《航空工程技术英语》第二章习题

模块,节,知识点,题干,题型,难易度,答案,解析,选项A,选项B,选项C,选项D

第二单元AircraftSystem,2.1AircraftGeneral,,SETTHESWITCHTOTHREECYCLESAMINUTE,单选题,简单,B,,设置电门每秒钟三个循环,设置电门每分钟三个循环,设置电门每三分钟三个循环,

第二单元AircraftSystem,2.1AircraftGeneral,,Thepressurelinesdivideindifferentdirections.,单选题,简单,C,,压力管分布在另一个方向上,压力管分布在相同的方向,压力管分布在不同的方向,

第二单元AircraftSystem,2.1AircraftGeneral,,"Thesepartscaneasilybend,breakorbecomeincorrectlyaligned.",单选题,简单,C,,这些部件不容易弯曲、断裂或对不齐,这些部件很容易掰断、断裂或对不齐,这些部件很容易弯曲、断裂或对不齐,

第二单元AircraftSystem,2.1AircraftGeneral,,Usethetorquewrenchtotightentheboltsprogressively.,单选题,简单,C,,使用力矩扳手间隔拧紧螺栓。,使用扭力扳手按顺序拧紧螺栓。,使用扭矩扳手逐步拧紧螺栓。,

第二单元AircraftSystem,2.1AircraftGeneral,,Donottightentheboltswithtoomuchforce.,单选题,简单,C,,不要给螺栓施加过大力矩。,安装螺栓时不要用太大的力。,不要用太大的力来拧紧螺栓。,

第二单元AircraftSystem,2.1AircraftGeneral,,Differentwordingsareusedfortighteningthebolts.,单选题,简单,A,,拧紧螺栓时使用不同的措辞。,使用不同的扳手拧紧螺栓。,拧螺栓时使用不同的扭矩。,

第二单元AircraftSystem,2.1AircraftGeneral,,Removetheboltandthestop.,单选题,简单,A,,拆下螺栓和止动块。,拆下螺帽和挡板。,拆下螺钉和螺帽。,

第二单元AircraftSystem,2.1AircraftGeneral,,将螺栓、螺母、卡环或接头拧紧到正确的力矩。,单选题,非常简单,B,,"Tightenthethreads,nuts,clips,orconnectorstothecorrecttorque.","Tightenthebolts,nuts,clamps,orconnectorstothecorrecttorque.","Tightenthebolts,spacers,clips,orconnectorstothecorrecttorque.",

第二单元AircraftSystem,2.1AircraftGeneral,,从法兰上拆下铆钉。,单选题,非常简单,B,,Removetheboltsfromtheflange.,Removetherivetsfromtheflange.,Removetherivetsfromtheflanks.,

第二单元AircraftSystem,2.1AircraftGeneral,,抓住螺丝刀松开卡子。,单选题,非常简单,C,,Grabapliertoreleasetheclips.,Grabascrewdrivertoreleasethebolts.,Grabascrewdrivertoreleasetheclips.,

第二单元AircraftSystem,2.2AirframeME,,确保螺栓上的标记与手柄上的标记水平.,单选题,非常简单,B,,Makesurethatthemarkontheboltisalignedwiththemarkonthehandle.,Makesurethatthemarkontheboltislevelwiththemarkonthehandle.,Makesurethatthemarkontheboltisparalleltothemarkonthehandle.,

第二单元AircraftSystem,2.2AirframeME,,在两个螺栓的螺纹上涂抹少量机油。,单选题,非常简单,B,,Makealittleoiltothethreadsofthetwobolts.,Applyasmallquantityofoiltothethreadsofthetwobolts.,Applyasmallquantityofoiltothethreadsofthetwonuts.,

第二单元AircraftSystem,2.2AirframeME,,拆下四个螺栓中的一个。,单选题,非常简单,B,,Moveanyofthefourbolts.,Removeoneofthefourbolts.,Removeeachofthefourbolts.,

第二单元AircraftSystem,2.2AirframeME,,确保螺栓拧紧。,单选题,非常简单,A,,Makesurethattheboltsaretight.,Makesurethatthescrewsaresecurelyinstalled.,Makesurethattheboltsareloose.,

第二单元AircraftSystem,2.2AirframeME,,铆钉之间的距离参见图401。,单选题,非常简单,A,,RefertoFIG.401forthedistancebetweenrivets.,"Ifyouwanttoknowthedistancebetweenbolts,refertoFIG.401.",LookatFIG.401forthedimensionbetweenbolts.,

第二单元AircraftSystem,2.2AirframeME,,Itisnotpermittedtoinstallmorethantwowashersforeachbolt.,单选题,简单,B,,It'snoteasytoinstallmorethantwowashersforeachbolt.,Itisforbiddentoinstallmorethantwowashersforeachbolt.,Installingonewasherforeachboltisforbidden.,

第二单元AircraftSystem,2.2AirframeME,,泵安装在液压马达后面,单选题,非常简单,B,,Thegearboxisinstalledbehindthepneumaticmotor,thepumpisinstalledbehindthehydraulicmotor,Thepumpisinstalledbehindthepneumaticturbine.,

第二单元AircraftSystem,2.2AirframeME,,Anormalblankpageshallbeidentifiedontheprecedingpageonly.,单选题,一般,B,,Theprecedingpageshallonlyidentifyanormalblackpage.,Anormalblankpageshallonlyberecognizedonthepreviouspage.,Onlyanormalblankpageshallberecognizedonthepagethatfollows.,

第二单元AircraftSystem,2.2AirframeME,,Thefirststepinlistingpossiblecausesofeachtroublestoshowwhatsectionsofthesystemmaybeatfault,单选题,一般,C,,"oshowwhatsectionsofthesystemmaybeatfault,listingpossiblecausesofeachtrouble15thefirstthingweshoulddo.",Whatsectionsofthesystemmaybeatfaultdependsonthefirststepinlistingpossiblecausesofeachtrouble.,Toshowwhatsectionsofthesystemmaybeatfaultisthefirststepwhenyoulistpossiblecausesofeachtrouble.,

第二单元AircraftSystem,2.2AirframeME,,"Inthecaseofarevisiontoanillustration,ablackverticallineorablackhandmaybeutilizectocallattentiontothechangedportion.",单选题,一般,B,,"Inthecasethatarevisiontoanillustrationhappens,ablackverticallineorablackhandneecnotbeusedtofocusonthechangedpart.","Ifanillustrationistoberevised,youmayuseablackverticallineorablackhandtodrawattentiontothemodifiedpart.",Ablackverticallineorablackhandoughtnottobeutilizedtorevisetheillustrationanddrawattentiontothechangedpart.,

第二单元AircraftSystem,2.3AirframeAV,,DefinitionsshouldbewordedassimplyaspossibleandmustconformtotheuseofthedefinedtermsintheHandbook.,单选题,简单,A,,定义的措词应尽可能简单，并且必须与手册中定义的术语相符,定义的措词必须与手册中使用的定义术语一致，还应该用简单的方式来表达,定义的措词应简单并符合手册中的术语,

第二单元AircraftSystem,2.3AirframeAV,,"Fordataaboutthelocationofcircuitbreakers,refertothewiringlist.",单选题,简单,A,,关于跳开关的位置，参阅线路清单,关于电路开关的位置，参阅线路清单,关于电门的位置，参阅线路清单,

第二单元AircraftSystem,2.3AirframeAV,,"Ifthemicroswitchbecomesunserviceable,dothedeactivationprocedureoftheactuatortopreventdamagetothevalve.",单选题,简单,B,,若临近电门无法使用，执行作动筒的解除程序，以防止损坏活门,若微动电门无法使用，执行作动筒的解除程序，以防止损坏活门,若微动电门无法使用，执行活塞筒的失效程序，以防止损坏活门,

第二单元AircraftSystem,2.3AirframeAV,,当拉下低位的轴承时，可必看到低位的封圈,单选题,非常简单,B,,Thelowerwashercomesintoviewduringyoupullthelowergeardown.,Thelowersealcomesintoviewwhenyoupullthelowerbearingdown.,Thelowershimgoesoutofviewwhileyoupullthelowersheetdown.,

第二单元AircraftSystem,2.3AirframeAV,,打开活门，让氮气进入减震支柱,单选题,非常简单,C,,Openvalvetoadmitnitrogentothedragstrut.,Openthevalveandallownitrogentoentertheoleostrut.,Openthevalvetoletnitrogengointotheshockstrut.,

第二单元AircraftSystem,2.3AirframeAV,,接近1号液压系统的储压器,单选题,非常简单,A,,Getaccesstotheaccumulatorfortheno.lhydraulicsystem.,Getaccesstothereservoirfortheno.lhydraulicsystem.,Getaccesstotheaccumulatorfortheno.lfluidsystem.,

第二单元AircraftSystem,2.3AirframeAV,,不要吸入咨迎雾。,单选题,非常简单,C,,Donotbreathethesolventfumes,Donotbreathethesmoke.,Donotbreathethefumes.,

第二单元AircraftSystem,2.3AirframeAV,,"调整倾斜仪,直到气泡在中心。",单选题,非常简单,A,,Adjusttheclinometeruntilthebubbleisinthecenter.,Adjustthethermometeruntilthebubbleisinthecenter.,Adjustthehygrometeruntilthebubbleisinthecenter.,

第二单元AircraftSystem,2.3AirframeAV,,使用孔探仪葱内部检査燃烧室。,单选题,非常简单,B,,"Useaholeinstrumenttoexaminetheturbineinternally,",Useaborescopetoexaminethecombustorinternally.,Useaholeinstrumenttoexaminethecombustorexternally,

第二单元AircraftSystem,2.3AirframeAV,,如果在泵中发现金属颗粒，找到它们的来源并修复有缺陷的部分,单选题,非常简单,B,,"Ifyoufindmetalparticlesinthereservoir,findtheirsourceandrepairthebrokenpart,","Ifyoufindmetalparticlesinthepump,findtheirsourceandrepairthedefectivepart.","Ifyoufindmaterialparticlesinthepump,findtheirsourceandrepairthedamagedpart.",

第二单元AircraftSystem,2.4Structure,,确保伺服控制组件处于打开位置。,单选题,非常简单,C,,Makesurethattheservicecontrolunitisintheopenposition.,Makesurethattheservocontrolunitisintherightposition.,Makesurethattheservocontrolunitisintheopenposition.,

第二单元AircraftSystem,2.4Structure,,让部件的温度下降直到其与周围的温度一致,单选题,非常简单,B,,Letthetemperatureofthecomponentincreaseuntilitisthesameastheambienttemperature.,Letthetemperatureofhecomponentdecreaseuntilitisthesameastheambienttemperature.,Letthetemperatureofthecompounddecreaseuntilitisthesameastheambienttemperature.,

第二单元AircraftSystem,2.4Structure,,让部件的温度下降直到其与周围的温度一致。,单选题,非常简单,B,,Letthetemperatureofthecomponentincreaseuntilitisthesameastheambienttemperature.,Letthetemperatureofhecomponentdecreaseuntilitisthesameastheambienttemperature.,Letthetemperatureofthecompounddecreaseuntilitisthesameastheambienttemperature.,

第二单元AircraftSystem,2.4Structure,,化合物腐蚀在表格6001中有规定,单选题,非常简单,A,,Corrosionwiththechemicalcompoundisspecifiedmtable6001.,Corruptionwiththechemicalcompoundisspecifiedintable6001.,Corruptionwiththechemicalcompensationisspecifiedintable6001.,

第二单元AircraftSystem,2.4Structure,,若觉得发动机过热，将电门设置在”关”位。,单选题,非常简单,C,,"Iftheengineappearstobeheating,turnitoff.","Iftheengineappearstobeoverheating,turnitoff.","Ifyouthinktheengineistoohot,turntheswitchto""off""'.",

第二单元AircraftSystem,2.4Structure,,系统内的所有流量控制装置，如单向活门、燃油泵、储压器和继电器均应包括在内。,单选题,非常简单,A,,"Allflowcontroldeviceswithinthesystem,suchascheckvalves,fuelpumps,accumulators,andrelaysshouldbeincluded.","Allfluecontroldeviceswithin.thesystem,suchassinglevalves,fuelpumps,storage,andrelaysshouldbeincluded.","Allflowcontroldeviceswithinthesystem,suchassinglevalves,fuelpumps,accumulators,andrelaysshouldbeincluded.",

第二单元AircraftSystem,2.4Structure,,系统接口电路去适应连接系统的物理特性。,单选题,非常简单,C,,Thesysteminterconnectcircuitsadapttothephysicalpropertiesoftheconnectedsystems.,Thesysteminterfacecircuitsadapttothephysicalprotectionsoftheconnectedsystems,Thesysteminterfacecircuitsadapttothephysicalpropertiesoftheconnectedsystems,

第二单元AircraftSystem,2.4Structure,,Puttheblankingcapsontheopenendsofthetelescopicductandtheslatduct,单选题,简单,B,,在伸缩管和缝翼输送管的开口端盖上堵盖,在伸缩管和缝翼输送管的末端打开堵盖,在防冰管和缝翼输送管的末端打开堵盖,

第二单元AircraftSystem,2.4Structure,,Asecondarysystemisusedtoestimatethefuelquantitywhentheaircraftisontheground.,单选题,简单,A,,当飞机在地面时用来估计燃油量的辅助系统,当飞机在地面时用来计算燃油量的辅助系统,当飞机在地面时用来探测燃油量的辅助系统,

第二单元AircraftSystem,2.4Structure,,"Thepurposeofsuchtermsistoprovidedefinitionswhichareofpracticalvaluefortechnical

communication.",单选题,一般,C,,Theintentionofsuchtermsistoprovidedefinitionswhichhavepracticalvaluefortechnicalcommunication.,Theproposeofsuchtermsistoprovidedefinitionswithpracticalvaluefortechnicalcommunication.,Theaimofsuchtermsistoprovidedefinitionsforpracticingvaluabletechnicalcommunication.,

第二单元AircraftSystem,2.5PowerPlant,,Writethetemperatureontheenginerecordcard.,单选题,简单,C,,在发动机记录卡上填写记录,在室温下填写发动机记录卡,把温度写在发动机记录卡上,

第二单元AircraftSystem,2.5PowerPlant,,Returnlinesneednotbeshowninentiretyunlessneededtounderstandthesystem.,单选题,一般,B,,Youdonotneedtogivethereturnprocessesinitsentiretyunlessyouneedtocomprehendthesystem.,"Unlessyouneedtounderstandthesystem,fullyshowthereturnlines.",Returnproceduresneednotbeshowncompletelyifyouneedtorealizethesystem,

第二单元AircraftSystem,2.5PowerPlant,,ThesequenceoftopicsintheHandbookisintendedtoincreasein-flightusefulness.,单选题,一般,A,,TheorderoftopicsintheHandbookisintendedtoincreasein-flightusefulness.,ThesequenceoftopicsintheHandbookisintendedtoincreasein-flightuseless.,ThesequenceoftopicsintheHandbookispretendedtoincreasein-flightusefulness.,

第二单元AircraftSystem,2.5PowerPlant,,设置开关到打开位,单选题,非常简单,A,,Settheswitchtoon.,Movetheswitchtoon.,Puttheswitchtoon.,

第二单元AircraftSystem,2.5PowerPlant,,ThePILOTCALLswitchisontheP19externalpowerpanel.Thispanelisforwardofthenosewheelwellontherightsideoftheairplane.,单选题,简单,C,,飞行员呼叫开关位于P19表面电源面板上。该面板位于飞机右侧的前轮上方。,飞行员呼叫开关位于P19外部电源面板上。该面板位于飞机右侧的前轮上方。,飞行员呼叫开关位于P19外部电源面板上。该面板位于飞机右侧的前轮舱前方