航空专业英语.docx

1、航空专业英语飞机Airplane半硬壳式Semi-monocoque机身Fuselage起落架Landing gear动力装置Power plant支柱Strut分为Divide into包括Contain天线Antenna玻璃纤维Fiberglass蜂窝状物Honeycomb整流罩Fairing铰链Hinge压力密封隔板Bulkhead驾驶舱flight compartment进口Entry机上厨房Galley登机梯Airstair电子设备舱Electronic equipment bay检修口Access door旅客舱Passenger cabin货舱Cargo逃逸Escape舱口Hat

2、ch空间Space燃油箱Fule bank终止Terminate辅助动力装置Auxiliary power unit程度安定面Horizontal stabilizer桁架Truss排出Exhaust设计Design和一样The same as伸长stretch延伸Extension脊鳍Dorsal fin增强Strengthen相对于Relaviate to 滑轨Skid构造structure修改reviseLESSON 2 THE PNEUMATICS SYSYTEM 增压系统一、生词目的Purpose压缩空气compressure Air 压缩空气pneumatic环境Environme

3、nt阶段，相位Phase得到Obtain发动机引气Engine bleed外部的External车Cart接头Connector整流罩Cowl热的Thermal防冰Anti-icing也，此外Also提供provide饮用水Potable water液压的Hydraulic启动器Starter在之内Within正常的Normal取代Substitute满足Meet需要，要求Need上部、顶部Top图形Figure绝缘Isolation活门Valve管道Duct结合、连接Join穿插、跨接crossover管理、调整govern适当的appropriateLESSON 3 AIR CONDINT

4、ION空调系统一、单词空气调节Air conditioning 环境Ambient机组Crew加热heat冷却Cool增压pressurization引出，放出Bled总管道Manifold别离Seprate独立的indenpendent冷却组件Cooling pack调节，管理regulate暖，热Worm减少Reduce期望Desire涡轮冷却器Air cycle machine整的Integral包括Consist of 共同的Common轴Shaft分开Leave膨胀VExpand膨胀NExpansion下降Drop零下Sub-zero分配Distribute此外In addition

5、配平空气管道Trim air line混合Mix室、容器Chamber加上，增加Add头顶上Overhead竖管Raise搜集器Collector防护罩Shroud过滤器Filter排出口discharge再分配Redistribute二等分halve二、TEXT(1)the air conditioning system provides a conditioned air environment for the passengers and crew , heats the cargo compartment, cools the electronic equipment, and sup

6、plies air for the pressurization system.空调系统为旅客和机组提供环境温度的控制，为客舱供热，为电子设备舱降温，还有为增压系统提供空气。(2)Air is bled from the pneumatic manifold and conditioned by 2 separate and independent cooling packs. Air flow into the packs is regulated by the pack valves. 空气从增压主管道和空调中通过2个隔离的，互相独立的冷却组件中被引入。空气流进组件中通过组件活门调节。(3

7、)Air from the pneumatic manifold is too warm and must be cooled. The pupose of 2 packs is to reduce engine bleed air temperature to the desired temperature.从增压主管道中来的空气太热，需要降温。两个组件的作用就是将发动机引气温度降低到需要的温度。(4)An air cycle machine is an integral unit of each cooling pack. The air cycle machine consists of

8、 a turbine wheel and a compressor wheel mounted on a common shaft. Air flowing through the air cycle machine drives the turbine, the turbine drives the compressor section. As the air leaves the turbine it expands greatly. This expansion can cause the temperature of the air to drop to sub-zero levels

9、.涡轮冷却器是构成每个冷却组件所必需的。它包括一个涡轮和一个压气机，安装在共同的轴上。气流通过涡轮冷却器驱动涡轮，涡轮驱动压气机局部。当空气分开涡轮后急剧膨胀。这种膨胀可以导致空气温度降到零度以下的程度。(5)In figure 3-1, we can see that the conditioned air from the right pack flows into the main distribution manifold, the conditioned air from the left pack flows into the main distribution manifold

10、and into the flight compartment. In addition, a trim air line from the left mix chamber adds hot air to the flight compartment duct. The main distribution manifold supplies the passenger compartment overhead distribution system through tow sidewall risers. 在图3-1中，我们可以看出，调节空气从右组件流向主分配管道，还有调节空气从左组件流向主

11、分配管道和进入驾驶舱。另外，从左混合舱出来的配平空气管道增加热空气给驾驶舱管道。主分配管道通过两个侧壁竖管供气给客舱顶局部配系统。(6)A 3-phase fan draws air from the collector shroud through filters and discharges into the main distribution manifold for redistribution.一个三相风扇从搜集器防护罩穿过过；滤器和排出口进入主分配管道，用以再分配。LESSON 4 PRESSURIZATION INTRODUCTION增压系统简介一、单词组件Pack控制Contr

12、ol座舱高度Cabin altitude外流阀Outflow valve保持Maintain尽可能的As as possible目的地destination平安的Safe舒适的Comfortable曲线Curve对时间的Against time起飞Takeoff巡航Curise虚线Dotted line实线Solid line爬升Ascend下降Descent近Near环境ambient减小decrease变化率rate确定、决定Determine大气Atmosphere例子Example磅/英寸Psi=pound per square inch参照By referring图表Chart描绘D

13、epict与的关系曲线versus称之为Is referred to as 制度Sytstem水银mercury毫巴Millibar相等的identical施加exert排出exhaust向机舱外outbroudLESSON 5 FIRE DETECTION火警探测一、单词火警探测Fire detection在周围Around组件Pack监控Monitor存在Exist泄漏Leak部件Component警告Alarm报警器horn过热Overheat铃声Bell规定specify发生Occur听觉Aural在之下beneath面板Panel器件device与相对应Respond to 机翼Wi

14、ng灭火器Extinguish盆basin厕所Lavatory瓶Bottle擦手纸斜槽Tower chute可选的optional角落Corner特征feature轮子wheel可用的Available放出discharge位置Location完成Accomplish元件element天花板Ceiling二、TEXT(1)the fire detection systems monitor airplane components for overheat, fire or smoke condition. Engine and APU fire and overheat indication

15、occurs on the P8 and P7 panels. Wing and body duct overheat warning occurs on the P5 and P7 panels. Lavatory smoke detection indication is an optional feature that is available. Indication can occur at the lavatory location and or on the P5 panel.火警探测系统监控飞机组件的过热、失火或烟雾等情况。发动机和APU过热和失火指示出如今P8或P7板上。机翼和

16、机身管道过热警告出如今P5或P7板上。厕所烟雾探测指示是一个可选装配件。指示可以出如今厕所位置或P5板上。(2)Engine fire and overheat detection is provided by detector elements located around the engine. The engine and APU fire detection accessory unit M279, located in the E/E bay determines if a fire or overheat condition exists. When detected indica

17、tions occur in the flight deck an alarm bell is provided by the aural warning devices unit M315 for a fire condition. The two engine fire extinguisher bottles are located on the upper left aft corner of the main wheel well and are discharged from the flight deck.发动机失火和过热信号探测由安装在发动机周围的探测元件提供。发动机和APU火

18、警探测组件M279，安装在电子设备舱，用于判断是否有失火或过热情况发生。当在飞机蒙皮探测到火警信号时，音响警告设备M315将给出一个警告铃声。两台发动机灭火瓶安装在主轮舱左下方后角处，并从处释放。(3)The APU detectors sense fire conditions only. Monitoring of the sensors is accomplished by the M279. indications occur on the P28 panel in the wheel well and also in the flight deck. The APU fire bot

19、tle is located behind the aft pressure bulkhead and is discharged either from the flight deck or P28 panel.APU探测器只感应火警信号。传感器的监控由M279完成。指示出如今P28板在主轮舱和FLIGHT DECK。 APU灭火瓶后压力隔板上，并通过P28板或FLIGH DECK释放。(4)Wheel well fire detection is provided by detector elements mounted on the wheel well ceiling. The det

20、ectors provide input to the M237 module located in the E/E bay. Indications occur on the P7 and P8 panels and an alarm bell is provided by the M315 module.轮舱火警探测由安装在轮舱天花板上的探测元件来提供。探测器提供信号给安装在电子设备舱的M237组件。指示信号出如今P7和P8板上，警告铃声由M315组件提供。(5)The wing and body overheat detection system exists to monitor th

21、e pneumatic system for leaks . the detection system is divided into a left and right system. The detectors provide input to the M237 module. Overheat indication occurs on the P5 and P7 panels.机翼和机身过热探测系统监控增压系统有无渗漏。探测系统分为左右两局部。探测器提供信号给M237组件。过热指示信号出如今P5和P7板上。(6)The lavatory smoke detector is located

22、in each lavatory, the detector will provide a warning horn and indication at a specified smoke level .located in each lavatory, beneath the wash basin, is a fire extinguisher bottle which responds to high temperature in the tower chute.厕所烟雾探测器安装在每个厕所里，探测器将在规定的烟雾层度发出警告信号。灭火瓶安装在每个厕所，洗手池下面，可以对擦手纸斜槽里的高温

23、情况作出响应。LESSON 6 OXYGEN SYSTEM氧气系统一、单词氧气Oxygen要求、命令Acquire单独的independent安装Install气态的Gaseous称为designate稀释器Diluter要求Demand化学上Chemically效劳员Attandent气缸Cylinder旅客效劳设备Passengers service unit面罩Mask切断Shut off数量Quantity压强计Gage即使In a event of排出Vent紧急情况Emergence锁定Latch释放Release作动筒Actuator机构Mechanism开动，启动activat

24、e自动地automatically人工地manuallyLESSON 7 ICE AND RAIN PROTECTION防冰、防雨一、单词雨Rain保护Protect帮助Aid为而提供Is provided for雨刷Wiper防雨剂Repellent叶片Vane卫生间Toilet排放Drain视线Vision皮托静压Pitot static探头Probe迎角叶片Alpha vane支柱管Mast堆积Buildup碰撞Impact强度Strengthen雾Fog导电的conductive涂层coating暴露expose气流Airstream形成Formatting结冰Freeze原因Caus

25、e出故障的Faulty损失Loss槽Sink嵌入Embed垫圈gasket装置fitting与结合在一起Are integrated withLESSON 8 THE POTABLE WATER SYSTEM 饮用水系统一、单词饮用水Potable water浪废Waste由组成Be composed of油箱tank数量Quantity制作Construct支架bracketU.S. gallonImperial gallon园筒形的Cylindrical覆盖层blanket充注管道Fill line外泄管道Overflow line水量传感器Quantity transmitter容积Ca

26、pacity簧片Reed二极管Diode浮子Float磁铁Magnet包围Surround标明Label关联的associate相应的corresponding空emptinessLESSON 9 FLIGHT DECK LIGHTING 飞行面板照明一、单词照明Lighting照明Illumination舒适Comfort最正确的Optimum效能Performance操作Handing主要的Major可变的Available强度Strength总体的Integral机长Captain副驾驶First office遮光板Glareshield发荧光的Fluorescent泛光灯Floodli

27、ght标记Identify顺时针方向的Clockwise增长Increase亮度Brightness白灼灯Incandescent自动驾驶仪AutopilotAFDSAutopilot flight director system暗淡Dim试验Test空间Space控制台Control stand与类似Similar to推力手柄盘Thrust lever quadrant电路跳开关Circuit breakerLESSON 10 737 ELECTRONIC EQUIPMENT BAY 737电子设备舱一、单词可以到达的accessible到达reach修改modification排故Tro

28、ubleshooting简化Simplify可挪动的Removable装配Assembly支架Rack搁板Shelf大气数据Air data计算机Computer自动油门Auto throttle数字式Digital失速Stall警告Warning 温度Temperature控制器Controller设置Location飞行管理计算机Flight management computer惯性基准系统Inertial reference system模拟量Analog适配器Adapter发动机Engine振动Vibration信号Signal选择呼叫系统Selective calling system偏航阻尼器Yaw damper综合飞行系统附件组件Integrated flight syst