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航空工程英语基础 ESSENTIAL ENGLISH OF AERONAUTICAL ENGINEERING

时间:2011-06-14 21:26来源:蓝天飞行翻译 作者:航空 点击:


暂时的  Temporary 燃油密封的  Fueling tight 金属和金属  Metal to metal
装配  Fit 化合剂  Compound 密封剂  Sealing compound
紧固件  Fastener 接口  Joint 翼肋  Rib
缓冲挡板  Baffer 单向活门  Check valve 增压泵  Boost pump
离开  Away off 加油站  Fueling station 填充  Fill
部份的  Partially 完全地  Completely 另一方面  Alternately
入口  port 转移  Transfer 浮子  Float
过满  Overfill 防止 …做 …  Prevent M from doing 放油  Defueling
利用  Utilize 用泵抽  Boost pump 供油  Feed 

各自的 交输  Crossfeed 可使用的  Usable
重量  Weight 容量  Capacitance 杆  Stick
芯片  Chip 微电子计算机  Microcomputer 液晶显示  Liquid crystal display
电阻电流  Resistive current 泄漏  Leakage 不能接受的  Unacceptable
错误  Error 代码  Code 刻度  Graduate
带  tape 高度  Height

(1) the purpose of the fuel system is to store and deliver fuel to the engine and APU. The fuel system is subdivided into dotrage, fueling, distribution and indicating systems.

燃油系统用于贮存并传输燃油给发动机和 APU。燃油系统细分为贮藏、供油、分配及指示系统。

(2) There are 3 tanks for fuel storage and 2 vent surge tanks for temporary fuel storage. Tank No.1 is located in the left wing, tank No.2 is located in the right wing and center tank is located in the fuselage under the passenger cabin. The 2 vent surge tanks are located outboard of the main tanks. All fuel tanks are fuel tight. Close metal-to –metal fit of all parts forms the basic seal. Sealing compounds and sealed fasteners are used on all joints to complete the fluid tight seal. Two of the wing ribs contain a series of baffle check valves to prevent fuel flow away from the boost pumps.

燃油系统有 3个贮油箱和 2个用于临时贮油的油箱。 1号油箱位于左机翼, 2号油箱位于右机翼,中央油箱位于机身客舱下方。 2个通气均压油箱位于两个主油箱的外侧。 Close metal-to –metal fit of all parts forms the basic seal.所有的油箱都是密封的。所有的接头处都用密封剂和密封紧固件进行密封。两个翼肋处包括又个连续的缓冲隔板单向活门,防止燃油从增压泵中流出。

(3) The fueling system provides a means of filling the fuel tanks on the airplane. Fueling can be accomplished by the use of a single pressure


fueling station through which all tanks can be filled partially or completely. Alternately, the main tanks(No.1 and No.2) can be filled through the overwing ports. The center tank can be filled by transferring fuel from the main tanks using the fuel station.
燃油系统提供一种在飞机上给油箱注油的方式。供油可以通过一个单压力加油口来完成,通过它,可以为所有的油箱全部或部份的加油。另一方面,主油箱( 1、2号)可以通过机翼上方口注油。中央油箱可以用加油站从主油箱中传输来过。
(4) The components associated with the fueling system are the fueling station located under the right wing leading edge outboard of the engine, 3 float switches – one for each tank, prevent the tanks from being overfilled. The tank fueling float switches are located near the top of e ach tank and sense full tank quantity. The tanks can be filled to any desired quantity, the float switches sense full tank condition and automatically stop the fueling. Power requirements are supplied by ground power, APU or the battery. Pressure fueling can also be done manually. Maximum fuel pressure is 55 psi.

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