航空发动机专业英语词汇大全

航空发动机专业英语词汇大全，值得收藏！2016-01-29 航佳技术 飞机维修砖家(​https:​/​​/​mp.weixin.qq.com​/​s?__biz=MjM5NDE3NDUyNw==&mid=401707380&idx=2&sn=e978bd203d72f37233d8b17218f820bc&scene=2&srcid=02068cRDUB7UnVM5VuMEIGGQ&from=timeline&isappinstalled=0&key=10c44060274d23941f630203ee119912ec93f59a0c90772daeb0ccbc8256790bda28a44d8d00f849414d9dc098eb53ffffd3d314736b6d4d31bdea8c239f59a998bbb84ca5aa8f5b0393c1801d2d8f50&ascene=1&uin=NzA1NTE4NDYw&devicetype=Windows+7&version=6203005d&pass_ticket=ZktNIwM7uZosldUVLXkSSUAlKbcIHkT3M4Xx2OTffGgAk6wCdI8X7IcNhUhJXfEI&winzoom=1"\l"#​)Part1Para.1 gasturbineengine燃气涡轮发动机aircraft飞机，飞行器（单复同形）powerplant发动机，动力装置appreciate理解，意思到priorto在…之前propulsion推进reaction反作用jet喷气,喷射,喷气发动机designer设计师initially最初，开始时unsuitability不适应性pistonengine活塞发动机airflow空气流present带来,产生obstacle障碍Para.2patent专利,获得专利jetpropulsionengine喷气推进发动机athodyd冲压式喷气发动机heatresistingmaterial耐热材料develop研究出，研制出inthesecondplace其次inefficient效率底的ramjet,ramjet冲压式喷气发动机conception构想,设计，概念Para.3grant授予propulsivejet推进喷射turbo-jetengine涡轮喷气发动机turbojetturbo-propellerengine涡轮螺桨发动机turbopropVickersViscountaircraft维克斯子爵式飞机befittedwith配备term术语,称为,叫做twin-spoolengine双转子发动机triple-spoolengine三转子发动机by-passengine双涵道发动机ductedfan涵道风扇发动机unductedfan(UDF)无涵道风扇发动机propfan桨扇发动机inevitable不可避免的,必然的p.4propeller螺旋桨   basicprinciple基本原理effect产生propel推进solely单独,只thrust推力p.5popularly普遍地,一般地pulsejet脉动式喷气发动机turbo/ramjet涡轮冲压式喷气发动机turbo-rocket涡轮火箭p.6accelerate加速acceleration加速度apparatus装置,机器slipstream滑流p.7momentum动量issue冒出toimpartMtoN把M给与Nrevolve旋转p.8whirl旋转sprinkler喷水器mechanism机构by[in]virtueof依靠hose软管afford提供carnival狂欢节p.9definitely确切地,明确地assume想象,以为expel排出,驱逐propulsiveefficiency推进效率Page3p.10differ不同convert转换p.11thermodynamic热动力的divergent扩散diverge扩散convergent收敛converge收敛entry进气段exit排气管kineticenergy动能airintake空气进口   divergingduct扩散管道outletduct排气管missile导弹targetvehicle靶机p.12intermittentcombustion间断式燃烧aerodynamic空气动力的involve具有robust结实的,坚固的inletvalve进气阀inject喷入eject喷出depression降压,减压exhaust排气cycle循环helicopterrotorpropulsion 直升飞机旋翼驱动器dispensewith省去,无需resonate共振resonatingcycle共振循环fuelconsumption燃油消耗equal比得上performance性能p.13decompose分解p.14inherent固有的draw吸入p.15arrangement结构simplicity简单性subsequent接下来的thermodynamic热力的Page7p.16disturbance扰动blade-tip叶尖departurefrom背离p.17offset抵消exceed超过p.18Machnumber马赫数p.19variableintake可变进口afterburning加力燃烧 variablenozzle可调喷口conventional常规的afterburner加力燃烧室inoperative不工作的divert使转向guidevane导流叶片duct管道，用管道输送sustained持续的cruise巡航mode模式p.21multi-stageturbine多级涡轮derive得到，取得kerosene,kerosine煤油beintheorderof…达到…的量级spray喷雾fuel-richmixture富油混合物dilute稀释surplus剩余的p.22interceptor截击机space-launcher航天发射器altitude高度attitude态度、姿态latitude纬度longitude经度accelerative加速的duration持续时间 Part2Para.1workingfluid工作流体conversion转换jetefflux喷射气流Para.2four-strokepistonengine四冲程活塞发动机constantpressure等压constantvolume等容induction进气compression压缩intermittent间断的beinvolvedin…与…有关charging进气eliminate消除idlestroke空冲程Para.3peak峰,峰值fluctuate,fluctuating波动,起伏withstand,withstood承受inexcessof超过employ采用cylinder汽缸highoctanefuel高辛烷值燃料lowoctanefuel低辛烷值燃料fabricated装配式的Para.4function运行,运转introduce,introducing输入remainder剩余部分discharge排出Para.5,6turbineassembly涡轮部件air-cooledblade气冷叶片consequently随之而来的,因此,所以Para.7embody体现beembodiedinM体现在M中bedirectlyproportionalto…与…成正比 beinverselyproportionalto…与…成反比Para.9trace描绘showup 表 关于同志近三年现实表现材料材料类招标技术评分表图表与交易pdf视力表打印pdf用图表说话 pdf 现Para.10attain达到,实现conversely相反地Para.11adiabatic绝热的friction摩擦conduction传导turbulence紊流Para.12propellingnozzle推力喷管momentum动量deceleration减速Page14Para.13effect实现conversion转换convert转换sonic音速的subsonic亚音速的supersonic超音速的encounter遇到venturi文氏管Para.14interference干扰componentfailure部件失效eddy涡流turbulence紊流Para.15frontalarea迎面面积straight-throughflowsystem直流式系统reverseflowsystem回流式系统subsequent接下来的Para.17conventionally常规地percentage部分，百分比duct管道，用管道输送remainder剩余物deliver送，流tobeconduciveto…有利于…specificfuelconsumption燃油消耗率Para.18designfeature设计特征by-passengine双涵道发动机by-passratio涵道比twin-spoolconfiguration双转子结构propfan桨扇发动机turbo-propeller涡轮螺桨发动机Para.19by-passairstream外涵道气流overboard向船外，排出ductedfan涵道式风扇发动机aftfan后风扇发动机 Part3Para.1centrifugal离心的axial轴流的couple耦合，联接coupling联轴器coupler联轴器shaft轴Para.2centrifugal(flow)compressor离心压气机impeller叶轮diffuser扩散器axial(flow)compressor轴流压气机multi-stageunit多级装置alternate交替的rotorblade转子叶片statorvane静子叶片diffuse扩散boost增压booster增压器Para.3withregardto关于robust坚固，结实developandmanufacture设计与制造consume消耗，使用attain达到airflow空气流量，空气流adoption采用favour(Am.E favor)喜爱，偏爱ruggedness坚固性 rugged坚固的outweigh胜过，重于Fig.3-1rotatingguidevane旋转导流叶片intakechute进气斜道swirlvane旋流叶片Para.5diffuservane扩散器叶片double-entryimpeller双面进气叶轮plenumchamber稳流室Para.6induce吸入radially径向地intakeduct进气管initialswirl预旋Para.7divergentnozzle扩散排气管Para.8tipspeed叶尖速度Para.9maintain保持leakage泄漏clearance间隙Para.10construction结构centeraround(about,at,in,on,round,upon)… 以…为中心ballbearing滚珠轴承rollerbearing滚柱轴承split分开detachment拆开，分离Para.11forged锻造的radiallydisposedvanes径向排列的叶片inconjunctionwith…和…共同sweptback后掠Para.12attach联接tangential相切的inneredge内缘inlinewith…与…一致buffetingimpulse扰流抖振脉冲Para.13rotorassembly 转子部件airfoilsection   翼型截面mount  安装bearing  轴承incorporate  安有，装有inseries  依次地designcondition  设计状态incorporation  引入，采用variablestatorvane  可调静子叶片succeedingstage下一级Para.14gradualreduction 逐渐减小annulus  环型statorcasing  静子机匣maintain  保持density  密度convergence  收敛taper，tapering  带斜度，带锥度arrangement  结构Para.16multi-spoolcompressor多转子压气机optimum 最佳（的），最优（的）flexibility 适应性，灵活性Para.17handle  处理duct  管道，用管道输送exhaustsystem 排气系统propellingnozzle  推力喷管match 使匹配obsolete  已不用but  除…….之外Para.18trend  趋势stage  阶段,级undergo  承受split  分开core  核心gasgenerator  燃气发生器optimumarrangement  最佳结构Para.19induce  吸入，引入，引导sweep,swept  扫，猛推adjacent  相邻的translate  翻译，转换decelerate  减速serve  起……作用deflection  偏转straightener  整流器swirl  旋流diagrammatically  图示地accompany  伴随progressive  不断的，逐渐的Para.20breakaway 分离stall 失速precede 在……前面Para.21incidence  攻角tolerate  允许interstagebleed   级间放气intermediatestage  中间级Para.22proportion    比例  pl. 尺寸,大小coaxial  同轴的innerradius  内半径supercharge  增压akin 相似的Para.23tocenteraround(round,on,upon,about,at,in)… 以…为中心alignment对中,同心cylindrical圆筒形的boltedaxialjoint轴向螺栓联接boltedcenterlinejoint中心线螺栓联接Para.24secure固定assemble装配weld焊接periphery边缘drum鼓筒Para.25circumferential周向的fixing安装,固定maintainability维护性blisk整体叶盘Para.26gradient梯度balanceout抵消twist扭angleofincidence攻角boundarylayer附面层,边界层stagnant滞止的compensatefor补偿camber弯度extremity端部end-bend端弯Para.27retainingring保持环insegments成组的shroud叶冠Para.28dissimilar不相似的,不同的workable可用的,可运转的implement实现,执行,完成retain保持Para.29imposeupon…强加于…之上departfrom偏离intention意图positiveincidencestall正攻角失速negativeincidencestall负攻角失速blading叶栅sustain承受得住surge喘振instantaneous即刻的expel排出margin欲度instability不稳定性Para.30provision提供margin欲度hydraulic液压的pneumatic气动的electronic电子的Para.31costeffective成本效益好的prevail流行，胜利Para.32rigid刚性的clearance间隙alloy合金nickelbasedalloy镍基合金titanium钛inpreferenceto优先于rigiditytodensityratio刚度密度比Para.33prime主要的fatiguestrength疲劳强度notch切口，开槽ingestion吸气inferior差的decline下降rub碰磨ignite点燃airworthiness飞行性能hazard危险Para.34dominate起支配作用Para.35solidforging实锻件chord弦mid-span叶片中部snubber 减振器clapper 拍板fabricate制造skin蒙皮honeycomb蜂窝Para.36robustsection坚固截面ingestioncapability吸气能力  Part4Para.1fuelsupplynozzle燃油喷嘴extensive广泛的，大量的accomplish完成Para.2range范围C---CentigradeorCelsiusturbinenozzle涡轮导向器Para.3consequent随之发生的，结果的Para.4kerosene,cerosine煤油light,litorlighted点燃blow,blew，blown吹alight燃烧的Para.5flametube火焰筒liner衬筒meter,metering调节配量Para.6snout进气锥体downstream下游，顺流swirlvane旋流叶片perforatedflare带孔的喇叭管primarycombustionzone主燃区upstream上游，逆流promote促进，引起recirculation环流，回流Para.7secondaryairhole二股气流孔toroidalvortex喇叭口形涡流anchor,anchoring锚，固定hasten促进，加速droplet小滴ignitiontemperature燃点Para.8conical锥形的intersect相交turbulence紊流breakup,breakingup分裂，破碎incoming进来的Para.9nozzleguidevane涡轮导向叶片amountto占…比例,达到progressively逐渐地dilutionzone掺混区remainder剩余物insulateMfromN使M与N隔离Para.10,11electricspark电火花igniterplug点火塞self-sustained自持的Para.12airstream=airflowdistinct=differenttypeinjection喷射，喷入ejection喷射，喷出atomize使雾化spraynozzle喷嘴pre-vaporization预蒸发Para.13vapor蒸汽vaporize蒸发vaporizer蒸发器feedtube供油管vaporizingtube蒸发管atomizerflametube装有雾化喷嘴的火焰筒Para.14multiple(combustion)chamber分管燃烧室tubo-annular(combustion)chamber环管燃烧室cannular(combustion)chamber环管燃烧室annular(combustion)chamber环形燃烧室Para.15F.g.4-6Para.16dispose布置delivery排气Para.17interconnect互相连通propagate传播Para.18bridgeagapbetween填补空白，使连接起来evolutionary发展，演变arrangement结构overhaul大修compactness紧凑性Para.19contain包含，安装beopento与…相通Para.20elimination消除propagation传播Para.21virtually实际上oxidize氧化carbonmonoxide一氧化碳non-toxic无毒的carbondioxide二氧化碳Para.22aerate,aerating吹气，供气over-richpocket过富区fuelvapour燃油蒸汽carbonformation积碳形成Para.23incur招致extinction熄灭relight重新点燃perform,performing完成，执行spraynozzleatomizer喷嘴雾化器Para.25intensity强度compact紧凑的exceptionally格外地，特别地Para.26calorificvalue热值Britishthermalunit(BTU)英国热量单位=252卡expenditure使用，消耗Para.27altitudecruise高空巡航Para.29weaklimit贫油极限richlimit富油极限extinguish熄灭 extinguisher灭火器dive俯冲idle,idling空载，慢速mixturestrength混合物浓度Para.30stabilityloop稳定区Para.32emission排放物pollutant污染物create产生，形成legislatively立法地hydrocarbon碳氢化合物oxidesofnitrogen氧化氮Para.34suppression抑制desirable合乎需要的conflict冲突compromise折中combustor燃烧室substantially实际上Para.35coating涂层insulation隔热，隔离Para.36corrosion腐蚀creepfailure蠕变失效fatigue疲劳Part5Para.1accessory,accessories附件solely=onlyextract,extracting提取toexposeMtoN使M暴露于NMisexposedtoNPara.2torque扭矩Para.3intermediate中间的interpose置于…之间tobederivedfrom…从…获得,取自free-powerturbine自由动力涡轮tobeindependentof…不受…的限制Para.4mean平均的deflection偏转inproportionto按比例sectionalthickness截面厚度disproportionately不相称地Para.5broadly主要地aerofoilshape翼型形状impulseturbine冲击式涡轮reactionturbine反作用式涡轮incorporate采用cartridgestarter弹药筒式起动机airstarter空气起动机Para.7toforceone’swayinto有力地冲入spin旋转whirl旋转Para.8tobegovernedby取决于,由…决定substantially实际上,大体上excessive过分的residual剩余的，剩余detrimental=harmfulstrut支柱,支杆Para.9twist,twisted带扭向的staggerangle斜罩角Para.10meansection中间截面Para.12self-aligningcoupling自动调节联轴器Para.15machinedforging机加锻件flange法兰，安装边bolt螺栓，用螺栓联结perimeter周边，圆周tohaveprovisionfor…为…作好准备attachment联接,安装Para.16heatconduction热传导Para.17degreeofreaction反力度Para.18fix确定,决定,trailingedge排气边soasto(do)为了preventM(from)+ingPara.19attach联接,安装fixing联接haveabearingon…对…有影响rimspeed轮缘速度deLavalbulbroot圆头叶根supersede代替,取代fir-treefixing纵树榫头联接involve需要,要求serration榫齿stiffen加劲,固牢Para.20contraction收缩shroud叶冠fit配备,安装segment部分,片peripheral外围的,周边的abradablelining易磨涂层A.C.C.---activeclearancecontrolshroudlessblade无冠叶片Para.21revolve旋转extract提取conventional常规的Para.22impractical不实际的dualalloydisc双金属轮盘blisk整体叶轮cast铸造bond粘接Para.23match匹配nozzleguidevane涡轮导向叶片backpressure反压surge喘振choke壅塞，阻塞Para.24obstacle障碍impartto…给与tensilestress拉应力limitingfactor限制因素Para.25endure承受nickelalloy镍合金ceramiccoating陶瓷涂层enhance增强Para.26resistance抵抗，耐fatiguecracking疲劳破坏Para.27ferritic铁素体 terrific可怕的，极妙的austenitic奥氏体alloyingelement合金元素extend延长fatigueresistance抗疲劳性powdermetallurgy粉末冶金Para.28inconnectionwith关于，与…有关glowingred-hot赤热发光ounce 盎施=28.35gbendingload弯曲载荷thermalshock热冲击corrosion腐蚀oxidization氧化Para.29foregoing前面的,上述的itfollowsthat因此,可见permissible允许的metallurgist冶金学家Para.30creep蠕变finiteusefullife有限使用寿命failure失效Para.31forge锻造forging锻件cast铸造creepproperty蠕变性能fatigueproperty疲劳性能Para.32reveal揭示,显示amyriadof无数crystal晶体equi-axed等轴的servicelife使用寿命directionalsolidification定向凝固usefulcreeplife有效蠕变寿命singlecrystalblade单晶叶片substantially实质上,显著地Para.33reinforcedceramic加固陶瓷Para.34balancing平衡operation工序inviewof考虑到Part6Para.1aero航空的pass排送resultantthrust合成推力，总推力create引起，产生contribute提供absorb吸收exertaninfluenceon…对…产生影响jetpipe尾喷管propellingnozzle推力喷管outletnozzle出口喷管Para.2distortion扭曲,变形cracking产生裂纹Para.3thrustreverser推力反向装置noisesuppressor消音器entail需要,要求lowby-passengine低涵道比发动机mixerunit掺混装置encourage促进Para.4exhaustcone排气锥hold保持residualwhirl剩余旋流strut支板straighten整流Para.5inrelationto…对…来说choked壅塞,阻塞upstreamtotalpressure上游总压pressurethrust压力推力momentum动量Para.6wastage损失,消耗withadvantage有效地convergent-divergentnozzle收扩喷管recover重新获得Para.7flared扩张的restriction限制progressively逐渐地longitudinal纵向的Para.9fixedareanozzle固定面积喷口variableareanozzle可变面积喷口offset抵消Para.13nickel镍titanium钛ventilate,ventilating通风lag,lagging用隔热材料保护insulatingblanket隔热层fibrous纤维状的stainlesssteel不锈钢dimple使起波纹acousticallyabsorbentmaterial吸声材料Para.14double-wallconstruction双壁结构induce引导ejectoraction喷射器作用enginenacelle发动机短舱Para.15streamlinefairing流线型整流板venthole通气孔Para.16chute斜道bondedhoneycombstructure粘接的蜂窝结构integratednozzleassembly整体喷管部件lightweightstrength低重强度（注：文档可能无法思考全面，请浏览后下载，供参考。可复制、编制，期待你的好评与关注！）