转矩扳手Torque wrench104.电动机扳手Motor wrench105.侧剪钳Slide cutting plier106.活节钳Combination plier107.可调快速扳手Speed wrench108.螺丝起子Screwdriver109.偏向螺丝起子Offset screw110.六角螺帽起子组Hexagon nut drivers set 111.手摇钻Straight hand drill112.手工锯Hacksaw frame113.锯片Hacksaw blade114.砂纸Silicon paper115.手拉葫芦Chain block116.高压管High pressure hose117.液压千金顶Hydraulic jack118.锤子Hammer119.平錾Cold chisel120.活动扳手Adjustable wrench121.螺丝刀Screwdriver122.侧剪铗Side cutting hipper123.螺栓剪Cable cutter124.敲击管钳Rap wrench125.砂轮Grinding wheel126.老虎钳Utility vise127.直梯Straight ladder128.踏梯Step ladder129.平台推车Platform trunk130.搬平车Gas cylinder carrier131.给油机Grease lubricator132.强力油泵Heavy duty pump oiler133.油壶Oil jag134.麻花钻Twist drill135.绞刀Pin reamer136.旋转中心钻Rolling center137.外径测微计Outside micrometer with counter138.六折式尺Six-folding rule139.弹性带尺Convex rule140.不锈钢直尺Stainless steel straight rule141.平面规Surface gauge142.平行直角定规Precision flat try square143.温度计Thermometer八、常用物料(Material in common use)1.阀研磨剂valve grinding compound2.电焊条steel electrode3.气焊条Steel welding wire4.细钢丝绳Seizing wire5.刚焊条Steel welding rod6.紫铜管Copper tube7.乙炔气瓶Acetylene cylinder8.木屑Saw dust9.水泥Cement10.石灰Lime11.帆布手套Canvas glove12.垫片Gasket.13.氧气瓶Oxygen cylinder14.抹布Rag15.垫隙片Shim16.电线Wire17.电缆Electric cylinder18.电池Rag19.灯泡Bulb20.胶布Insulating tape21.插头Plug22.插座Socket23.保险丝Fuse24.不锈钢Stainless steel25.铸铁Cast iron26.黄铜Brass27.青铜Bronze28.铝合金Aluminium alloy29.橡胶Rubber30.石棉Asbestus31.低碳钢Soft steel32.高碳钢High-carbon steel33.合金钢Alloy steel34.木材Wood35.塑料Plastic36.球墨铸铁Nodular iron九、常用紧固件(Part of fixation in common use) 1.螺栓Bolt2.螺丝Screw3.螺母Nut4.方头螺栓Sq head bolt5.埋头螺栓Counter sunk head screw 6.套筒螺栓Socket head bolt7.定位螺栓Set screw8.十字接头Cross9.锥形销Taper pin10.锁紧螺母Lock nut11.六角头螺栓Hex head bolt十、常用油类(Oil in common use)1.汽油Gas oil2.煤油Kerosene3.润滑油Lubricating oil4.汽缸油Cylinder oil5.压缩机油Compressor oil6.齿轮油Gear oil7.机油Motor oil8.凡士林Vaseline9.燃油Fuel oil10.油脂Grease11.柴油Diesel oil十一、常用量词(Quantifier in common use) 1.件,只,个Piece2.条,张,片Sheet3.双Pair4.套,组,副Set.5.盒Box6.箱Case7.瓶Bottle8.米Meter9.厘米Centimeter10.毫米Millimeter11.公斤Kilogram12.克Gram13.公升Liter14.平方Square15.袋Bag16.码Yard17.吨Ton18.磅Pound19.加仑Gallon20.立方Cubic十二、国家名称(Name of country)1.中国China2.美国American3.日本Japan4.英国Britain5.法国France6.德国German7.韩国South Korea8.希腊Greece9.泰国Thailand10.印度India11.挪威Norway12.俄罗斯Russia13.新加坡Singapore14.澳大利亚Australia15.伊朗Iran16.丹麦Denmark17.加拿大Canada18.丹麦Denmark19.芬兰Finland20.巴基斯坦Pakistan21.意大利Italy十三、常用缩语(abbreviation in common use)1.主机M/E2.付机A/E3.阀V/V4.泵P/P5.备车St/by6.完车 F.W.E.7.前进三FAHD8.微速后退 D.S.Ast9.前进二H.Ahd10.高压H.P.11.低压L.P.12.重油/柴油H.O./D.O.13.前后F/A14.左舷P: port15.无人机舱UMS16.自动Auto17.气缸Cyl18.燃油柜 19.滑油柜20.沉淀柜.21.排出Disc22.吸入Suct23.柴油柜 十四、船用动态常用单词(marine tends word)1.停靠Alongside2.接近Approach3.停泊Berth4.浮筒Buoy5.码头Pier6.港口Port7.移泊Shift8.航次V oyage9.试验Try10.值班Watch11.航行Sail十五、船舶机电设备操作词汇(manipulate of marine equipment)1.调整Adjust2.压载Ballast3.转换Change over4.清洁Clean5.联接Connect6.排放压载Deballast7.放残水Drain8.卸载Off9.油漆Paint10.接通Put on11.吹灰Soot blown12.开始Start13.顶端Top14.洗Wash15.吹Blow16.检查Check 17.铲Chip18.断开Cut out19.排放Discharge20.除垢Descale21.检验Examine22.受载On(load)23.用泵排出Pump out24.调整Set25.停止Stop26.调驳Transfer27.加满Top up十六、故障常用单词(words about malfunction)1.失常的Abnormal2.烧坏Burn3.堵塞Clog4.裂缝Crack5.变形Deform6.毁坏Destroy7.磨损Wear8.出故障In trouble9.敲击Knock10.松开Loose11.不对中Misalign12.不足的Insufficient13.失灵Out of order14.过载Overload15.过度磨损Over-worn16.尺寸过大Oversized17.尺寸过小Under-sized18.振动Vibrate19.不平的Uneven20.不准确Inaccurate21.全船断电Black out22.出故障Fail23.关掉Shut off24.弯曲Bend25.停车Break drown26.腐蚀Corrode27.腐蚀的Corrosive28.损坏Damage29.有毛病的Faulty30.有缺陷的Defective31.破裂Fracture32.卡住Jam33.漏泄Leak34.漏泄的Leaky35.融化Melt36.噪声Noise37.过热Overheat38.咬住Seize39.紧的Tight40.松的Loosen41.发现Find42.停止Stop43.脏的Dirty44.油污的greasy45.失效的ineffective46.椭圆形的oval47.点不着火misfire48.接错misjoin49.放错misplace50.老化perish51.麻点pit52.凸起ridge53.划伤score54.拉痕scuff十七、保养检修常用词汇(Words about maintain and examination)1.卡死Blind2.用卡钳量Caliper3.关闭Close4.解体Disassemble5.安装Fix6.组装Box up7.检验Check8.拆卸Dismantle9.装配Fit10.紧固Fasten11.测量Gauge12.安装Install13.测量Measure14.打开Open15.上油漆Paint16.换新Renew17.上紧Tighten18.洗Wash19.涂油脂Grease20.松开Loosen21.加油Oil22.检修Overhaul 23.重新组装Reassemble24.测取读数Take reading25.拧开螺栓Unbolt26.抽出Withdraw十八、常用数字(Numeral in common use)一One二Two三Three四Four五Five六Six七Seven八Eight九Nine十Ten十一Eleven十二Twelve十三Thirteen十四Fourteen十五Fifteen十六Sixteen十七Seventeen十八Eighteen十九Nineteen二十Twenty三十Thirty四十Forty五十Fifty六十Sixty七十Seventy八十Eighty九十Ninety百Hundred千Thousand万Ten thousand百万Million第一First第二Second第三Third第四Fourth第五Fifth第六Sixth第七Seventh第八Eighth第九Ninth第十Tenth第十一Eleventh第十二Twelfth第二十Twentieth十九、时间、季节与方向(Time、Season andDirection)1.星期一Monday2.星期二Tuesday3.星期三Wednesday4.星期四Thursday5.星期五Friday6.星期六Saturday7.星期日Sunday8.春季Spring9.夏季Summer10.秋季Autumn11.冬季Winter12.一月January13.二月February14.三月March15.四月April16.五月May17.六月June18.七月July19.八月August20.九月September21.十月October22.十一月November23.十二月December24.小时Hour25.分钟Minute26.秒Second27.月Month28.天Day29.夜Night30.周Week31.早晨、上午Morning32.下午Afternoon33.傍晚Evening34.正午Noon35.今天Today36.昨天Yesterday37.明天Tomorrow38.前天The day before yesterday 39.后天The day after tomorrow 40.本周This week41.上周Last week 42.下周Next week43.九月十日Sep.10th44.去年Last year45.明年Next year46.上周二Last Tuesday47.下周一Next Monday48.东East49.西West50.南South51.北North52.西北Northwest53.东北Northeast54.东南Southeast55.西南Southwest56.世纪Century二十、常用词组(Phrases in common use)1.发现已无法修复found beyond repair2.发现尺寸过大found over-sized3.发现反应缓慢found slow function4.发现不正常found out of order5.发现不合标准found not up to standard6.发现不准确found inaccurate7.发现失去作用found out of function8.发现轧住found seized9.发现过热found overheated10.发现过度磨损found excessive wear11.发现过度磨掉found worn out12.发现有一点倾斜found a little bit inclined13.发现不正常found abnormal14.发现因过热而损坏found destroyed byoverheating15.发现龟裂found chapped16.发现塌陷found collapsed17.发现运转失灵found out of operation18.发现呈椭圆形found oval19.发现拉痕found scored20.发现拉毛found scuffed21.发现变形found deformed22.发现松动found loose23.发现油污found greasy24.发现肮脏found dirty25.发现咬住found stuck26.发现挤压found squeezed27.发现弯曲found bent28.发现故障found faulty29.发现损坏found damaged30.发现破碎成片found broken to pieces31.发现部分剥离found partly detached32.发现部分堵塞found partly choked33.发现剧烈震动found violent vibration34.发现烧坏found burnt35.发现断裂found fractured36.发现接地found earthed37.发现敲缸found knocking38.发现溶化found melted away39.发现泄漏found leaking (found leaky)40.发现冻结found stuck fast by icing41.发现锈蚀found rusty42.发现失效found ineffective43.发现故障found out of order44.发现结霜found frosted45.发现丢失 found lost46.发现出故障 found in trouble 47.发现失灵 found out of order 48.发现失灵 found out of action 49.发现不一致 found out of operation 50.发现错位 found out of place 二十一、常用动词和例句(Verb in common use and example)1.借 borrow我要向你借这份图纸I want to borrow the drawing from you. 我可以向你借这个手锤吗?May I borrow the hammer from you? 2.裂 break 阀杆断裂了The valve spindle is broken. 滚动轴承断裂成碎片了The ball bearing are broken to pieces. 3.加强 build up 叶轮应该堆焊The impeller should be built up by welding. 4. 烧 burn电动机烧了 The motor is burnt. 5. 进行 carry out 应进行负载试验The load test should be carried out. 6.吹blow管子必须用压缩空气吹清The pipe should be blown with compressed air. 7.铸 cast按原样铸造一个8.引起 cause损坏是有剧烈振动引起的The damage was caused by violent vibration. 9.倒角 chamfer油槽须倒角 Oil groove is to be chamfered. 法兰切削后须倒角The flange should be chamfered after being machined.10.换掉 change把它们换掉,否则我拒绝验收Have them changed, otherwise I refuse to accept them.11.龟裂 chap轴瓦上的白合金龟裂了The white metal on the bearing bush is chapped. 12.核查 check用桥规核查主轴承Check the main bearing with bridge gauge. 修理前后要核查拐档差Check the crankshaft deflection before and after repair.13.清洁 clean装前须清洁 Clean it before fit back. 14.阻塞 clog燃油滤器阻塞了 The fuel filter is clogged. 15.涂漆 coat用红丹涂管子 Coat the pipe with red lead. 泵壳里涂防护漆The pump casing is to be coated with anti-fouling. 16.完成 complete finish 你什么时候能完成修理工作?When can you complete (finish) the repair job? 17.连接 connect把电动机和淡水泵连接起来Connect the motor with the fresh water pump18.腐蚀 corrode泵壳和叶轮均有腐蚀The pump casing and impeller are corroded. 19.盖 cover请把所有卸下的部件盖起来Please cover all the removed parts. 20.裂二号缸头裂开穿透至冷却水空间No.2 cylinder head is cracked. 21.吊 crane把液压马达吊上岸去修理Crane the hydraulic motor ashore for repair. 22.割 cut 把底座割掉Cut off the bedplate. 23.损坏 damage 滚动轴承严重损坏The ball bearings are seriously damaged. 24.脱落 detach白合金部分脱落了The white metal is partly detached. 25.查看 detect查看氟里昂系统有无泄漏 Detect the Freon system for leakage. 26.解体 disassemble解体,清洁并检查高压油泵Disassemble, clean and check the H.P. fuel pump. 27.脱开 disconnect 把起动空气管脱开Disconnect the starting air pipe. 将发电机与原动机脱开。
Glider Flying Handbook说明书
Glider Flying Handbook2013U.S. Department of TransportationFEDERAL AVIATION ADMINISTRATIONFlight Standards Servicei iPrefaceThe Glider Flying Handbook is designed as a technical manual for applicants who are preparing for glider category rating and for currently certificated glider pilots who wish to improve their knowledge. Certificated flight instructors will find this handbook a valuable training aid, since detailed coverage of aeronautical decision-making, components and systems, aerodynamics, flight instruments, performance limitations, ground operations, flight maneuvers, traffic patterns, emergencies, soaring weather, soaring techniques, and cross-country flight is included. Topics such as radio navigation and communication, use of flight information publications, and regulations are available in other Federal Aviation Administration (FAA) publications.The discussion and explanations reflect the most commonly used practices and principles. Occasionally, the word “must” or similar language is used where the desired action is deemed critical. The use of such language is not intended to add to, interpret, or relieve a duty imposed by Title 14 of the Code of Federal Regulations (14 CFR). Persons working towards a glider rating are advised to review the references from the applicable practical test standards (FAA-G-8082-4, Sport Pilot and Flight Instructor with a Sport Pilot Rating Knowledge Test Guide, FAA-G-8082-5, Commercial Pilot Knowledge Test Guide, and FAA-G-8082-17, Recreational Pilot and Private Pilot Knowledge Test Guide). Resources for study include FAA-H-8083-25, Pilot’s Handbook of Aeronautical Knowledge, FAA-H-8083-2, Risk Management Handbook, and Advisory Circular (AC) 00-6, Aviation Weather For Pilots and Flight Operations Personnel, AC 00-45, Aviation Weather Services, as these documents contain basic material not duplicated herein. All beginning applicants should refer to FAA-H-8083-25, Pilot’s Handbook of Aeronautical Knowledge, for study and basic library reference.It is essential for persons using this handbook to become familiar with and apply the pertinent parts of 14 CFR and the Aeronautical Information Manual (AIM). The AIM is available online at . The current Flight Standards Service airman training and testing material and learning statements for all airman certificates and ratings can be obtained from .This handbook supersedes FAA-H-8083-13, Glider Flying Handbook, dated 2003. Always select the latest edition of any publication and check the website for errata pages and listing of changes to FAA educational publications developed by the FAA’s Airman Testing Standards Branch, AFS-630.This handbook is available for download, in PDF format, from .This handbook is published by the United States Department of Transportation, Federal Aviation Administration, Airman Testing Standards Branch, AFS-630, P.O. Box 25082, Oklahoma City, OK 73125.Comments regarding this publication should be sent, in email form, to the following address:********************************************John M. AllenDirector, Flight Standards Serviceiiii vAcknowledgmentsThe Glider Flying Handbook was produced by the Federal Aviation Administration (FAA) with the assistance of Safety Research Corporation of America (SRCA). The FAA wishes to acknowledge the following contributors: Sue Telford of Telford Fishing & Hunting Services for images used in Chapter 1JerryZieba () for images used in Chapter 2Tim Mara () for images used in Chapters 2 and 12Uli Kremer of Alexander Schleicher GmbH & Co for images used in Chapter 2Richard Lancaster () for images and content used in Chapter 3Dave Nadler of Nadler & Associates for images used in Chapter 6Dave McConeghey for images used in Chapter 6John Brandon (www.raa.asn.au) for images and content used in Chapter 7Patrick Panzera () for images used in Chapter 8Jeff Haby (www.theweatherprediction) for images used in Chapter 8National Soaring Museum () for content used in Chapter 9Bill Elliot () for images used in Chapter 12.Tiffany Fidler for images used in Chapter 12.Additional appreciation is extended to the Soaring Society of America, Inc. (), the Soaring Safety Foundation, and Mr. Brad Temeyer and Mr. Bill Martin from the National Oceanic and Atmospheric Administration (NOAA) for their technical support and input.vv iPreface (iii)Acknowledgments (v)Table of Contents (vii)Chapter 1Gliders and Sailplanes ........................................1-1 Introduction....................................................................1-1 Gliders—The Early Years ..............................................1-2 Glider or Sailplane? .......................................................1-3 Glider Pilot Schools ......................................................1-4 14 CFR Part 141 Pilot Schools ...................................1-5 14 CFR Part 61 Instruction ........................................1-5 Glider Certificate Eligibility Requirements ...................1-5 Common Glider Concepts ..............................................1-6 Terminology...............................................................1-6 Converting Metric Distance to Feet ...........................1-6 Chapter 2Components and Systems .................................2-1 Introduction....................................................................2-1 Glider Design .................................................................2-2 The Fuselage ..................................................................2-4 Wings and Components .............................................2-4 Lift/Drag Devices ...........................................................2-5 Empennage .....................................................................2-6 Towhook Devices .......................................................2-7 Powerplant .....................................................................2-7 Self-Launching Gliders .............................................2-7 Sustainer Engines .......................................................2-8 Landing Gear .................................................................2-8 Wheel Brakes .............................................................2-8 Chapter 3Aerodynamics of Flight .......................................3-1 Introduction....................................................................3-1 Forces of Flight..............................................................3-2 Newton’s Third Law of Motion .................................3-2 Lift ..............................................................................3-2The Effects of Drag on a Glider .....................................3-3 Parasite Drag ..............................................................3-3 Form Drag ...............................................................3-3 Skin Friction Drag ..................................................3-3 Interference Drag ....................................................3-5 Total Drag...................................................................3-6 Wing Planform ...........................................................3-6 Elliptical Wing ........................................................3-6 Rectangular Wing ...................................................3-7 Tapered Wing .........................................................3-7 Swept-Forward Wing ..............................................3-7 Washout ..................................................................3-7 Glide Ratio .................................................................3-8 Aspect Ratio ............................................................3-9 Weight ........................................................................3-9 Thrust .........................................................................3-9 Three Axes of Rotation ..................................................3-9 Stability ........................................................................3-10 Flutter .......................................................................3-11 Lateral Stability ........................................................3-12 Turning Flight ..............................................................3-13 Load Factors .................................................................3-13 Radius of Turn ..........................................................3-14 Turn Coordination ....................................................3-15 Slips ..........................................................................3-15 Forward Slip .........................................................3-16 Sideslip .................................................................3-17 Spins .........................................................................3-17 Ground Effect ...............................................................3-19 Chapter 4Flight Instruments ...............................................4-1 Introduction....................................................................4-1 Pitot-Static Instruments ..................................................4-2 Impact and Static Pressure Lines................................4-2 Airspeed Indicator ......................................................4-2 The Effects of Altitude on the AirspeedIndicator..................................................................4-3 Types of Airspeed ...................................................4-3Table of ContentsviiAirspeed Indicator Markings ......................................4-5 Other Airspeed Limitations ........................................4-6 Altimeter .....................................................................4-6 Principles of Operation ...........................................4-6 Effect of Nonstandard Pressure andTemperature............................................................4-7 Setting the Altimeter (Kollsman Window) .............4-9 Types of Altitude ......................................................4-10 Variometer................................................................4-11 Total Energy System .............................................4-14 Netto .....................................................................4-14 Electronic Flight Computers ....................................4-15 Magnetic Compass .......................................................4-16 Yaw String ................................................................4-16 Inclinometer..............................................................4-16 Gyroscopic Instruments ...............................................4-17 G-Meter ........................................................................4-17 FLARM Collision Avoidance System .........................4-18 Chapter 5Glider Performance .............................................5-1 Introduction....................................................................5-1 Factors Affecting Performance ......................................5-2 High and Low Density Altitude Conditions ...........5-2 Atmospheric Pressure .............................................5-2 Altitude ...................................................................5-3 Temperature............................................................5-3 Wind ...........................................................................5-3 Weight ........................................................................5-5 Rate of Climb .................................................................5-7 Flight Manuals and Placards ..........................................5-8 Placards ......................................................................5-8 Performance Information ...........................................5-8 Glider Polars ...............................................................5-8 Weight and Balance Information .............................5-10 Limitations ...............................................................5-10 Weight and Balance .....................................................5-12 Center of Gravity ......................................................5-12 Problems Associated With CG Forward ofForward Limit .......................................................5-12 Problems Associated With CG Aft of Aft Limit ..5-13 Sample Weight and Balance Problems ....................5-13 Ballast ..........................................................................5-14 Chapter 6Preflight and Ground Operations .......................6-1 Introduction....................................................................6-1 Assembly and Storage Techniques ................................6-2 Trailering....................................................................6-3 Tiedown and Securing ................................................6-4Water Ballast ..............................................................6-4 Ground Handling........................................................6-4 Launch Equipment Inspection ....................................6-5 Glider Preflight Inspection .........................................6-6 Prelaunch Checklist ....................................................6-7 Glider Care .....................................................................6-7 Preventive Maintenance .............................................6-8 Chapter 7Launch and Recovery Procedures and Flight Maneuvers ............................................................7-1 Introduction....................................................................7-1 Aerotow Takeoff Procedures .........................................7-2 Signals ........................................................................7-2 Prelaunch Signals ....................................................7-2 Inflight Signals ........................................................7-3 Takeoff Procedures and Techniques ..........................7-3 Normal Assisted Takeoff............................................7-4 Unassisted Takeoff.....................................................7-5 Crosswind Takeoff .....................................................7-5 Assisted ...................................................................7-5 Unassisted...............................................................7-6 Aerotow Climb-Out ....................................................7-6 Aerotow Release.........................................................7-8 Slack Line ...................................................................7-9 Boxing the Wake ......................................................7-10 Ground Launch Takeoff Procedures ............................7-11 CG Hooks .................................................................7-11 Signals ......................................................................7-11 Prelaunch Signals (Winch/Automobile) ...............7-11 Inflight Signals ......................................................7-12 Tow Speeds ..............................................................7-12 Automobile Launch ..................................................7-14 Crosswind Takeoff and Climb .................................7-14 Normal Into-the-Wind Launch .................................7-15 Climb-Out and Release Procedures ..........................7-16 Self-Launch Takeoff Procedures ..............................7-17 Preparation and Engine Start ....................................7-17 Taxiing .....................................................................7-18 Pretakeoff Check ......................................................7-18 Normal Takeoff ........................................................7-19 Crosswind Takeoff ...................................................7-19 Climb-Out and Shutdown Procedures ......................7-19 Landing .....................................................................7-21 Gliderport/Airport Traffic Patterns and Operations .....7-22 Normal Approach and Landing ................................7-22 Crosswind Landing ..................................................7-25 Slips ..........................................................................7-25 Downwind Landing ..................................................7-27 After Landing and Securing .....................................7-27viiiPerformance Maneuvers ..............................................7-27 Straight Glides ..........................................................7-27 Turns.........................................................................7-28 Roll-In ...................................................................7-29 Roll-Out ................................................................7-30 Steep Turns ...........................................................7-31 Maneuvering at Minimum Controllable Airspeed ...7-31 Stall Recognition and Recovery ...............................7-32 Secondary Stalls ....................................................7-34 Accelerated Stalls .................................................7-34 Crossed-Control Stalls ..........................................7-35 Operating Airspeeds .....................................................7-36 Minimum Sink Airspeed ..........................................7-36 Best Glide Airspeed..................................................7-37 Speed to Fly ..............................................................7-37 Chapter 8Abnormal and Emergency Procedures .............8-1 Introduction....................................................................8-1 Porpoising ......................................................................8-2 Pilot-Induced Oscillations (PIOs) ..............................8-2 PIOs During Launch ...................................................8-2 Factors Influencing PIOs ........................................8-2 Improper Elevator Trim Setting ..............................8-3 Improper Wing Flaps Setting ..................................8-3 Pilot-Induced Roll Oscillations During Launch .........8-3 Pilot-Induced Yaw Oscillations During Launch ........8-4 Gust-Induced Oscillations ..............................................8-5 Vertical Gusts During High-Speed Cruise .................8-5 Pilot-Induced Pitch Oscillations During Landing ......8-6 Glider-Induced Oscillations ...........................................8-6 Pitch Influence of the Glider Towhook Position ........8-6 Self-Launching Glider Oscillations During Powered Flight ...........................................................8-7 Nosewheel Glider Oscillations During Launchesand Landings ..............................................................8-7 Tailwheel/Tailskid Equipped Glider Oscillations During Launches and Landings ..................................8-8 Aerotow Abnormal and Emergency Procedures ............8-8 Abnormal Procedures .................................................8-8 Towing Failures........................................................8-10 Tow Failure With Runway To Land and Stop ......8-11 Tow Failure Without Runway To Land BelowReturning Altitude ................................................8-11 Tow Failure Above Return to Runway Altitude ...8-11 Tow Failure Above 800' AGL ..............................8-12 Tow Failure Above Traffic Pattern Altitude .........8-13 Slack Line .................................................................8-13 Ground Launch Abnormal and Emergency Procedures ....................................................................8-14 Abnormal Procedures ...............................................8-14 Emergency Procedures .............................................8-14 Self-Launch Takeoff Emergency Procedures ..............8-15 Emergency Procedures .............................................8-15 Spiral Dives ..................................................................8-15 Spins .............................................................................8-15 Entry Phase ...............................................................8-17 Incipient Phase .........................................................8-17 Developed Phase ......................................................8-17 Recovery Phase ........................................................8-17 Off-Field Landing Procedures .....................................8-18 Afterlanding Off Field .............................................8-20 Off-Field Landing Without Injury ........................8-20 Off-Field Landing With Injury .............................8-20 System and Equipment Malfunctions ..........................8-20 Flight Instrument Malfunctions ................................8-20 Airspeed Indicator Malfunctions ..........................8-21 Altimeter Malfunctions .........................................8-21 Variometer Malfunctions ......................................8-21 Compass Malfunctions .........................................8-21 Glider Canopy Malfunctions ....................................8-21 Broken Glider Canopy ..........................................8-22 Frosted Glider Canopy ..........................................8-22 Water Ballast Malfunctions ......................................8-22 Retractable Landing Gear Malfunctions ..................8-22 Primary Flight Control Systems ...............................8-22 Elevator Malfunctions ..........................................8-22 Aileron Malfunctions ............................................8-23 Rudder Malfunctions ............................................8-24 Secondary Flight Controls Systems .........................8-24 Elevator Trim Malfunctions .................................8-24 Spoiler/Dive Brake Malfunctions .........................8-24 Miscellaneous Flight System Malfunctions .................8-25 Towhook Malfunctions ............................................8-25 Oxygen System Malfunctions ..................................8-25 Drogue Chute Malfunctions .....................................8-25 Self-Launching Gliders ................................................8-26 Self-Launching/Sustainer Glider Engine Failure During Takeoff or Climb ..........................................8-26 Inability to Restart a Self-Launching/SustainerGlider Engine While Airborne .................................8-27 Self-Launching Glider Propeller Malfunctions ........8-27 Self-Launching Glider Electrical System Malfunctions .............................................................8-27 In-flight Fire .............................................................8-28 Emergency Equipment and Survival Gear ...................8-28 Survival Gear Checklists ..........................................8-28 Food and Water ........................................................8-28ixClothing ....................................................................8-28 Communication ........................................................8-29 Navigation Equipment ..............................................8-29 Medical Equipment ..................................................8-29 Stowage ....................................................................8-30 Parachute ..................................................................8-30 Oxygen System Malfunctions ..................................8-30 Accident Prevention .....................................................8-30 Chapter 9Soaring Weather ..................................................9-1 Introduction....................................................................9-1 The Atmosphere .............................................................9-2 Composition ...............................................................9-2 Properties ....................................................................9-2 Temperature............................................................9-2 Density ....................................................................9-2 Pressure ...................................................................9-2 Standard Atmosphere .................................................9-3 Layers of the Atmosphere ..........................................9-4 Scale of Weather Events ................................................9-4 Thermal Soaring Weather ..............................................9-6 Thermal Shape and Structure .....................................9-6 Atmospheric Stability .................................................9-7 Air Masses Conducive to Thermal Soaring ...................9-9 Cloud Streets ..............................................................9-9 Thermal Waves...........................................................9-9 Thunderstorms..........................................................9-10 Lifted Index ..........................................................9-12 K-Index .................................................................9-12 Weather for Slope Soaring .......................................9-14 Mechanism for Wave Formation ..............................9-16 Lift Due to Convergence ..........................................9-19 Obtaining Weather Information ...................................9-21 Preflight Weather Briefing........................................9-21 Weather-ReIated Information ..................................9-21 Interpreting Weather Charts, Reports, andForecasts ......................................................................9-23 Graphic Weather Charts ...........................................9-23 Winds and Temperatures Aloft Forecast ..............9-23 Composite Moisture Stability Chart .....................9-24 Chapter 10Soaring Techniques ..........................................10-1 Introduction..................................................................10-1 Thermal Soaring ...........................................................10-2 Locating Thermals ....................................................10-2 Cumulus Clouds ...................................................10-2 Other Indicators of Thermals ................................10-3 Wind .....................................................................10-4 The Big Picture .....................................................10-5Entering a Thermal ..............................................10-5 Inside a Thermal.......................................................10-6 Bank Angle ...........................................................10-6 Speed .....................................................................10-6 Centering ...............................................................10-7 Collision Avoidance ................................................10-9 Exiting a Thermal .....................................................10-9 Atypical Thermals ..................................................10-10 Ridge/Slope Soaring ..................................................10-10 Traps ......................................................................10-10 Procedures for Safe Flying .....................................10-12 Bowls and Spurs .....................................................10-13 Slope Lift ................................................................10-13 Obstructions ...........................................................10-14 Tips and Techniques ...............................................10-15 Wave Soaring .............................................................10-16 Preflight Preparation ...............................................10-17 Getting Into the Wave ............................................10-18 Flying in the Wave .................................................10-20 Soaring Convergence Zones ...................................10-23 Combined Sources of Updrafts ..............................10-24 Chapter 11Cross-Country Soaring .....................................11-1 Introduction..................................................................11-1 Flight Preparation and Planning ...................................11-2 Personal and Special Equipment ..................................11-3 Navigation ....................................................................11-5 Using the Plotter .......................................................11-5 A Sample Cross-Country Flight ...............................11-5 Navigation Using GPS .............................................11-8 Cross-Country Techniques ...........................................11-9 Soaring Faster and Farther .........................................11-11 Height Bands ..........................................................11-11 Tips and Techniques ...............................................11-12 Special Situations .......................................................11-14 Course Deviations ..................................................11-14 Lost Procedures ......................................................11-14 Cross-Country Flight in a Self-Launching Glider .....11-15 High-Performance Glider Operations and Considerations ............................................................11-16 Glider Complexity ..................................................11-16 Water Ballast ..........................................................11-17 Cross-Country Flight Using Other Lift Sources ........11-17 Chapter 12Towing ................................................................12-1 Introduction..................................................................12-1 Equipment Inspections and Operational Checks .........12-2 Tow Hook ................................................................12-2 Schweizer Tow Hook ...........................................12-2x。
轮机英语会话评估问答题翻译
D轮机英语会话评估问答题参考答案第一章1. How long have you worked on board?你在船上工作多长时间了?)(For 5 years.五年了2. Which certificate do you have now?(你现在持有什么证书?)(2nd Engin eer certificate.)大管证书3. What is your marital status?(你的婚姻状况是什么?)How many departme nts are there on board?船上有多少个部门?)(I am unm arried. There are three departme nts on board. Such asengine, deck and service departme nts.我未婚。
船上有三个部门,即甲板部、轮机部和服务部。
4. How many people are there in your family? Are you married?你家里有几口人?你结婚了吗?)(Three. No, I'm not married.)三口,未婚5. How many coun tries have you ever bee n to?你曾经去过多少个国家?)(Four. Such as Japan ,America,Ca nada...四个,例如日本,美国,加拿大等等6. Whe n did you begi n to work on board? What kind of ship have you worked on?你什么时候开始上船工作的?你在哪些类型的船上工作过?)(In 1999. Cargo ship.)1999年,货船7. How many importa nt can als are there all over the world?(世界上有几大重要的运河?)(Two. the Pan ama and Suez两大运河,巴拿马和苏伊士运河8. Can you tell me what is the most importa nt thi ng for a seafarer?能不能告诉我对于一个船员来说最重要的事情是什么吗?)(Safety. Safety first)安全,安全第一9. What kinds of ma in engine and gen erator engine have you worked on?你工作过的主机和发电机是什么类型的?)(Ma in engine: Sulzer, Man B & W engines and so on. Gen erator engin e:Yama, Watsila Diesela nd so on.主机:苏尔寿,Man B &W 主机等等,辅机:雅玛,瓦锡兰等等10. W hich classification society is your ship registered with?你们的船在哪个船级社登记注册的?)(CCS.)中国船级社11. H ave you worked any ship that caused damage in critical equipme nt?你工作过的船发生过重大机损吗?)(Yes, I have worked on a cargo ship that the main engine had bee n damagedJNo, I served my job cautiously是的,我工作过的货船主机损坏过12. How do you make your mai nte nance schedules?如何制定你们的维修保养计划?)(It is based on ship ' planed maintenance system and the machinery running hours records.)(它基于船舶计划维护保养体系和机器机械的运转时间记录)13. Could you list intern ati onal conven tio ns concerning marine shipp ing?(你能列举有关海运的国际公约吗?)(STCW, SOLAS, MARPOL, ISM Code and so on.)14. Could you tell the usagesof the STCW convention?(你能谈谈STCW 公约的用途吗?)(To provide sta ndards of trai ning, certificati on and watch keep ing for seafarers.)提供船员培训、发证和值班标准的国际公约。
底特律发动机喷油器故障分析
2020年4月 物 探 装 备 第30卷 第2期底特律发动机喷油器故障分析孙军和*1 刘金中2 房拴虎2 李永政3 许庆宝3(东方地球物理公司:1.国际勘探事业部,河北涿州 072750;2.装备服务处;3.塔里木物探处)孙军和,刘金中,房拴虎,李永政,许庆宝.底特律发动机喷油器故障分析及排查.物探装备,2020,30(2):112-115摘要 底特律发动机广泛应用于各种型号的可控震源,其喷油器结构采用DDEC 电控系统结构。
发动机运转大于2万小时后,喷油器故障率逐渐升高。
喷油器的故障会直接导致发动机遇大负载时熄火,机油内混入燃油,高耗燃油等问题。
本文针对底特律发动机喷油器引发的故障类型,结合喷油器结构原理对发动机故障进行分析,总结出一种简单排除发动机喷油器故障的方法。
关键词 可控震源 底特律发动机 喷油器 故障排除Sun Junhe ,Liu Jinzhong ,Fang Shuanhu ,Li Yongzheng and Xu Qingbao .Troubleshooting of Detroit engine injector .EG P ,2020,30(2):112-115Abstract Detroit engine is widely used in various types of vibrators , its injector structure is based on the DDEC electronic control system. After more than 20,000 hours of engine operation , the injector failure rate gradually increased. The failure of the injector will directly cause the engine load to stall , engine oil mixed with fuel and engine fuel consumption. Based on the types of engine injector faults in Detroit , this paper analyzes engine faults based on the structural principles of the injector , and summarizes a simple method to eliminate engine injector faults.Key words vibrator ,Detroit engine ,injector ,troubleshooting0 引言DDEC 电控泵喷油器是将泵油柱塞、喷油嘴及电磁阀合成一体,然后安装在一个壳体里。
电动车降速利弊英语作文
Electric vehicles,or EVs,are becoming increasingly popular due to their environmental benefits and innovative technology.However,the issue of speed regulation for these vehicles has sparked a debate.Here,we will explore the advantages and disadvantages of imposing speed limits on electric vehicles.Advantages of Speed Limitation for Electric Vehicles:1.Enhanced Safety:Lowering the speed of electric vehicles can significantly reduce the risk of accidents.Higher speeds often lead to shorter reaction times,which can be critical in emergency situations.2.Increased Battery Life:Speeding can drain the battery faster due to increased power consumption.By maintaining a moderate speed,the battery life can be extended,leading to longer driving ranges between charges.3.Reduced Energy Consumption:Slower speeds mean less energy is needed to propel the vehicle.This can lead to more efficient energy use and potentially lower electricity costs for the driver.4.Environmental Impact:While electric vehicles are already environmentally friendly due to their lack of tailpipe emissions,reducing their speed can further decrease the energy needed to manufacture and power them,thereby reducing their overall carbon footprint.5.Noise Pollution Reduction:Electric vehicles are generally quieter than their internal combustion engine counterparts.However,at higher speeds,the noise generated by tires and wind resistance can increase.Limiting speed can help keep noise levels down in residential areas.Disadvantages of Speed Limitation for Electric Vehicles:1.Decreased Convenience:Imposing speed limits on electric vehicles may reduce their convenience for longdistance travel.Drivers may find it takes longer to reach their destinations,which could deter some from choosing electric vehicles.2.Impact on Performance:Electric vehicles are known for their quick acceleration and smooth performance.Restricting their top speed could diminish the driving experience for some users who value the performance aspect of EVs.3.Economic Implications:If speed limits are imposed,it could affect the marketability ofelectric vehicles.Consumers who prioritize speed and performance might be less inclined to purchase EVs,potentially slowing down the adoption rate of these vehicles.4.Technological Limitations:Some electric vehicles are designed with advanced technology that allows for highspeed driving.Limiting their speed could be seen as underutilizing this technology and not allowing the vehicles to perform to their full potential.5.Inconsistency with Existing Infrastructure:Most roads and highways are designed with the assumption that vehicles can travel at certain speeds.Imposing lower speed limits on electric vehicles could create inconsistencies and potential safety issues as drivers adjust to different speed expectations.In conclusion,while there are clear benefits to imposing speed limits on electric vehicles, such as increased safety and environmental benefits,there are also significant drawbacks that could impact the adoption and enjoyment of these vehicles.It is essential to strike a balance that promotes the sustainable use of electric vehicles while also respecting the needs and preferences of drivers.。
跑步比赛英语作文
Running is a popular form of exercise that not only promotes physical health but also fosters a competitive spirit.A running race can be an exhilarating event that brings together individuals from various backgrounds,all striving to achieve a common goalto reach the finish line as quickly as possible.The Preparation for a Running RaceBefore a running race,athletes engage in rigorous training.This includes building up stamina through longdistance runs,improving speed with interval training,and enhancing agility with plyometric exercises.Nutrition also plays a vital role,with athletes often adjusting their diets to maximize performance.Carbohydrate loading is a common practice to ensure energy levels are high for the race.The Atmosphere of a Running RaceOn the day of the race,the atmosphere is electric.Participants gather at the starting line, stretching and warming up,their faces a mix of excitement and apprehension.Spectators line the route,cheering on the runners and providing muchneeded encouragement.The air is filled with anticipation as the starting pistol fires,signaling the beginning of the race. The Strategy of a Running RaceDuring a race,athletes employ various strategies to gain an advantage.Some runners start at a fast pace to establish a lead,while others prefer a more measured approach, conserving energy for a final sprint.Pacing is crucial a runner must balance speed with endurance to avoid exhausting themselves too early.The Mental Aspect of a Running RaceMental fortitude is as important as physical strength in a running race.Runners must maintain focus and determination,especially during the challenging middle stages of a race.Visualization techniques,positive selftalk,and goal setting are all tools that runners use to push through the pain and fatigue that inevitably sets in.The Finish LineAs the runners approach the finish line,the crowds cheers grow louder,and the excitement reaches a crescendo.Every runner,regardless of their position,experiences a sense of accomplishment.The finish line is not just the end of the race but also a testament to the hard work,dedication,and perseverance of each participant.Reflections on a Running RaceAfter the race,runners often reflect on their performance.Some may celebrate personal bests,while others may analyze areas for improvement.Regardless of the outcome,the experience of a running race is a valuable one,offering lessons in discipline,resilience, and the joy of pushing ones limits.In conclusion,a running race is more than just a physical challenge it is a journey of selfdiscovery and personal growth.It is a testament to the human spirits ability to strive for excellence and to overcome obstacles.Whether you are a seasoned athlete or a firsttime participant,the experience of a running race is one that will stay with you, inspiring you to continue pursuing your own personal best.。
speeding habits 英语作文
speeding habits 英语作文Speeding Habits: Understanding the Impact and Solutions。
Speeding is a prevalent issue on roads worldwide, posing significant risks to both drivers and pedestrians. Understanding the reasons behind speeding habits and exploring effective solutions are essential steps towards creating safer road environments. This article delves into the causes of speeding, its consequences, and proposes strategies to address this concerning behavior.One of the primary reasons for speeding is the misconception that it saves time. Many drivers believe that reaching their destination faster is worth the risk of breaking speed limits. However, studies have shown that the time saved by speeding is often minimal, especially for short distances. Moreover, the potential consequences of speeding, such as accidents and fines, outweigh any perceived time benefits.Another factor contributing to speeding habits is societal pressure. In today's fast-paced world, there is a constant urge to rush through tasks, including driving. This pressure can lead individuals to disregard speed limits and prioritize speed over safety. Additionally, peer influence plays a significant role, with some drivers feeling compelled to match the speed of surrounding vehicles to avoid being left behind.Furthermore, advancements in technology have made cars faster and more powerful, tempting drivers to test the limits of their vehicles. The thrill of speed combined with the accessibility of high-speed vehicles can fuel reckless driving behavior. Additionally, distractions such as mobile phones and in-car entertainment systems can divert attention away from the road, making it easier for drivers to exceed speed limits unintentionally.The consequences of speeding are severe and far-reaching. Firstly, speeding increases the likelihood and severity of accidents. High speeds reduce reaction times and make it more challenging to control vehicles, leading to a higher risk of collisions. Furthermore, accidents at high speeds are more likely to result in fatalities or seriousinjuries, impacting not only the individuals involved but also their families and communities.Moreover, speeding contributes to environmental degradation and increased fuel consumption. Vehicles traveling at higher speeds emit more pollutants, worsening air quality and contributing to climate change. Additionally, higher speeds require more fuel, leading to increased fuel consumption and higher carbon emissions. Addressing speeding habits is therefore crucial for mitigating the environmental impact of road transportation.To tackle speeding effectively, a multi-faceted approach is needed. Firstly, raising awareness about the dangers of speeding through education campaigns and public service announcements can help change attitudes and behaviors towards driving. Emphasizing the consequences of speeding, both in terms of personal safety and legal repercussions, can encourage drivers to adhere to speed limits.Secondly, implementing stricter enforcement measures, such as speed cameras and increased police presence on roads, can deter speeding and hold offenders accountable. By enforcing speed limits consistently and fairly, authorities can send a clear message that speeding will not be tolerated, thereby reducing the prevalence of this risky behavior.Additionally, investing in infrastructure improvements, such as traffic calming measures and redesigned road layouts, can help create safer driving environments. Measures such as speed bumps, roundabouts, and narrower lanes can encourage drivers to slow down and improve overall road safety. Furthermore, promoting alternative modes of transportation, such as public transit, cycling, and walking, can reduce the reliance on cars and alleviate traffic congestion.In conclusion, speeding habits pose significant challenges to road safety and public health. Understanding the underlying causes of speeding and implementing effective solutions are essential steps towards creating safer road environments. By raising awareness, enforcing speed limits, and investing in infrastructure improvements, we can work towards reducing speeding-related accidents and creating a culture of responsible driving.。
矿用水泵维修进度计划英语
矿用水泵维修进度计划英语Mine Dewatering Pump Maintenance Schedule.Introduction.Dewatering pumps play a crucial role in mining operations by removing excess water from mine sites. To ensure efficient and safe operation, regular maintenance of these pumps is essential. This maintenance scheduleoutlines the specific tasks, intervals, andresponsibilities for maintaining mine dewatering pumps.Scope.This schedule applies to all dewatering pumps used in the mining operation, including submersible, centrifugal, and positive displacement pumps.Maintenance Tasks and Intervals.Daily.Visual inspection for leaks, vibrations, and unusual noises.Check water flow and pressure.Monitor pump temperature.Weekly.Clean pump intake and discharge screens.Inspect bearings and lubricate if necessary.Check oil levels and top up if required.Monthly.Test pump performance and record data.Calibrate pressure and flow gauges.Inspect pump impeller and casing for wear.Quarterly.Disassemble pump for thorough inspection.Replace worn components, such as bearings, seals, and impellers.Recondition or replace damaged parts.Annually.Overhaul pump, including disassembly, cleaning, inspection, and replacement of major components.Test pump performance and calibrate sensors.Conduct vibration analysis and alignment check.Responsibilities.Maintenance Personnel.Responsible for performing all maintenance tasks as per the schedule.Document maintenance activities and findings.Report any issues or concerns promptly.Supervisors.Ensure that maintenance personnel are trained and certified.Monitor maintenance progress and adherence to the schedule.Conduct regular inspections to verify pump performance and safety.Engineering Team.Provide technical support and guidance to maintenance personnel.Analyze pump performance data and make recommendations for improvements.Design and implement modifications to enhance pump efficiency and reliability.Materials and Spare Parts.Ensure that all necessary materials, spare parts, and tools are available for maintenance activities.Maintain an inventory of critical spare parts to minimize downtime.Training and Certification.All maintenance personnel must receive proper training and certification for the specific pumps being maintained.This training should cover:Pump operation and maintenance principles.Safety procedures.Troubleshooting and repair techniques.Use of specialized tools and equipment.Monitoring and Evaluation.Regularly monitor pump performance and maintenance history.Track downtime and repair costs.Conduct periodic audits to assess the effectiveness of the maintenance program.Make adjustments to the schedule as needed based on performance data and industry best practices.Documentation.Maintenance activities and findings should be documented in detail.Records should include dates, tasks performed, parts replaced, and any observations.Maintain historical records for reference and analysis.Emergency Procedures.In the event of a pump failure or other emergency situation, the following procedures should be followed:Stop the pump immediately.Isolate the pump from the system.Notify maintenance personnel and supervisors.Follow established emergency response protocols.Continuous Improvement.The maintenance schedule should be reviewed and updated regularly to reflect changes in pump technology, operating conditions, and best practices. Feedback from maintenance personnel and supervisors should be incorporated to enhance the effectiveness of the program.。
极限运动失误英语
极限运动失误英语极限运动是一项充满挑战和刺激的运动,但它也带来了很多风险。
在进行极限运动时,有时会发生失误,这可能导致严重的后果。
以下是一些与极限运动失误相关的英语词汇和短语。
1. Accident - 意外事故2. Injury - 伤害3. Risk - 风险4. Danger - 危险5. Safety - 安全6. Protective gear - 保护装备7. Fall - 跌落8. Crash - 碰撞9. Mishap - 不幸事件10. Mistake - 失误11. Error - 错误12. Misjudgment - 判断错误13. Overconfidence - 过度自信14. Lack of preparation - 缺乏准备15. Negligence - 疏忽16. Carelessness - 不小心17. Risk-taking behavior - 冒险行为18. Impulsive behavior - 冲动行为19. Inexperience - 缺乏经验20. Caution - 谨慎21. Vigilance - 警惕性22. Adrenaline rush - 肾上腺素飙升23. Thrill-seeking - 追求刺激24. Extreme sports - 极限运动25. Base jumping - 跳底26. Skydiving - 跳伞27. Bungee jumping - 蹦极28. Rock climbing - 攀岩29. Surfing - 冲浪30. Snowboarding - 滑雪板31. Skateboarding - 滑板32. Parkour - 跑酷33. Motocross - 摩托越野34. Paragliding - 滑翔伞35. Wingsuit flying - 翼装飞行在进行极限运动时,请务必注意安全并遵守规则。
船用柴油机调速系统技术要求和试验方法-最新国标
船用柴油机调速系统技术要求和试验方法1范围本文件规定了船用柴油机调速系统的术语和定义、技术要求、试验方法等。
本文件适用于船用柴油机调速系统的设计、制造和验收。
2规范性引用文件下列文件中的内容通过文中的规范性引用而构成本文件必不可少的条款。
其中,注日期的引用文件,仅该日期对应的版本适用于本文件;不注日期的引用文件,其最新版本(包括所有的修改单)适用于本文件。
中国船级社《钢质海船入级规范》3术语和定义下列术语和定义适用于本文件。
3.1调速系统speed governing system指由调速器和调节对象组成的系统。
调速器包括位置控制式燃油喷射系统和时间控制式燃油喷射系统,调节对象包括柴油机及其负载装置。
3.2转速调节的过渡过程transitional process of speed adjustment指负载变化引起的转速随时间变化的过程(见图1)。
图1转速调节过渡过程曲线3.3额定功率specified powerPer指柴油机按用途和使用特点在铭牌上所标明的功率,亦称额定负载。
3.4额定转速specified speedrn 指柴油机发出额定功率时的相应转速。
3.5额定工况specified working condition 柴油机在额定功率和额定转速下运行的工况。
3.6最高瞬时转速maximum transient speedmaxn 柴油机在额定工况下运行时,突卸额定负载后,转速升高达到的最大值。
3.7空载转速no-load speedin 3.8min柴油机在不带载情况下的稳定转速。
最低瞬时转速 minimum transient speedn 柴油机在空载下稳定运行时,突加额定负载后,转速降落达到的最小值,以n min 表示。
3.9部分负载时的转速part-load speedLn 柴油机在部分负载下运行时的稳定转速。
3.10转速波动率speed stability bandwidth υ柴油机在负载不变的工况下运行,在一定的时间间隔内(不少于1min)测得的最高转速1n 和最低转速2n 之差对两倍额定转速r n 的百分比,并按公式(1)计算:1r100%n nn υ-=⨯22 (1)式中:n 1——测得的最高转速,单位为转每分(r/min);n 2——测得的最低转速,单位为转每分(r/min);n r ——额定转速,单位为转每分(r/min)。
与外国飞机对抗流程
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1. 识别的责任。
防空部队负责识别进入中国领空的外国飞机。
非计划拔管不良事件改进流程
非计划拔管不良事件改进流程英文回答:Unplanned Extubation Adverse Event Improvement Process.Introduction.Unplanned extubation (UE) is a common and potentially severe adverse event in critically ill patients receiving mechanical ventilation. It can lead to patient harm, prolonged hospital stays, and increased healthcare costs. The implementation of an effective unplanned extubation improvement process is essential to minimize the incidence of this event and improve patient outcomes.Process.The unplanned extubation improvement process should involve a multidisciplinary team approach. The team should include physicians, nurses, respiratory therapists, andother relevant healthcare professionals. The process should include the following steps:1. Identify Root Causes:Conduct a thorough root cause analysis of all unplanned extubation events to identify contributing factors.Use tools such as failure mode and effects analysis (FMEA) or the Swiss cheese model to identify potential weaknesses in the system.2. Develop and Implement Interventions:Based on the identified root causes, develop and implement interventions to address each contributing factor.Examples of interventions may include:Enhancing patient and family education.Increasing nurse surveillance.Using physical restraints or securing devices.Modifying sedation protocols.3. Monitor and Evaluate Outcomes:Continuously monitor the incidence of unplanned extubation and measure the effectiveness of implemented interventions.Use data to track progress and identify areas for further improvement.4. Sustain and Improve:Regularly review the unplanned extubation improvement process and make necessary adjustments to ensure its effectiveness.Engage stakeholders in the process to fosterownership and continued improvement.Technology.Technology can play a significant role in reducing unplanned extubation. The following technologies can be utilized:Patient Monitoring Systems: Advanced patient monitoring systems can provide continuous monitoring of vital signs, including respiratory parameters, to detect impending signs of extubation.Voice-Activated Devices: Voice-activated devices allow patients to communicate with healthcare providers without removing the endotracheal tube, reducing the risk of accidental extubation.Telehealth: Telehealth platforms can facilitate remote monitoring of ventilated patients, allowing healthcare providers to assess patients and make adjustments to their management from a distance.Education and Training.Education and training are crucial for preventing unplanned extubation. Healthcare professionals should receive comprehensive training on the following topics:Identification and Management of Risk Factors:Identifying patients at risk for unplanned extubation and implementing appropriate preventive measures.Proper Extubation Technique: Safe and effective extubation procedures to minimize the risk of complications.Use of Technology: Familiarizing healthcare providers with the use of technology to support unplanned extubation prevention.Conclusion.The implementation of a comprehensive unplanned extubation improvement process is essential in reducing theincidence of this adverse event and improving patient outcomes. A multidisciplinary team approach, evidence-based interventions, technology utilization, and ongoingeducation and training are key elements of an effective unplanned extubation prevention program.中文回答:意外拔管不良事件改进流程。
P57英语臀部肌肉注射模拟器产品说明书
P57®EnglishIntramuscular Injection Simulator-ButtockThank you for choosing a 3B Scientific® product. Please read the user manual carefully before using the unit to ensure a flawless operation and to enable you to work in a satisfactory way with this product. Table of contents:1. Quick Instructions3 1.1 Turning the unit on 3 1.2 T button / C button 3 1.3 Matrix of the result indicator 41.4 Turning the unit off 42. Getting started and operation 4 2.1 Accessories 4 2.2 Some preliminary remarks 4 2.3 Power supply 4 2.4 Inserting and removing thebatteries 4 3. Working with the P57 6 3.1 Operation 6 3.1.1 Layout of the display 6 3.1.2 Turning the unit on and off 6 3.1.3 Training mode (T button) 6 3.1.4 Control mode (C button) 63.2 Administering an intramuscular(i.m.) injection into thebuttock musculature 7 3.2.1 A dministering ventroglutealinjections using the ‘A. vonHochstetter’ method 73.2.2 Disinfection of the skin 74. Operation and storage7 4.1 Tabletop operation 7 4.2 Storage 75. General safety precautions 86. Frequently asked questions (FAQ’s) 8 6.1 The battery indicator is flashing.After turning the unit on again,the indicator is off. But whydoes it then light up again? 8 6.2 Why can’t the injectionsimulator be turned on againafter prolonged storage? 8 6.3 Which types of batteries arerecommended for the injectionsimulator? 8 6.4 Can I also operate the injectionsimulator with rechargeablebatteries? 87. Transport and packaging 88. Maintenance 8 8.1 Care instructions 8 8.2 Exchanging the silicone skin 8 8.3 Warranty 11 8.4 Request for replacement parts 112EnglishIntramuscular Injection Simulator-Buttock1.1 Turning the unit ONBefore using the unit for the first time please insert the supplied batteries (2x AA), (see p. 4/ 2.4).In the training mode (T button), you will immediately receive feedback as follows whileadministering the injection: • p ositive feedback (result indicator (LED green) when you have performed the injection into the muscle correctly,• n egative feedback (result indicator (LED red) + acoustic signal) when you hit the bone.In the control mode (C button) you will receive no feedback while performing an injection into the muscle. The result will be saved and you have to press the C button again to check whether you have carried out the intramuscular injection correctly or incorrectly. You will receive• positive feedback (result indicator (LED green)) when you have performed the intramuscular injection correctly,•n egative feedback (result indicator (LED red)) when you have performed the injection incorrectly. When you hit the bone while injecting, you will immediately receive negative feedback (resultindicator (LED red) + acoustic signal).12345671. Quick InstructionsStatus light (red LED) for battery Start buttonT button (training mode)Status indicator (yellow LED) for C button C button (control mode)Result indicator (red and green LED)3®English1.3 Matrix of the result indicatorResult indicator (training mode)Result indicator (control mode)Correct injection/site green greenIncorrect injection/site no signal redNot deep enough no signal red Injection into the bone red red1.4Turning the unit OFFThe unit automatically switches off when it has not been used for a period of two minutes, or can be manually turned off by simultaneously pressing the T button and the C button.2 Getting started and operation2.1 Accessories•P57 Injection simulator (buttock), (foam) muscle and silicone skin preassembled•Disposable 5 ml syringe•Injection cannula for intramuscular injections• 2 AA batteries•Control unit•Connecting cable (control unit / simulator)2.2 Some preliminary remarks• Place the supplied batteries into the P57 Injection Simulator before first usage. (see 2.4 Inserting the batteries)• Please use only the (rechargeable or non-rechargeable) batteries for the P57 Injection Simulatorrecommended on page 8 (section 6.3).• When inserting the batteries, please ensure correct polarity! Incorrectly inserted batteries may damage the unit!• The skin of the 3B Scientific injectable buttock is made of an elastic material (silicone). Afterprolonged usage and repeated punctures in the same area it may become necessary to substitute the s kin with a replacement skin. Injections into the simulator should only be performed usingcannula gauges (20 and 21 gauge /0.8, 4 cm long, syringe).2.3 Power supplyThe P57 Injection Simulator is supplied with two 1.5 V, type AA/LR6 alkaline manganese batteries. These enable an operating time of up to 20 hours. This period may vary depending on the type of batteries used.2.4. Inserting and replacing the batteriesRemove the cap of the battery compartment at the back of the control unit by sliding it downwards. Then insert the supplied AA batteries, ensuring correct polarity (see p. 5, figs. 1 and 2). Intramuscular Injection Simulator-Buttock4English Intramuscular Injection Simulator-Buttock fig. 1fig. 2fig. 35English3 Working with the P573.1 Operation3.1.1 Layout of the displayStatus light (red LED) for battery Start buttonT button (training mode)Status indicator (yellow LED) for T button Status indicator (red LED) for C button C button (control mode)Result indicator (red and green LED)3.1.2 Turning the unit ON and OFF Turning ON• • ••• This is to prevent any leaking batteries from causing damage to the unit.• • • Now administer the injection.• You will receive immediate feedback as follows while performing the injection- positive feedback (result indicator (LED green)) when you have performed the intramuscular injection correctly,- negative feedback (result indicator (LED red) + acoustic signal) when you hit the bone.• • • 1234567Intramuscular Injection Simulator-Buttock6®English• Now administer the injection.• The information whether the site and depth of the injection have been selected correctly is now temporarily saved by the unit, but not yet displayed.• After completing the injection, press the C button once more to indicate the result. The yellow status indicator next to the C button will flash during this process. You will receive- positive feedback (result indicator (LED green)) when you have performed the injection into the muscle correctly (correct site and correct depth),- negative feedback (result indicator (LED red)) when you have performed the injection incorrectly (at wrong sites and/or not deep enough).• When hitting a bone during the injection you will receive immediate negative feedback (result indicator (LED red) + acoustic signal).•3.2 Administering an intramuscular (i.m.) injection into the buttock musculature3.2.1 Administering ventrogluteal injections using the ‘A. von Hochstetter’ methodA relatively safe method for intramuscular injections in the buttock region is the ‘A. von Hochstetter’ method. The injection is administered into the gluteus medius muscle, or into the gluteus minimus muscle located underneath.The injection can be administered with the patient either in the supine or lateral position. Anatomical landmarks are (1) the greater trochanter, (2) the anterior iliac spine, and (3) the iliac crest. These are eas-ily palpable bony landmarks.To locate the injection site, spread the index and middle fingers apart as far as possible. Palpate the anterior iliac spine with the tip of the index or middle finger located ventrally (depending on the side of the body). Palpate the iliac crest with the other (abducted) finger. Then rotate this finger approx. 2 cm downward, while the other finger remains on the anterior iliac spine. As a result of the rotation, the ball of the hand should rest on the great trochanter. The lower part of the triangle now formed by the index and middle fingers is the injection site.Disinfect the injection site and insert the needle perpendicularly, i.e. at a 90° angle to the body surface. Before injecting, aspirate by pulling back on the plunger of the syringe to avoid inadvertent vessel punc-turing. Now start injecting, making sure that the needle is protected against any change of position. When finished, remove the needle and compress the injection site with a sterile pad.3.2.2 Disinfection of the skinPlease use only normal tap water to disinfect the skin, since ordinary disinfectants may damage the materials of the model.4. Operation & storage4.1 Tabletop operationPosition the injection simulator on a level and non-slippery surface.4.2 Storage• The injection simulator is best stored at a dry place at room temperature.• Do not expose the injection simulator to direct sunlight, since heat over 45°C may cause the material to deform or become brittle.• When the injection simulator is not used for a prolonged period of time, it is recommended to remove the batteries.Intramuscular Injection Simulator-Buttock7®English5. General safety precautions• Keep out of the reach of children!• Do not recharge batteries (LR6) under any circumstances! Risk of Explosion!• Empty batteries must be disposed of in accordance with the national requirements!• E nvironment: components must be disposed of in accordance with the relevant national environment regulations concerning the decommissioning and final disposal of the unit.• Recharge batteries only with a suitable charging set.• D o not use any powerful chemicals to clean the unit, since these may cause damage to the materials of the model.6. Frequently asked questions (FAQs)6.1 The battery indicator is flashing. After turning the unit on again, the indicator is off. But why does it then light up again?This may happen when batteries of different capacities are used. In this case, please replace the batteries with new ones. Tip: As a rule, only use batteries of the same type, the same capacity, the same age and the same manufacturer. Mark “matching” batteries accordingly.6.2 Why can’t the injection simulator be turned on again after prolonged storage?Rechargeable batteries are subject to self-discharge, even while the unit is turned off. Self-discharge is approximately 20% per month. Even disposable batteries run down slightly while the injection simulator is turned off. Tip: Remove the batteries from the battery compartment when not using the unit for a prolonged period of time. This is to prevent that any leaking batteries cause damage to the unit. Afterthe injection simulator has not been used for a prolonged period of time, only insert freshly recharged batteries or new batteries into the unit.6.3 Which types of batteries are recommended for the injection simulator?We recommend the use of alkaline manganese batteries (type AA batteries or LR6). Zinc carbon batteries should not be used.6.4 Can I also operate the injection simulator with rechargeable batteries?Yes, you can use Ni-MH (nickel metal hydride) or Ni-Cd (nickel cadmium) rechargeable batteries.You will achieve a substantially longer operation time with Ni-MH batteries than with Ni-Cd batteries. Tip: Use batteries of the same type, age and manufacturer only.7. Transport and packagingPlease check the shipping and product packaging for any damage. In case of transport damage, please contact your dealer. Please keep the original packaging. This special packaging is the best protection for your valuable product during transport.8. Maintenance8.1 Care instructionsThe silicone skin of the injection simulator can be cleaned with a mild soap solution. Please do not use any detergents containing solvents, as these will damage the silicone skin.8.2. Exchanging the silicone skinLift the silicone skin up on one side of the injection simulator and then pull it up on the left and the right until it is completely detached from the frame (see p. 9/figs. 4 + 5).Attention: Please make sure that the (foam) muscle is not detached from the underlying bone during this process. The silicone skin can now be easily removed and exchanged with a replacement skin (see p. 10/figs. 6 ). The old silicone skin can be disposed of with normal household waste. Intramuscular Injection Simulator-Buttock8Intramuscular Injection Simulator-ButtockEnglishfig. 59Intramuscular Injection Simulator-ButtockEnglish Array fig. 610®English 8.3 WarrantyThe warranty period for the injection simulator is 36 months from the invoice date and shall include engineering, material and manufacturing defects and the electronic functions of the unit, provided that the unit has been subjected to normal usage and appropriate maintenance. The warranty shall not cover parts subject to wear, such as silicone skin, foam core, injection cannula, disposable syringe and batteries.Within the scope of the warranty claim, 3B Scientific shall not be obliged to pay compensation for damage caused in the context of or as a consequence of non-authorized persons carrying out or attemptingrepairs, modifications or changes, or when the product or any part of it has been damaged by an accident, unintended usage or misuse.8.4 Request for replacement parts• Silicone skin (XP302)In case of a complaint, please indicate the serial number located at the center of the bottom of the base housing under the felt cover of the injection simulator.Intramuscular Injection Simulator-Buttock11P 57-04/07-1。
闯红灯的英语作文
闯红灯的英语作文Title: Consequences of Running Red Lights。
Running red lights is a dangerous behavior that notonly jeopardizes the safety of oneself but also endangers the lives of others on the road. In this essay, we will explore the reasons behind this reckless action and itsdire consequences.Firstly, it's essential to understand why people runred lights. One primary reason is impatience. In today'sfast-paced world, many individuals are constantly in a rush, whether it's to get to work on time, attend an appointment, or simply reach their destination quickly. This impatience often leads them to take unnecessary risks, such asspeeding up to beat a red light.Moreover, some drivers may run red lights due to distraction. With the proliferation of smartphones andother electronic devices, distracted driving has become asignificant concern. Checking messages, making calls, or even adjusting the GPS can divert one's attention from the road, causing them to miss traffic signals.Another factor contributing to red light running is disregard for traffic laws. Some drivers may have acavalier attitude towards traffic regulations, believing that they can bend or break the rules without consequence. This lack of respect for the law not only puts the individual at risk but also undermines the safety of everyone else sharing the road.Regardless of the reasons behind it, the consequences of running red lights can be severe. Firstly, there's the risk of causing a traffic collision. When a driver runs a red light, they are essentially entering an intersection when they shouldn't, increasing the likelihood of T-bone or side-impact collisions with vehicles crossing on the green light. These types of crashes are among the most dangerous and can result in severe injuries or even fatalities.Furthermore, running red lights can have legalrepercussions. In many jurisdictions, it is considered a traffic violation punishable by fines, license points, or even license suspension. Repeat offenders may face more severe penalties, including increased insurance premiums or mandatory attendance at defensive driving courses.Beyond the immediate consequences, there's also the emotional toll of being involved in a traffic accident. Not only does it cause physical harm, but it can also lead to psychological trauma for both the individuals directly involved and their loved ones. The guilt and remorse of causing harm to others can haunt a person long after the accident has occurred.In addition to the human cost, there are also economic implications associated with red light running. Traffic accidents result in property damage, medical expenses, and loss of productivity due to injuries or fatalities. These costs are borne not only by the individuals involved but also by society as a whole through increased insurance premiums and healthcare expenses.To address the issue of red light running, various measures can be implemented. These include increasing enforcement through traffic cameras or police patrols, improving intersection design to reduce conflict points, and raising awareness through public education campaigns about the dangers of running red lights.In conclusion, running red lights is a reckless behavior with serious consequences. Whether due to impatience, distraction, or disregard for traffic laws, the risks associated with this action far outweigh any perceived benefits. By understanding the reasons behind red light running and implementing measures to prevent it, we can work towards creating safer roads for everyone.。
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Speeding-up Fault Injection Campaigns in VHDL modelsB. Parrotta, M. Rebaudengo, M. Sonza Reorda, M. ViolantePolitecnico di Torino, Dip. di Automatica e Informatica, C.so Duca degli Abruzzi 24,I-10129 Torino, Italy{parrotta, reba, sonza, violante}@polito.itAbstract. Simulation-based Fault Injection in VHDL descriptions is increas-ingly common due to the popularity of top-down design flows exploiting thislanguage. This paper presents some techniques for reducing the time to per-form the required simulation experiments. Static and dynamic methods areproposed to analyze the list of faults to be injected, removing faults as soonas their behavior is known. Common features available in most VHDL simu-lation environments are also exploited. Experimental results show that theproposed techniques are able to reduce the time required by a typical FaultInjection campaign by a factor ranging from 43.9% to 96.6%.1 IntroductionIn recent years, there has been a rapid increase in the use of computer-based sys-tems in areas such as railway traffic control, aircraft flight, telecommunications, and others, where failures can cost lives and/or money. This trend has led to concerns regarding the validation of the fault tolerance properties of these systems and the evaluation of their reliability.On the other side, the continuous increase in the integration level of electronic systems is making more difficult than ever to guarantee an acceptable degree of reliability, due to the occurrence of un-modeled faults and soft errors that can dra-matically affect the behavior of the system. As an example, the decrease in the magnitude of the electric charges used to carry and store information is seriously raising the probability that alpha particles and neutrons hitting the circuit could introduce errors in its behavior (often modeled as Single Upset Errors) [1].To face the above issues, mechanisms are required to increase the robustness of electronic devices and systems with respect to possible errors occurring during their normal function, and for these reasons on-line testing is now becoming a major area of research. No matter the level these mechanisms work at (hardware, system soft-ware, or application software), there is a need for techniques and methods to debug and verify their correct design and implementation.Fault Injection [2] imposed itself as a viable solution to the above problems. Sev-eral Fault Injection techniques have been proposed and practically experimented; they can basically be grouped into simulation-based techniques (e.g., [3][4]), soft-ware-implemented techniques (e.g., [5][6][7][8]), and hardware-based techniques (e.g., [9][10]).As pointed out in [2] physical fault injection (hardware- and software-implemented fault injection approaches) is more suited when a prototype of the system is already available, or when the system itself is too large to be modeled and simulated at an acceptable cost. Conversely, simulation-based fault injection is very effective in allowing early analysis of designed systems, since it can be exploited when a prototype is not yet available. The main disadvantage of simulation-based fault injection technique versus hardware- and software- ones is the high CPU time required to simulate the model of the system.In the last years, VHDL has become a de-facto standard for describing systems in particular when automatic synthesis tools are exploited; therefore, several research-ers have addressed the problem of how to perform fault injection campaigns on VHDL descriptions [3] [4]. These approaches are simulator-independent, i.e., injec-tion is performed through the adoption of special data types or fragments of VHDL code that are dedicated to modify the system behavior. They do not rely on simula-tor features, nor require the modification of simulation tools, therefore can easily fit on any design flow.The approaches proposed so far neglect the problem of reducing the time spent running fault injection campaigns. To deal with complex system new methods should be devised to minimize the time spent during simulations.In this paper we address the problem of improving the efficiency of simulation-based fault injection and we show how simulation time can be dramatically short-ened. The technique we developed analyzes the faults that will be injected in order to identify fault effects as early as possible and exploits the features provided by modern commercial VHDL simulators to speed-up injection operations. Our ap-proach comprises three steps:1.golden run executions: the system is simulated without injecting any faults anda trace file is produced, recording information on the system behavior. Moreo-ver, the state of the simulator is sampled and stored allowing to resume the simulation at a given time instant;2.static fault analysis: given an initial fault list, by exploiting the informationgathered during golden run computation, we identify those faults which effects on the system are known a-priori, and remove them from the fault list. This step exploits a sub-set of already proposed fault collapsing rules [11];3.dynamic fault analysis: during fault injection, the behavior of the system is pe-riodically compared with the golden run. The simulation is stopped as early as the effect of the fault on the system becomes known, i.e., either the fault alters the system behavior or the fault does not produce any effect.We exploit standard commands offered by commercial VHDL simulators for in-jecting faults and tracing system behavior. This technique minimizes the intrusive-ness of our approach and, by exploiting standard commands that are usually pro-vided by modern VHDL simulators, it is of general use.To assess the effectiveness of our technique, we performed fault injection ex-periments on a benchmark target system composed by a single microcontroller. Weanalyzed the behavior of several programs, and we recorded a speed-up ranging from 43.9% up to 96.6%.The remainder of this paper is organized as follows. Section 2 describes the sys-tem architecture where faults are injected. Section 3 describes the techniques we developed, while Section 4 reports some preliminary results assessing their effec-tiveness. Finally, Section 5 draws some conclusions.2 The target architectureThe system we considered is composed of an Intel i8051 microcontroller equipped with an external RAM memory storing the code the i8051 executes. All the programs we have considered have a data segment that fits in the i8051 internal memory composed of 128 bytes of static RAM; therefore our target architecture does not exploit an external RAM for storing data. The whole system is described in VHDL at the Register Transfer (RT) level.The fault model we are considering is the transient single bit flip. We injected faults in the following system components:•i8051 control registers and internal SRAM•external RAM storing the code.This assumption allows us to evaluate the effects of single transient faults both in the data or in the code.3 Proposed approachThe purpose of our approach is to minimize the time required for performing fault injection campaigns. We addressed this problem by performing fault analysis (before starting and during the fault injection campaign) and resorting to simulator commands that can be used to quickly reach injection time. The proposed approach is based on the assumption that the simulation runs are deterministic, i.e. for a given set of inputs there is only one trace of the system golden execution.To implement this approach the fault injection tool cooperates with a standard VHDL simulator, as Figure 1 shows. The fault injection manager issues commands (such as run commands or query commands) to the simulation back-end, which in turn sends responses to the Fault Injection manager.In the following subsections we will detail how our technique can be imple-mented; in particular, subsection 3.1 describes the information we gather on the behavior of the system during golden run execution, then subsection 3.2 shortly recalls the fault-collapsing rules we exploited and subsection 3.3 details how dy-namic fault analysis can be implemented. Finally, subsection 3.4 describes a tech-nique which exploits simulator facilities and that allows to save the most of the time required to reach injection time.Fig. 1. Fault injection tool overview3.1 Golden run executionThe purpose of this step is to gather information on the behavior of the system: given a set of input stimuli that will remain constant in the following fault injection campaigns, two sets of information are gathered, one for performing static fault analysis and one for performing dynamic fault analysis.Static fault analysis requires:•data accesses: whenever a data is accessed, the time, the type of access (read or write) and the address are stored;•register accesses: whenever a register is accessed, the time, the register name and the type of access are stored;•code accesses: at each instruction fetch, the address of the fetched instruction is stored in a trace file;We collect the needed information resorting to ad-hoc modules written in VHDL, called code/data watchers, that we insert in the system model (Figure 2). This ap-proach is not intrusive, since code/data watchers work in parallel with the system and do not affect its behavior.Conversely, for performing dynamic fault analysis we sample the state of the system with a given sampling frequency. The state of the system reports the content of the processor registers and the content of the data memory. We gather this infor-mation by periodically stopping the simulation and observing the system state re-sorting to simulator commands. The values gathered during sampling are stored in main memory, where we record the time at which the sample is taken, the contents of processor control registers and the content of the processor memory.This approach is very simple and effective because allows to capture snapshots of the system with zero intrusiveness. On the other hand, when addressing very large systems, it could require the availability of large amounts of both memory and disk space. As a consequence, the sampling frequency should be carefully selected.3.2 Static fault analysisFaults are removed from an initial fault list according to two sets of rules; one for faults intended to be injected in the data and one for faults in the code. The rules areapplied by analyzing the information gathered during golden run execution.We remove from the fault list a fault affecting data if it verifies at least one of the following conditions:1.given a fault f to be injected at time T at address A, remove f from the fault list ifA is no longer read after time T: this rule allows removing the faults that:−do not affect the system behavior, or−remain latent at the end of the simulation;2.given a fault f to be injected at time T at address A, remove f from the fault list ifthe very first operation that involves A after time T is a write operation.Conversely, we remove a fault in the code if it verifies the following condition: given a fault f to be injected at time T at address A, remove f from the fault list if the address A corresponds to an instruction that is no longer fetched after time T. This rule identifies faults that do not produce any effect and whose injection is therefore useless.Fig. 2. Modified system architecture3.3 Dynamic fault analysisDynamic fault analysis is based on the idea of identifying as early as possible the effect of the injected fault.As soon as the effect of a fault become evident, we stop the simulation, poten-tially saving a significant amount of simulation time.The fault injection routine we exploit is described in Figure 3.Fig. 3. Fault injection routineThe fault injection routine starts by settings a set of breakpoints in the VHDL code of the system. Breakpoints are a feature of modern VHDL simulators that of-fers a simple mechanism to capture the following situations:1.program completion: a breakpoint is set so that simulation is stopped after theexecution of the last instruction of the program running on the system;2.interrupt: in order to detect asynchronous events, a breakpoint is set to the VHDLstatements implementing the interrupt mechanism activation;3.time out: the simulation is started with a simulation time higher than the timerequired for program completion. A time out condition is detected if simulation ends and no breakpoint has been reached.After all the required breakpoints have been properly set, we simulate the system up to the injection time, then we inject the fault. Injection is done by exploiting the VHDL simulator commands to modify signals/variables in the VHDL source. After injection we start a loop where the system is simulated up to a sample point and the state of the system is compared with the information gathered during golden run execution.At each sample point, we check for the following situations:1.no failure: the state of the system is equal to the state of the golden run at thesame time, this implies that the fault effects disappeared from the system and that the fault has no effect on the system behavior; as a consequence, the simulation can be stopped;2.the state of the system does not match the golden run; in this case two alterna-tives are available:−failure: the fault has affected system outputs, therefore its effect on the system is known, and simulation can be stopped;−latent fault: the fault is still present in the system but it has not affected system outputs, and therefore further simulation is still required.3.4 Checkpoint-based optimizationsModern VHDL simulators offer several features that can be exploited to effec-tively reduce simulation time of fault injection campaigns. In particular, we ex-ploited the possibility of storing simulator state and then restoring it during simula-tions. The rationale behind this approach is shown in Figure 4.Fig. 4. Simulator-dependent optimizationGiven a fault f to be injected at time T , a not-optimized fault injection tool will spend a time equal to T setup to reach injection time. Conversely, during golden run execution, we sample the status of the simulator (and thus the status of the system under analysis) with a given frequency, and we store the information we obtain in a collection of system status files . Then, when fault f has to be injected, we resume the simulator from the first checkpoint before T (checkpoint 2 in the example of Figure 4 therefore, the time spent to reach injection time becomes T’’setup .Two conditions must be satisfied for this approach to be effective:1. let T R be the time for restoring the status of the system at a given checkpoint, the following inequality must hold:setup R setup T T T <+"(1)2. the size of the checkpoints collection should be kept as small as possible.As a consequence, the number of checkpoints should be carefully selected on the basis of both the time required for simulating the system and the size of the system.4 Experimental resultsTo evaluate the effectiveness of the proposed approach we wrote a prototypical implementation of the Fault Injection manager shown in Figure 1, which amounts to 790 lines of C code. During our experiments, we exploited Modeltech VSIM ver 5.1to run VHDL simulations.We wrote some simple benchmark programs and run them on the system archi-tecture described in Figure 2 which amounts to 6,700 lines of VHDL code (380 linesare devoted to implement CODE and DATA watchers). The benchmarks charac-teristics are summarized in Table 1.Table 1. Benchmarks descriptionFor each benchmark, we randomly selected 2,000 faults (1,000 in the data and 1,000 in the code) and we serially injected them in the system without resorting to any optimization. We then turned on dynamic fault analysis and checkpoint-based optimization and re-injected the selected faults. Finally, we collapsed the initial fault list resorting to static fault analysis and then injected the remaining faults. In the latter experiments dynamic fault analysis and checkpoint-based optimization are turned on. Results, gathered on a Sun SparcStation/5 running at 170 MHz and equipped with 128 Mbytes of RAM are reported in Table 2 and 3. Table 2 reports results gathered when injecting in the data, while Table 3 reports data gathered when injecting in the code. The columns have the following meaning:1.benchmark reports the name of the benchmark;2.T0 is the time required for injecting 1,000 faults (either in the data or in the code)when no optimizations are exploited;3.T1 is the time required by fault injection when dynamic fault analysis and simu-lator dependent optimization are exploited;4.T2 is the time required by fault injection when all the optimization previouslydescribed are exploited;5.1-T1/Tand 1-T2/Tare the speed-up we attain when the correspondent optimiza-tions are turned on.From the reported tables, we can observe that the complexity introduced in the Fault Injection manager to perform dynamic and static fault analysis and to exploit simulator facilities is worth paying, since it allows to speed-up simulated fault in-jection up to 96.6%. Moreover, static fault analysis plays a key role, since its adop-tions always double the attained speed-up.Our approach attains the best results when injecting faults in the data. This can be explained by considering that several faults exist that disappear from the system very soon after their injection (due to error detection and correction mechanisms or due to the system behavior) without affecting the system. Even if this faults cannot be eliminated by static analysis, the will be catch by dynamic analysis, thus saving a significant amount of CPU time.Conversely, when faults in the code are concerned, if a fault is injected because it fails static analysis, it remains latent during all the program execution. Therefore,simulation can be stopped only when fault effects reach system outputs or when the program ends.Table 2. Results on dataTable 3.Results on codeWe evaluated the performance of our approach when varying the number of checkpoints. We considered the BUBBLE benchmark and we run four fault injection campaigns where 100 faults are injected and respectively 5, 25, 50 and 100 check-points are used. We recorded the time and the disk occupation each campaign re-quired, and plotted them in Figure 5.Fig. 5. Space occupation versus timeAs this figure suggests, a trade-off exists between space required for storing checkpoints and the time for performing a fault injection campaign. For the bench-mark we considered, 25 checkpoints offer the best trade-off since the experiment requires approximately 7 Mbytes of disk space and injects 100 faults in 219 seconds.5 ConclusionsThis paper presented some techniques for reducing the time required for per-forming simulation-based fault injection campaigns. Static and dynamic methods are proposed to analyze the list of faults to be injected, removing faults as soon as their behavior is known. Common features available in most VHDL simulation environments are also exploited. 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