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飞行器维修技术专业英语

202leading edge

203逃生滑梯

204自动飞行

210主起落架

215Aelectronic equipment

216Aassessment of performance unit

217Aexecution element

218Aforward airstair

219direct current (DC)

221escape slide

222emergency exit

223control valve

226solenoid valve

228alternating current (AC)

229The fuselage is divided into four sections: （）, （）, （） and section 48

230auxiliary power unit (APU) 译为：地面电源组件。

231air-conditioning bays, wheel well, hydraulic bay and aft cargo compartment 译为：空调舱，轮舱，液压舱和后货舱。

232center and aft portion of the passenger cabin 译为：货舱中后部。

233the passenger cabin and the forward cargo compartment译为：客舱和后货舱

234pressure bulkhead译为：压力头盔。

235radar antenna behind a fiberglass honeycomb fairing译为：玻璃纤维整流罩后的雷达天线

236The fuselage is divided into four sections: section 41, section 43, section 46 and section 50

237On cargo planes, the cabin is replaced by a cargo compartment

238APU is （）

241传输活门

244前起落架

245放出,伸出

249The landing gear provides support for the airplane static and ground maneuvering conditions

250The landing gear consists of two main gears (MLG) and a nose gear (NLG)

251Located inboard of each engine, aft of the rear wing spar，the main gear provides the support for the aft section of the fuselage

252Landing impact is absorbed by five air-oil shock struts, functioning primarily as air springs

253The body and wing gear doors each have wheel well doors and shock strut doors

254The nose wheel steering system supplies the ground directional control by hydraulically actuated cylinders

255The airplane can be towed forward or aft from the nose gear

256Each main gear wheel (wing and body) is provided with a brake unit installed on the axle on the side nearest the shock strut

257Install the ground locks in all landing gear very carefully for an accidental retraction can cause injury to persons and damage to equipment

258The 737 airplane has a tricycle type landing gear with air/oil shock struts

263downlock pin

264solenoid lock

265bypass valve

269A液压制动压力指示器

270A停留刹车

271A主起落架轮舱

272A减震支柱

277torsion link

280external power

283The landing gear consists of （）and （）

284The landing gear is also called undercarriage译为：起落架又称作着陆装置

285The shock-absorbing struts can cushion the blow of landing译为：减震支柱能够缓冲着陆时的冲击。

286The wheels of most airplanes are attached to shock-absorbing struts

287The main gears are attached to the wing rear spar and retract to stow under the main cabin aft of the wing rear spar

288The landing gear is not retracted and extended hydraulically

289The nose gear is used for maneuvers on the ground

290The nose gear is retracted forward into a wheel well in the lower nose compartment

291It consists of the nose gear and the after gears

292The landing gear supports the airplane when it is resting on the ground or in water and during the takeoff and landing

293The hazard around the engine in operation include inlet suction, exhaust heat, exhaust velocity, and noise

294In the combustor, the high pressure air from the HPC is mixed with the fuel from the fuel nozzles

295The fan, located on the front of the engine, is the first component of a turbofan engine

296The engine is made up of four main sections: compressor section, combustion section, turbine Section, and accessory drives

297The turbine exhaust system is aft of the thrust reverser

298The engine cowling is a cover that contains and gives protection to the engine components

299The CFM56-7B is a high bypass ratio, a two-spool, axial flow turbofan engine

300It also provides bleed air for air conditioning, pressurization, anti-icing, and drives a gearbox used for electrical power and hydraulic power