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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Hatch空间Space燃油箱Fule bank终止Terminate辅助动力装置Auxiliary power unit水平安定面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结构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Environment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交叉、跨接crossover管理、调整govern适当的appropriateLESSON 3 AIR CONDINTION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分离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离开Leave膨胀VExpand膨胀NExpansion下降Drop零下Sub-zero分配Distribute此外In addition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收集器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 supplies 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,相互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) 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 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.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,涡轮驱动压气机部分。当空气离开涡轮后急剧膨胀。这种膨胀能够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 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部分配系统。(6) A 3-phase fan draws air from the collector shroud through filters and discharges into the main distribution manifold for redistribution.一个三相风扇从收集器防护罩穿过过;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Control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安全的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Depict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Wing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 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过热和失火指示出现在P8或P7板上。机翼和机身管道过热警告出现在P5或P7板上。厕所烟雾探测指示是一个可选装配件。指示能够出现在厕所位置或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 indications 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 bottle 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。指示出现在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 detectors 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。指示信号出现在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 the 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部分。探测器提供信号给M237组件。过热指示信号出现在P5和P7板上。(6) The lavatory smoke detector is located 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服务员Attandent气缸Cylinder旅客服务设备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activate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Cause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bracket3.785公升U.S. gallon4.546公升Imperial 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Capacity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最佳的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Floodlight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 BAY737电子设备舱一、单词可以达到的accessible到达reach修改modification排故Troubleshooting简化Simplify可移动的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 system accessory unit旅客广播Passenger address放大器Amplifier遥控电子装置Remote equipment unit甚高频Very hight frequency通信Communication空中交通管制Air traffic control数字飞行数据采集装置Digital flight data acquisition测距机Distance measuring equipment 静变流机Static inverter电瓶充电器Battery charge变压器transformer整流器Rectifier减速板Speed break襟翼Flap缝翼Slat电门Switch过热Overheat失火Fire探测器detector导航navigation继电器relay LESSON 11 ELECTRICAL POWER 电源系统一、单词:电源Electrical power不同的Various电瓶battery发电机Generator地面保障设备Ground support equipment交流Alternating current驱动Drive插座Receptacle转换Convertion分布Distribute产生Produce主要是Primarily额定容量Is rated at 千伏安Kilovolt ampere汇流条Slip-ring换向器Commutator电刷Brush励磁器Exciter完整的Complete整流器Rectifier磁极Pole磁场Field转 子Armature装有Is supplied with调节器Regulator引出Develop送入Fed into定子Stator恒速传动装置Constant speed drive附件齿轮箱Accessory gearbox关键的critical缺少absence变压器transformer备份的backupLESSON 12 FUEL 燃油一、单词燃油Fuel存贮Store运送Deliver细分Subdivide贮藏Storage加燃油Fueling油箱Tank通气装置Vent通气均压油箱Vent surge tank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HeightLESSON 13 HYDRAULIC POWER一、 单词液压的Hydraulic动力,电源Powr反推装置Reverser共享Share责任、负责液压传动的Dydrallically有要求的On demond起落架Landing gear前轮转弯Nose wheel steering副翼aileron动力控制组件Power control unit升降舵Elevator方向舵Rudder飞行扰流板Flight spoiler刹车Brake动力转换装置Driven transfer unit发动机传动泵Engine driven pump电动马达传动泵Electric motor driven pump关闭Shutoff截流阀Shutoff valve油箱Reservoir压力过滤器Pressure filter消除Relief润滑Lubricate热交换器Exchanger返回Return后缘Trailing edge前缘Leading edge交替的Alternate单独地individually龙骨Keel beam带保护罩的开关Guarded switch节LESSON 14 LANDING GEAR起落架一、单词主起落架Main gear前起落架Nose gear梁Spar防滑的Antiskid无效的Inoperative自动刹车Autobrake解除预位Disarm使动作Actuate借助于By means of 减压Depressurize电磁线圈Solenoid限制Restrict相应的Respective移动,变换Transit一致Agree充当Serve as形态Configuration在情况下In case of 故障Malfunction减震支柱Shock strut缓冲Absorb碰撞Inpact冲撞Shock振动Vibration滑行Taxi整流罩Fairing机构Mechanism保证Assure阻力杆Drag brace扭力臂Torsion link圆筒Cylinder轴颈销钉Trunnion pin稳定性Stability牵引tow环Lug横向螺栓crossbolt牵引杆tow bar碰撞Bump注入Charge氮气Nitrogen折迭Fold环collar转弯力矩Turning moment手轮Handwheel脚蹬pedalLESSON 15 FLIGHT CONTROLS一、单词飞行Flight 操纵Control 机动动作maneuver水平的Lateral纵向的longitudinal垂直的Vertical轴Axes增加Increase升力Lift起飞Takeoff着陆Landing阻力Drag地面Ground被分成Are divided into集团Group主要的Primary次要的Secondary方法、手段Means驾驶盘Control wheel配平Trim位置Position导致Cause转 动Rotate姿.态Attitude角度Angular量; 值Amount操纵面Control surface建立Establish大小、尺寸Magnitude达到Reach再成流线型Refair全部的Total对起作用Act on 平衡Balance保持remain稳定的Stable坡度bank角度Angle降低Lose命令Command驾驶舱Flight deck操纵台Control stand传感器Sensor反馈Feedback信号Signal自动驾驶仪Autopilot转动鼓轮bus Drum驾驶盘操纵Control wheel steering换能器transducer副翼操纵力限制Aileron force limiter考虑Consider升力中心Center lift重心Center gravity反向力Counter force横滚Roll俯仰(率)Pitch rate驾驶杆Control column扭力管Torque tube调整片Tab扇形盘quadrant操纵杆Control rod 曲柄Crank供给、容许admitLESSON 16 POWER PLANT (1)一、单词动力装置Power plant推力thrust帮助aid反推装置Thrust reverser驱动drive齿轮箱gearbox高函道比High bypass rate涡轮风扇turbofan装配fitting相同的轴流axes转子rotor定子叶片State vane压缩机compressure经由Via轴shaft涡轮turbine机械地mechanically独立的independent相互Each other气流Airstream燃烧combusion环形的提高increase排气Discharger air能够Is capable of大约approximately主要的major组件module核心core附件齿轮箱Accessory gearbox维护maintenance助推器booster轴承支座Bearing support入口inlet支架frame喷嘴nozzle防护罩shroud转换transfer继续continue加速accelerate引导direct结果result交付deliver用泵抽pump截流阀Shutoff valve起动手柄Start lever警告waring头顶上方的overhead照亮illuminate暗淡的dim热交换器Heat exchange过滤器filter失败failure堵塞blockage主发动机控制器Main engine control离开leave转入Is ported to 机械mechanism和一起In conjunction with转/分Revolution per minute测量meter发射机transmitter测量measure指示器indicator回油scavenge旁通活门Bypass valveLESSON 17 PPOWER PLANT (2)一、单词起动Start点火Ignition扭矩Torque转动Rotate加速Accelerate慢车Idle起动器Starter一套电路Circuitry高压压气机High pressure compressor外壳Case位置Position完成Accomplish级Stage空气涡流发动机Turbine-air motor把转换Convert into能量Energy足够的Sufficient地面源Ground source交叉引气Crossbleed另一个Another与有关Related to 火花Spark混合物Mixture起飞Take off着落Landing有害的Adverse天气Weather情况Condition要求Require点火Ignite励磁器Exciter三维的triaxial屏蔽Shield引线lead入口整流罩Inlet cowl预冷器Percooler限制Limit温度Temperature总管道manifold相反revers方向Director套筒sleeve遥控器Remote展开Deploy在之前Prior to 展开Deployment阻流门Blocker door排列Arrange连接在上Is attached to 螺栓Bolt阻力连杆Drag link装置Fitting移动Translate强迫Forcing级联的Cascade部分、段Segment形成Form参数Parameter仪表Instrument发光二极管Light emitting diode百分比Percent排气温度Exhaust gas temperature超出Exceed红线Redline重量Weight总的Total消耗Consume顺序Sequence 复位Reset振动Vibration最大的maximumLESSON 18 AUSILLARY POWER UNIT (1) 一、单词电的Electrical完全地Completely封入Enclose钛Titanium入口Inlet入口Entrance分开Split通路Path孔、洞Hole喷射管Jet pipe组件Pack容易地Readily容易接近地Accessible检查Inspection拆卸removal简单的Simple吊车Hoist电缆Cable离心的Centrifugal径向的radial流入、内流Inflow电磁线圈Solenoid放置Place超控Override调节Regulate最初的initial污染contamination施加apply测量Meter接近Near恒定的Constant速度Speed安全的Safe插头Plug电路Circuit点火激励器Ignition exciter密封的hermetically密封Seal金属Metal安装Install连接interface程序化的Sequencing通电Energize保证Ensure起燃Initiate最低Minimum润滑lubricate形成Build up表压Psig释放De-energize保持状态Remain引导Conduct噪音Noise消音器Muffler因而Thus园柱体Cylindrical绝缘纸Felt衬垫Liner集油盘Drip pan间隔GapLESSON 19 AUXILIARY POWER UNIT (2)一、单词首先Primarily供给Furnish接线端teminal中线Neutral导线Lead在外面Outside放电器Discharger开缝的slotted频率Frequency得到Achieve跳开关Breaker闭合Closing松开Tripping永久磁铁Permanent magnet帮助Assist锁定Latch弹簧Spring保持hold触点Contact接触器Contactor信号Signal获得Gain应用Application允许Allow短暂的Momentary通电Energize线圈Coil极性po
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