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機務(wù)職稱英語1

1

.fuselage機身

2.

.Antenna天線

3.

.Hatch艙口

4.

5.Terminate終止

.

6.isolationvalve隔離活門

.

7.monocoque硬殼式

.skid滑撬

8.

.dorsalfin脊鰭

9.

1也landinggear起落架

11accessdoor檢修口

12verticalstabilizer垂直安定面

13structure結(jié)構(gòu)

1bullockline縱剖線

4.pressurization增壓

1

pneumatics氣源系統(tǒng)

15&.

obtain得到

1Z

connector接頭

1&

19starter啟動器

2hydraulics液壓系統(tǒng)

2OL.cowl整流罩

2

2potablewater飲用水

21horizontalstabilizer水平安定面

2appropriate適當?shù)?/p>

4.manifold總管

25.

26.shaft軸

27&.coolingpack冷卻組件

2redistribution再分配

29.filter過濾器

0.

3Lextension延伸

Z

3outflowvalve外流活門

3工cruise巡航

3curveA曲線

4.

destination目的地

35&.

3ambient環(huán)境

37&.isolation隔離

3pressuredifferential壓差

39.extinguisher滅火器

30L.designate標明

42float浮子

4warning警告

3.battery電瓶

44.

45&.attenuator消音器

4solidline實線

4checkvalve單向活門

4antiskit防滑

nozzle噴咀

47.accelerate加速

48.hoist吊車

49.receptacle插座

50.compute計算

51.heading航向

52.stepclimb分段爬升

53.supplement補充

54.compass羅盤刻度盤

55.airborne機載的

56.reflection反射

57.collision碰撞

58.moisture溫度

59.component部件

60.module組件

61.actuator作動筒

62.drain排放

63.faulty出故障的

64.gasket墊圈

65.diode二極管

66.magnate磁鐵

67.optimum最佳

68.autopilot自動駕駛儀

69.engine發(fā)動機

70.disengage斷開

71.rectifier整流器

72.buffer緩沖

73.fueling加燃油

74.capacitance電容

75.shockstrut減震支柱

76.aileron副翼

77.turbine渦輪

78.detector探測器

79.leakage泄漏

80.accomplish完成

81.alarm警報

82.specify指定

83.sensor傳感器

84.install安裝

85.diluter稀釋器

86.cylinder氣缸

87.mask面罩

88.gage壓強計

89.latch鎖定

90.emergency緊急情況

91.release放行

92.mechanism機制

93.manually人工地

94.generator發(fā)電機

95.regulator調(diào)節(jié)器

96.vent通氣

97.coating涂層

98.fitting裝置

99.impact沖擊

100.probe探頭

101.vane葉片

102.conductive導(dǎo)電的

103.formation形成

104.strength強度

105.integrate結(jié)合

106.dielectric絕緣的

107.slat縫翼

108.repellent防雨劑

109.cylindrical圓筒形的

110.capacity容積

111.transmitter發(fā)射機

112.controlstand控制臺

113.illumination照明

114.lighting照明

115.performance性能

116.intensity亮度

117.integral完整的

118.shield屏蔽

119.fluorescent發(fā)熒光的

120.floodlight泛光燈

121.clockwise順時針方向的

122.incandescent白熾的

123.quadrant計量器

124.amplifier放大器

125.inverter變流機

126.charger充電機

127.flap襟翼

144.switch電門

145.idle慢車

146.rack支架

147.alternatingcurrent交流

148.conversion轉(zhuǎn)換

149.commutator換向器

150.backup備用

151.frequency頻率

152.exciter勵磁器

153.stator定子

154.databus數(shù)據(jù)總線

155.electricalload電荷

156.compound化合物

157.fastener堅固件

158.joint接頭

159.boostpump增壓泵

160.transfer轉(zhuǎn)換

161.subdivide細分

162.defueling放油

163.chip芯片

164.decode解碼

165.graduate刻度

166.utilize利用

167.overfill過滿

168.feed供油

169.seal密封

170.baffle緩沖隔板

171.non-returnvalve單向活門

172.crossfeed交輸

173.responsibility責(zé)任

174.elevator升降舵

175.spoiler擾流板

176.reservoir油箱

177.teailingedge后緣

178.alternate備用

179.eschanger交換器

180.relief消除

181.lubricant潤滑劑

182.rudder方向舵

183.thrustreverser反推裝置

184.configuration形態(tài)

185.inoperative不工作的

186.malfunction故障

187.solenoid電磁線圈

188.dragbrace阻力桿

189.depressurize減壓

190.taxi滑行

191.disa解除預(yù)位

192.elevation標高

193.bolt

A螺帽B螺栓C螺釘D螺絲B

194.stability

A穩(wěn)定性B安定面C標準化D靈敏度A

195.towbar

A扭矩B扭力管C扭力臂D牽引桿D

196.servomotor

A伺服機構(gòu)B服務(wù)監(jiān)控C伺服馬達D勤務(wù)機構(gòu)C

197.dragbrace

A阻力桿B阻力連桿C偏流角D集油盤A

198.maneuver

A委托B管理C機動D處理C

199.longitudinalaxis

A橫軸B縱軸C縱剖線D環(huán)形線B

200.lateralaxis

A橫軸B縱軸C軸流式D當?shù)卮咕€A

201.lift

A重力B升力C阻力D推力B

202.trim

A配平B斷開C桁架D平移A

203.position

A定位B定位器C穩(wěn)定D穩(wěn)定器A

204.attitude

A高度B緯度C姿態(tài)D校準C

205.annular

A圓柱形的B方形的C刀形的D環(huán)形的D

206.controlsurface

A舵面B操縱桿C駕駛桿D操縱臺A

207.establish

A基本B穩(wěn)定C建立D排氣C

208.magnitude

A磁鐵B粉品紅C尺寸D強制C

209.rotate

A安裝B轉(zhuǎn)動C調(diào)節(jié)D復(fù)位B

210.refair

A反射B不公平C再分配D再成流線型D

211.balance

A平衡B緩沖C傾斜D擋板A

212.feedback

A反射B饋線C反饋D供油C

213.transducer

A整流器B消音器C變壓器D傳感器D

214.torquetube

A扭力管B扭力臂C阻力桿D阻力連桿A

215.pitch

A轉(zhuǎn)彎B俯仰C橫滾D荷蘭滾B

216.roll

A俯仰B橫滾C升降D旋轉(zhuǎn)B

217.tab

A膠帶B滑行C配平D調(diào)整片D

218.axialflow

A橫軸B縱軸C軸流D氣流C

219.bypassratio

A旁通活門B接近速率C傳播速度D函道比D

220.combustion

A組合B燃燒C控制D補充B

221.blockage

A刀形B環(huán)形C堵塞D隔板C

222.booster

A增壓泵B吊桿C支架D助推器U____________________一批注[hl]:書簽

223.shroud

A屏蔽B套筒C防護罩D擱板c

224.inlet

A入口B出口C內(nèi)流D軸流A

225.indicator

A標高B索引C點火器D指示器D

226.seaenge

A供油B饋線C回油D搜索C

227.rotor

A定子B轉(zhuǎn)子C路線D方向舵B

228.bearing

A基座B支座C吊桿D軸承D

229.segment

A部分B整體C順序D傳送A

230.precooler

A冷卻器B預(yù)冷器C預(yù)測D預(yù)防措施B

231.ingition

A點火B(yǎng)識別C照明D指示A

232.spark

A火花B梁C彈簧D停留D

233.triaxial

A氣流的B軸流的c三維的D通過的C

234.sleeve

A支柱B支座c套筒D滑環(huán)C

235.translate

A發(fā)射B接收c轉(zhuǎn)換D移動D

236.parameter

A參數(shù)B平行c段落D稀釋A

237.esceed

A擴展B施加c超出D延伸C

238.torque

A扭矩B扳扭c扭力管D扭力臂A

239.reset

A定位B復(fù)位c返回D修改B

240.inspection

A尊敬B完善c檢查D安裝C

241.centrifugal

A向心的B離心的c共心的D三維的B

242.override

A駕駛B過熱c過滿D超控D

243.contamination

A繼續(xù)B污染C轉(zhuǎn)換D通信B

244.hermetical

A重的B危險的C十六進制D密封的D

245.interface

A互換B接口C干擾D互鎖B

246.muffler

A緩沖隔板B消音器C混合物D稀釋器B

247.de-energize

A通電B斷電C銜接D降壓B

248.initiate

A禁止B裝有C起始D結(jié)束C

249.energize

A能量B銜接C通電D斷電C

250.plug

A插頭B插座C聚合物D混合物A

251.circuitry

A回路B電路C電路板D整套電路D

252.radial

A徑向的B三維的C雷達罩D背面的A

253.compressor

A燃燒室B壓氣機C計算機D部件B

254.coil

A線圈B支架C線聯(lián)D環(huán)A

255.polarity

A極性B磁極C優(yōu)先權(quán)D概率A

256.detent

A鎖定B探測C確定D下降A(chǔ)

257.achieve

A加速B肯定C完成D啟動C

258.discharger

A充電機B排氣裝置C簽派人D斷開B

259.spring

A旋轉(zhuǎn)B火花C彈簧D滑動C

260.contactor

A接觸器B容器C導(dǎo)體D換向器A

261.slotted

A有槽的B刀形的C環(huán)形的D縫翼的A

262.identification

A相同B點火C識別D照明C

263.deviation

A確定B裝置C目的地D偏離D

264.absoluteheight

A相對高度B絕對高度C截獲高度D損失高度B

265.accumuate

A堆積B備用C接近D作動A

266.pitotpressure

A全壓B靜壓C按壓D過壓A

267.staticpressure

A全壓B靜壓C過壓D增壓B

268.optimize

A選擇B最優(yōu)化C取向D光導(dǎo)B

269.profile

A平面B剖面C規(guī)劃D預(yù)測B

270.discrete

A離散的B無效的C審慎的D絕緣的A

271.summation

A補充B監(jiān)視C累加D抑制C

272.descend

A上升B下降c展開D壓下B

273.ascend

A上升B下降c裝配D指定A

274.suppression

A補充B代替c累加D抑制D

275.aitimeter

A高度表B壓力表c油量表D傾斜儀A

276.annunciation

A指示B指示器c天線D衰減器A

277.memory

A信息B儲存器c調(diào)制D瞬時B

278.monochromatic

A單色的B單調(diào)的c瞬時的D縮小的A

279.revert

A復(fù)位B修改c返回D拉油門C

280.concentric

A同心的B離心的c導(dǎo)電的D絕緣的A

281.compatible

A適用的B不適用的c兼容的D不兼容的A

282.impedance

A沖擊B阻塞c阻抗D變形C

283.orientation

A定位B起源c優(yōu)化D全向A

284.nozzle

A指針B槽c消音器D噴嘴D

285.oscillator

A振蕩器B多諧振蕩器c監(jiān)視器D定位器A

286.perpendicular

A水平的B垂直的c向心的D離心的B

287.velocity

A證實B速率c變化D速度D

288.Propagation

A頻率B比例c傳播D預(yù)測C

289.schematic

A順序B定期C計劃D簡圖D

290.surveillance

A監(jiān)視B調(diào)查C抑制D補充A

291.update

A過期B更新C改裝D利用B

292.expiration

A有效期B截止期C擴展D延伸B

293.deform

A形式B變形C突出D規(guī)定B

294.squat

A靜噪B抑制C起飛D著陸D

295.subsonic

A載波B亞音速的C超音速的D副載波B

296.inertial

A起始B慣性C惰性D起燃B

297.manipulation

A處理B機動C總管D強制A

298.alignment

A聯(lián)合B校準C分派D環(huán)境B

299.accelerometer

A傾斜儀B加速度表C計量儀D附件裝置B

300.increment

A裝置B降低C提高D增量D

301.Thepressurizationsystemcontrolscabin_byregulatingairflowfromthe

fuselage.(B)

AattitudeBaltitudeClatitudeDlongitude

302.Theflightcontrolsprovideliftfortakeoffandlandingasincreasedaerodynamic

—bothinflightandontheground.(B)

AliftBdragCthrustDgravity

303.Movingthe_outoftheirtrimmedpositioncausestheairplanetorotateandchange

attitude.(C)

AelevatorBrudderCaileronDflap

304.Theairconditioningpackssupplyconditionedairintothe_system.(C)

AdepressionBsuppressionCpressurizationDdepressurization

305.Thewindowheatsystemconsistsof_coatingsinthewindowsstructureheatcontrol

units,controlandindications.(A)

AconductiveBdielectricCconduciveDhermetical

306.ThedistributionsystemallowsfueltobesuppliedtotheenginesandAPU.The_

valveallowsfromonetanktobesuppliedtobothengines.(A)

AcrossfeedBcrossbleedCcrossbiltDcrossover

307.TheAPUexhaustconductstheenginegasoverboardandreducesthenoiselevelof

thehighvelocitygasflow.Theexhaustductconsistsofaheatshieldanda_.(C)

AbaffleBbufferCmufflerDattenuator

308.Thepurposeoftheignitionsystemistoproduceahighcurrentelectricalspark

toignitethefuel/airmixtureintheenginecombustionchamberduringstartingand

toprovidecontinuousignitionduringtakeoff,landingandoperationin—

conditions.(C)

AcompatibleBincompatibleCadverseDinadvertent

309.Thewindowheatsystemimprovesthe_strengthoftheflightcompartmentwindow

andpreventsfogandice-buildup.(B)

AcollisionBimpactCisolationDlimitation

310.Theamountofelevatormovementestablishestheairplane_.(B)

ArollrateBpitchrateCrollaxisDpitchaxis

311.Withthe_ofIRS.Itbecamepossibletoflyamoredirectroutefromoriginto

destination.(A)

AadventBadvantageCadverseDadversity

312.TheAPUgeneratorproducestheACpower_bytheairplanesystemsprimarilyfor

groundoperation.(B)

ArequiresBrequiredCrequiringDrequirement

313.TheMainEngineControlinconjunctionwiththepowermanagementcontrol_power

leverangle,faninletpressureandtemperature,N1rpmandN2rpmtometerthecorbect

amountfueltocombustor.(C)

AusingBuseCusesDisused

314.Enginestartingisaccomplishedby_airfromthepneumaticsystemthroughthe

stallvalvetothestarter.(C)

AsupplyBsuppliedCsupplyingDsent

315.Engineoilpressuredisplaysdisplayengineoilpressurein_.(A)

ApsiBpsidCrmpD%offull

316.TheAPUisreadily_forinspection,maintenanceorremovalthroughalargedoot

inthefuselagedirectlybelowit.(D)

ApossibleBenableCpotableDaccessible

317.Thesection41of737-300fuselagecontainstheradarantenna,flightcompartment

forwardairstairand_.(D)

ApassengercabinBcargoCescapehatchesDelectronic

Compartmentequipmentbay

318.Thepneumaticsystem_thetemperatureandpressureofenginebleedairsource.(B)

AcontrolBcontrolsCcontrolledDcontrolling

319.—systemprovidesaconditionedairenvironmentforthepassengersandcrew,heats

thecargocompartmentandcoolstheelectronicequipment.(A)

ATheairBTheCThehydraulicDThepneumatic

Conditioningpressurization

320.Theairplanealtitudeabovesealevelisdeterminedbymeasuringthepressureof

the_.(B)

AcabinBambientatmosphereCairDairconditioning

321.Thefiredetectionsystems_airplanecomponentsforoverheat,fireorsmoke

condition.(C)

AcontrolBprovideCmonitorDoperate

322.Theflightcrewoxygensystemisahighpressuregaseoussystemfor_useonly.(D)

AattendantsBpassengersCmembersofflightcrewDflightcrew

323._systemprotectstheairplaneandaidstheflightcrewwhenoperatingunderice

andrainconditions.(A)

ATheiceBThewingCThewindowDThedrain

andrainanti-iceheatanti-icing

324.Theflightcontrols_maneuveringcontrolaboutthelateral,longitudinaland

verticalaxes.(B)

AprovidesBprovideCprovidingDisprovided

325.Theelectricpower_thecontrol,operation,andindicationofthevariousairplane

systemsonthegroundandinflight.(D)

AusesBisusedtoCisusedDisusedfor

326.HydraulicsystemAandBfull-timeoperatingsystemduringflightthat

responsibilityforallhydraulicallypoweredcomponents.(D)

AassignBassistCdistributeDshare

327.Flightcontrolsaredividedintotwomajorgroups:primaryandsecondary.The

primaryflightcontrolsconsistof—.(B)

Atheflaps,Btheailerons,CtheleadingedgeDall

slatsandelevatorsanddevices,trailingcontrol

stabilizerrudderflapssurpaces

328.TheB737engineiscapableofproducingapproximately18,500to23,500poundsof

_atsealevelstaticcondition.(D)

AliftBdragCgravityDthrust

329.Thepressurizationsystemmaintainscabinaltitudeasclosetosealevel_orat

analtitudeequaltothealtitudeofotherflightdestination.(B)

ApossibleBaspossibleCpossiblyDpossibility

330.The_preventsicebuildupthedrainsformthetoiletsandlavatorysinks.(C)

ApitotstaticBtemperatureCdrainanti-icingDwing

probeprobesystemanti-icesystem

331.Thethrustreversersystemreversesthedirectionofthefanexhaustandprovides

additionalbrakingoftheairplane.Thereversercanbedeployed_withhydraulic

pressureavailable.(C)

AinflightBduringapproachConthegroundDbeforetouchdown

332._separateandindependenthydraulicsystemsareinstalledinB737.(D)

AAmainBTwoCTwopairDThree

333.Fuelisfirstsuppliedtobothenginesfrom_andthenfromtherespectivetanks

toengines.(D)

AtankNo.1BtankNo.2CventsurgetankDcentertank

334.Theelectricpowerisobtainedfromthebattery,generatorand_.(C)

AcircuitbreakerB28VdeSTBTBUSCgroundsupportDturbine

equipmentframe

335.Theengineconsistsof4majormodules:fan,core,lowpressureturbineand_.(C)

AvbvsystemBHPcomprssorCaccessorygearboxDturbineframe

336.Theaircyclemachine_aturbinewheelandacompressorwheelmountedonacommon

shaft.(B)

AcomposesofBconsistsofCcomposedofDconsistsin

337.Ourlaboratoryis_andbrightlylighted.(D)

Aair-conditioningBair-conditionerCair-conditionDair-conditioned

338.FAArequiresthatcertainrepairs_reportedtotheadministrator.(D)

AareBisCtobeDbe

339.Ifanaircraft_inanabortedtakeoffinwhichmaximumbrakinghasbeenapplied

andhelduntiltheaircraftwasstopped,thebrakemustberemoved.(B)

AhasinvolvedBhasbeenChasbeingDbeinvolved

Involvedinvolved

340.Electricitymaybe_intotwocomponents_aspositiveandnegative.(B)

Aseperated:specifBseparated:specifCseparated:specifDseperated:

ledyingiedspecifying

341.What'scorrosion?It'sachemical_inwhichmetalistransformedintosaltand

oxides.(B)

AreactBactionCreactionDresponse

342.Priorto_test,theaircraftshouldbeproperlyconfigured.(C)

AbeginBbeginwithCbeginningDbeginto

343.Markangsontheheadsoftheboltshelptoidentifythematerial_theyaremade.(B)

AwhichBofwhichCforwhichDtowhich

344.Wecantakestepstocontrolitby_itscausesandminimizingitseffects.(C)

AobserveBobservationCforwhichDtoboserve

345.Theflightcrewoxygensystemisa_systemforflightorewuseonlyisdesignated

a_system.(A)

AhighpressureBchemically-ChighpressureDchemically-

gaseous:dilutergeneratedgaseous:continuegenerated

demandoxygen:continuouusflowoxygen:diluter

sflowdemand

346.Frequentlythefogisso_aroundSanFranciscothatyoucannotsee

theGoldenGateBridge.(A)

AtenseBdenseCtensityDdensity

347.Thepictureis—;pleasestraightenit.(C)

AhighBlevelCtiltedDadjustable

348.Prior_1944therewerenoatomicbombs.(C)

AatBbeforeCtoDback

349.Thetwinswore_swimsuit.(B)

AcolorfulBidenticalCfashionableDill-fitting

350.Thesymbolsofmathematics_wearefamiliararethesignsofaddition,subtraction,

multiplication,divisionandequality.(D)

AtowhichBwiththatCinwhichDwithwhich

351.Yourcaris_mine.(C)

AthesamelikeBasCsimilartoDalike

352.Inorderto_thedamageandtoalleviatesomeofthesufferingresultingfrom

earthquakes,scientistsareworkingonwaystoenableaccurateprediction.(D)

ArelieveBdeductCweakenDminimize

353.Cabinaltitudestartsatthetakeoffaltitude.Astheairplaneclimbs,theambient

pressuredecreases:_thealtitude,—thepressure.(B)

Ahelower:Bthehigher:Cthelowest:Dthehighest

Thehigherthelowerthehighestthelowest

354.Thecabinpressure_psidandindicatesthedifferentialpressure,inpoundsper

squareinch,betweeninsideandoutsideoftheairplane.(D)

ArefertoBisreferredasCreferredtoDisreferredtoas

355.Generallyspeaking,theairplanestartsitsflightatanairportaltitudenearsea

level,ascends,cruises,and_toalandingairportnearlevel.(D)

AtakeoffsBlandsCdescentsDdescends

356.Theaftoutflowvalvemodulatesallowingcabinairtoexhaustoverboard_cabin

pressure.(B)

AtomeasureBtomaintainCmeasuringDmaintaining

357.Airis_fromthepneumaticmanifoldand_by2separateandindependentcooling

packs.(C)

Ableeding:Bbleeded:Cbled:Dbleeding:

Conditioningconitionedconditionedconditioned

358.Anaircyclemachineisan_unitofeachcoolingpack.(C)

AintegratingBintegratedCintegralDintegration

359.TheEngineandAPUFireDetectionAccessoryUnitM279locatedintheE/Ebay_

ifafireoroverheatconditionexists.(B)

AdetermineBdeterminesCdeterminedDdetermining

360.ThedistributionsystemallowsfueltobesuppliedtotheenginesandAPU.In

additionthesystemcanbeusedfordefuelingthetanksandforfuel_betweenthe

tanks.(B)

AtransductionBtransferCtranslationDtransmission

361.SystemAandSystemBarefull-timeoperatingsystemsduringflightthat_

responsibilityforallhydraulicallypoweredcomponents.(A)

AshareBsharesCsharedDsharing

362.Inthehydraulicsystem,thestandbypumpisoperatedwhenrequiredtopowerthe

rudder,thrustreversers,or_theleadingedgedevices.(C)

AextendedBisextendedCtoextendDextending

363.NormalsystemA_iswithbothpumpsoperatingtooutputfluidpressurizedto3000

psithroughthepressuremoduletotheusingsystems.(B)

AcombinationBconfigurationCcontaminationDcomputation

364.Threeredmanualextensionhandlesarelocatedontheflooroftheflightcompartment

justafterofthefirstofficer'sstation,formanualextensionofthelandinggear

_hydraulicmalfunctioninhydraulicsystemA.(B)

AinabsenceofBincaseofCrelativetoDsimilarto

365.Themainlandinggearprovidestheaftsupportforthefuselage.Itusesanair-oil

typestruttoabsorbimpact_landing,andshocksandvibrationwhiletaxiing.(B)

AofBonCinDat

366.Thelandinggearishydraulicallyactuatedtoextendand_bymeansoflanding

gearselectorlever,(C)

AextractBdeployCretractDcontrol

367.TheCFM56-3engineisanaxialflowturbofanwithtworotorsand_statorvanes.(A)

AvariableBremovableCcapableDportable

368.Themainfunctionofthefanistoacceleratetheairdirectedtotheenginesecondary

airflownozzle.Thisresults_producingapproximately78%ofthetotalengine

thrust.(C)

AfromBto

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