航空专业词汇ooo

amyriadf数abradablelini易g磨涂层absorb吸收accelerati加速的accessory,accessor附件accompany伴随accomplish完成Acousticallyabsorbentmat吸声材料adiabati绝热的adjacent相邻的adoption采用aerate,aerating气供气aerofoilshape型形状aero航空的aftfa后风扇发动机airflc空气流量，空气流airstart空气起动机air-cooledbla气冷叶片airfoilsect翼型截面airstream=airflowairworthines飞行性能akin相似的aligh燃烧的alignment对中，同心alloyingeleme合金元素alloy合金alternat交替的altitudecru高空巡航altitud高度amountto占…比例，达到anchor,anchorin锚，固定angleofinciden攻角annular(combustion)chambe环形燃烧室annulus环型arrangement结构assemble装配atomizerflametu装有雾化喷嘴的火焰筒atomize使雾化attachment联接，安装attach联接，安装attai达到，实现attitud态度、姿态austenit奥氏体axial(flow)compres轴流压气机axia轴流的backpressui反压balanceou抵消balancin平衡ballbearigg珠轴承bedirectlyproportion…与too成正比beembodiedin体现在M中Beintheorder••达至I」…的量级Beinverselyproportiona•与1…成反比beinvolved…与…有关beopent与…相通bearing轴承bendingloa弯曲载荷bladings栅blis整体叶轮blis整体叶盘blow，blewblown吹boltedaxialj轴向螺栓联接boltedcenterline中心线螺栓联接bolt螺栓，用螺栓联结Bondedhoneycombstruetur粘接的蜂窝结构bond粘接boostert曾压器boost增压boundarylaye附面层,边界层breakup,breaking分p裂，破碎breakaway分离bridgeagapbetwe填补空白，使连接起来Britishthermalunit英国热量单位=252卡broadly主要地buffetingimpul扰流抖振脉冲but除 之外by-passairstre外涵道气流by-passengin双涵道发动机by-passrat涵道比calorificva热值camber弯度cannular(combustion)chamb环管燃烧室carbondioxi(二氧化碳carbonformatio积碳形成carbonmonoxide—氧化碳cartridgestai弹e药筒式起动机cast铸造Centeraround(about,at,in,on,round,・upon)•为中心centrifugal(flow)compressor离心压气机centrifugal离心的ceramiccoating陶瓷涂层charging进气choked壅塞,阻塞choke壅塞，阻塞chord弦chute斜道circumferential周向的clapper拍板clearance间隙coating涂层coaxial同轴的combustor燃烧室compactness紧凑性compact紧凑的compensatefor补偿componentfailure部件失效compression压缩compromise折中conduction传导conflict冲突conical锥形的consequently随之而来的,因此,所以consequent随之发生的，结果的constantpressure等压constantvolume等容construction结构consume消耗，使用contain包含，安装contraction收缩contribute提供conventionally常规地conventional常规的convergence收敛convergent-divergentnozzle收扩喷管conversely相反地conversion转换convert转换core核心corrosion腐蚀costeffective成本效益好的coupler联轴器couple耦合，联接coupling联轴器cracking产生裂纹create产生，形成create引起，产生creepfailure蠕变失效creepproperty蠕变性能creep蠕变crystal晶体cylinder汽缸cylindrical圆筒形的deLavalbulbroot圆头叶根decelerate减速deceleration减速decline下降deflection偏转deflection偏转degreeofreaction反力度delivery排气deliver送，流density密度departfrom偏离derive得到，取得designcondition设计状态designfeature设计特征desirable合乎需要的detachment拆开，分离detrimental=harmfuldevelopandmanufacture设计与制造diagrammatically图示地diffuservane扩散器叶片diffuser扩散器diffuse扩散dilute稀释dilutionzone掺混区dimple使起波纹directionalsolidification定向凝固discharge排出dispose布置disproportionately不相称地dissimilar不相似的,不同的distinct=differenttypedistortion扭曲，变形divergentnozzle扩散排气管dive俯冲

dominate起支配作用double-entryimpeller双面进气叶轮double-wallconstruction双壁结构downstream下游，顺流droplet小滴drum鼓筒dualalloydisc双金属轮盘Ductexhaustsystem排管道，用管道输送气系统ductedfan涵道式风扇发动机duct管道，用管道输送duration持续时间eddy涡流effect实现ejection喷射，喷出ejectoraction喷射器作用electricspark电火花electronic电子的eliminate消除elimination消除embody体现emission排放物employ采用encounter遇到encourage促进end-bend端弯endure承受enginenacelle发动机短舱enhance增强entail需要,要求equi-axed等轴的evolutionary发展，演变exceptionally格外地，特别地excessive过分的exertaninflueneeon…对…产生影响exhaustcone排气锥expel排出expenditure使用，消耗exposeMtoN使M暴露于Nextend延长extensive广泛的，大量的extinetion熄灭extinguisher灭火器extinguish熄灭extraet,extraetingto提取extract提取extremity端部fabricated装配式的fabricate制造failuredominate起支配作用double-entryimpeller双面进气叶轮double-wallconstruction双壁结构downstream下游，顺流droplet小滴drum鼓筒dualalloydisc双金属轮盘Ductexhaustsystem排管道，用管道输送气系统ductedfan涵道式风扇发动机duct管道，用管道输送duration持续时间eddy涡流effect实现ejection喷射，喷出ejectoraction喷射器作用electricspark电火花electronic电子的eliminate消除elimination消除embody体现emission排放物employ采用encounter遇到encourage促进end-bend端弯endure承受enginenacelle发动机短舱enhance增强entail需要,要求equi-axed等轴的evolutionary发展，演变exceptionally格外地，特别地excessive过分的exertaninflueneeon…对…产生影响exhaustcone排气锥expel排出expenditure使用，消耗exposeMtoN使M暴露于Nextend延长extensive广泛的，大量的extinetion熄灭extinguisher灭火器extinguish熄灭extraet,extraetingto提取haveabearingon…对…有影响hazard危险heatconduction热传导highoctanefuel高辛烷值燃料hold保持honeycomb蜂窝hydraulic液压的hydrocarbon碳氢化合物idlestroke空冲程idle,idling空载，慢速igniterplug点火塞ignite点燃ignitiontemperature燃点impartto…给与impeller叶轮implement实现,执,完成imposeupon…强加于…之上impractical不实际的impulseturbine冲击式涡轮inconjunctionwith…和…共同inconnectionwith关于，与…有关inexcessof超过inlinewith…与 一致inpreferenceto优先于inproportionto按比例inrelationto…对…来说insegments成组的inseries依次地inviewof考虑到incidence攻角incoming进来的incorporate安有，装有incorporate采用incorporation引入，采用incur招致induce吸入，引入，引导induction进气inferior差的ingestioncapability吸气能力ingestion吸气initialswirl预旋injection喷射，喷入inneredge内缘innerradius内半径

instability不稳定性instantaneous即刻的insulateMfromN使M与N隔离insulatingblanket隔热层insulation隔热，隔离intakechute进气斜道intakeduct进气管Integratednozzleassembly整体喷管部件intensity强度intention意图interceptor截击机interconnect互相连通interference干扰intermediatestage中间级intermediate中间的intermittent间断的interpose置于…之间intersect相交interstagebleed级间放气introduce,introducing输入involve需要，要求itfollowsthat因此，可见jetefflux喷射气流jetpipe尾喷管kerosene,cerosine煤油kerosene,kerosine煤油lag,lagging用隔热材料保护latitude纬度leakage泄漏legislatively立法地light,litorlighted点燃lightweightstrength低重强度limitingfactor限制因素liner衬筒longitude经度longitudinal纵向的lowby-passengine低涵道比发动机lowoctanefuel低辛烷值燃料machinedforging机加锻件maintainability维护性maintain保持margin欲度match匹配match使匹配meansection中间截面mean平均的metallurgist冶金学家meter,metering调节配量mid-span叶片中部mixerunit掺混装置mixturestrength混合物浓度mode模式momentum动量mount安装multiple(combustion)chamber分管燃烧室multi-spoolcompressor多转子压气机multi-stageturbine多级涡轮multi-stageunit多级装置negativeincidencestall负攻角失速nickelalloy镍合金nickelbasedalloy镍基合金nickel镍noisesuppressor消音器non-toxic无毒的notch切口，开槽nozzleguidevane涡轮导向叶片obsolete已不用obstacle障碍offset抵消operation工序optimumarrangement最佳结构optimum最佳(的)，最优(的)outletnozzle出口喷管outweigh胜过，重于overboard向船外，排出overhaul大修over-richpocket过富区oxidesofnitrogen氧化氮oxidization氧化oxidize氧化pass排送peak峰,峰值percentage部分，百分比perforatedflare带孔的喇叭管perform,performing完成，执行perimeter周边，圆周peripheral外围的,周边的periphery边缘

permissible允许的pl.尺寸，大小plenumchamber稳流室pneumatic气动的pollutant污染物positiveincidencestall正攻角失速powdermetallurgy粉末冶金precede在 前面pressurethrust压力推力prevail流行，胜利pre-vaporization预蒸发preventM(from)+ingprimarycombustionzone主燃区prime主要的progressively逐渐地progressive不断的，逐渐的promote促进，引起propagate传播propagation传播propellingnozzle推力喷管propfan桨扇发动机proportion比例provision提供Radiallydisposedvanes径向排列的叶片radially径向地range范围reactionturbine反作用式涡轮recirculation环流，回流recover重新获得reinforcedceramic力口固陶瓷relight重新点燃remainder剩余部分remainder剩余物residualwhirl乘0余旋流residual剩余的，剩余resistance抵抗，而寸restriction限制resultantthrust合成推力，总推力retainingring保持环retain保持reveal揭示，显示reverseflowsystem回流式系统revolve旋转richlimit富油极限rigiditytodensityratiorigiditytodensityratio刚度密度比rigid刚性的rimspeed轮缘速度robustsection坚固截面robust坚固，结实rollerbearing滚柱轴承rotatingguidevane旋转导流叶片rotorassembly转子部件rotorblade转子叶片rub碰磨ruggedness坚固性rugged坚固的secondaryairhole二股气流孔sectionalthickness截面厚度secure固定segment部分,片self-aligningcoupling自动调节联轴器self-sustained自持的serration榫齿serve起……作用servicelife使用寿命shaft轴showup表现shroudlessblade无冠叶片shroud叶冠singlecrystalblade单晶叶片skin蒙皮snout进气锥体snubber减振器soasto(do)为了solely=onlysolidforging实锻件sonic音速的space-launcher航天发射器specificfuelconsumption燃油消耗率spin旋转split分开spraynozzleatomizer喷嘴雾化器spraynozzle喷嘴spray喷雾stabilityloop稳定区stage阶段,级staggerangle斜罩角stagnant滞止的stainlesssteel不锈钢stall失速statorcasing静子机匣statorvane静子叶片stiffen加劲，固牢straightener整流器straighten整流straight-throughflowsystem直流式系统streamlinefairing流线型整流板strut支板strut支柱，支杆subsequent接下来的subsonic亚音速的substantially实际上，大体上substantially实质上，显著地succeedingstage下一级supercharge增压supersede代替，取代supersonic超音速的suppression抑制surge喘振surplus剩余的sustain承受得住sweep,swept扫，猛推sweptback后掠swirlvane旋流叶片swirl旋流tangential相切的taper，tapering带斜度，带锥度tensilestress拉应力terrifi