航空工程英语基础(4)

LESSON 8 THE POTABLE WATER SYSTEM 饮用水系统 一、单词 饮用水 油箱 支架 园筒形的 外泄管道 簧片 磁铁 关联的 Potable water tank bracket Cylindrical Overflow line Reed Magnet associate 浪废 数量 3.785公升 覆盖层 水量传感器 二极管 包围 相应的 Waste Quantity U.S. gallon blanket Quantity transmitter Diode Surround corresponding 浮子 标明 空 Float Label emptiness 由?组成 制作 4.546公升 充注管道 容积 Be composed of Construct Imperial gallon Fill line Capacity 二、TEXT

(1) the potable water system supplies potable water to the galleys and lavatories. The waste system is for storing and removing waste from the toilets. The water and waste system is composed of independent but related systems.

饮用水系统为机上厨房及卫生间提供饮用水。水系统是用于贮水及排放卫生间废水饮用水及废水系统是由相互独立并相互关联的系统。 (2) The potable water system consists of a water tank, quantity indication, pressurization components, and distribution tubing. The water tank and pressurization components are located aft of the aft cargo compartment. The quantity indication is in the aft section of the passenger cabin. 饮用水系统由一个水箱、流量指示器、增压组件及分配管道组成。水箱及增压组件位于后货舱的后面，流里指示器位于客舱后部。 (3) The water tank stores potable water for use by the passengers and crew.the tank is constructed of fiberglass and attached by struts and mounting brackets to the airplane structure. The 30 U.S. gallon tank is cylindrical. It is protected from freezing by a 3-pieces fiberglass blanket. On the upper section of the tank are connections for the air pressure line, fill line, overflow line, supply line, and a quantity transmitter, the fill and overflow valve is used to fill the tank to the capacity determined by a standpipe, this

valve is operated a handle. A drain valve is located on the bottom of the tank.

水箱用以贮存供旅客及机组使用 的饮用水。水箱由玻璃纤维制成，并固定在飞机桁架上。30加仑的圆柱形水箱。用三个玻璃纤维垫片防止结冰。水箱上部连结着一个空气连接管道，充注管道，过流管道，供水管道及一个流量传感器，注水及过流阀 此阀门被一个手柄控制。一个排放活门被安装在水箱底部。

(4) The quantity indication shows the amount of water in the tank. The quantity transmitter consists of 10 reed switches and 3 inside a tube. A float with 3 magnets surrounds the tube. In addition, the indicator consists of 5 lights the tank determines the position of the float. The magnets on the float close the associated reed switches. Using the push button on the quantity indicator, allows the corresponding quantity lights to illuminate if the tank is emptiness, the E light is illuminated, if the tank is full, all lights are illuminated.

流量指示器显示水箱水量。流量传感器包括10个簧片、3个管道。1个浮子和3个磁铁包围着管道。另外，指示器包括5个水位指示灯。浮子上的磁铁与弹簧开关相关联。按下水量指示器上的按钮，当水箱空了时，相关的指示灯E灯就会亮，若水箱是满的，所有的灯都会亮。

LESSON 9 FLIGHT DECK LIGHTING 飞行面板照明 一、单词 照明 最佳的 主要的 总体的 遮光板 标记 亮度 AFDS Lighting Optimum Major Integral Glareshield Identify Brightness Autopilot 照明 效能 可变的 机长 发荧光的 顺时针方向的 白灼灯 flight 暗淡 Illumination Performance Available Captain Fluorescent Clockwise Incandescent Dim 舒适 操作 强度 副驾驶 泛光灯 增长 自动驾驶仪 试验 Test Comfort Handing Strength First office Floodlight Increase Autopilot director system 空间 Space quadrant 控制台 lever 电路跳开关 Control stand Circuit breaker 与?类似 Similar to 推力手柄盘 Thrust 二、TEXT

(1) the purpose of the lighting system is to provide the necessary illumination for passenger comfort, optimum flight crew work performance, service and cargo handling, and provide for lighting undremergency conditions. 灯光系统的作用是为旅客舒适、极佳的机组工作效能、服务及货舱操作，及在应急条件下提供灯光。

(2) The major systems are :flight compartment lights, passenger compartment lights, exterior lights and emergency lights. In this lesson, we will introduce the flight deck lighting only.

主系统包括：驾驶舱灯光、客舱灯光、外部灯光及应急灯光。本文中，我们将只讲驾驶舱灯光。

(3) Variable intensity controls for the integral instrument and main instrument panel lights are identified as PANEL and located on the lower portion of the captain’s and first officer’s panels. The captain’s variable intensity PANEL switch controls these lights on the captain’s main panel, the center panel and the glareshied. The first officer’s PANEL switch controls these lights on the first officer’s panel.

亮度调节面板作为调节亮度的整体及主要手，段位于机长及副驾面板的下方。机长的亮度调节面板开关控制着机长面板、中央面板及遮光板上的灯光。副驾驶面板开关控制副驾驶面板上的灯光。

(4) White fluorescent floodlights are positioned under the glareshield to direct background lighting onto the main panels. One variable –intensity switch, which controls these lights, is on the lower portion of the captain’s main panel and identified as ACKGROUND, movement of this switch in a clockwise direction increases the brightness of the fluorescent lights. 白色的荧光屏泛光灯位于遮光板下方。一个亮度调节开关控制着这些

灯，它是位于机长主面板下方标识为ACKGROUND的开关，顺时针转动开关增加荧光屏亮度。

(5) White incandescent floodlights are positioned above the autopilot flight director sysem (afds)panel, one variable –intensity switch, which controls these lights, is on the lower portion of the captain’s main panel and identified as AFDS FLOOD. Clockwise movement of this switch increases brightness of the lights

白色荧光指示灯位于自动飞行指引系统面板上方，一个控制这些灯的亮度调节开关位于机长主面板的下方，并标识为AFDSFLOOD。顺时针转动开关可增加灯光亮度。

(6) The flight compartment system indicator lights may be dimmed or tested by the use of a LIGHT switch located on the center instrument panel. Placing the switch in the test position illuminates the indicator lights, and placing the switch in the dim position dims them.

驾驶舱指示器系统的灯光可通过中央面板上的“灯光”开关来调暗或测试。将开关置于测试位照亮指示器灯光，将开关置于暗位来调暗灯光。

(7) The control stand instrument panels are integrally lighted similar to those unit on the main instrument panels. In addition, there is a white flood light on the forward overhead panel which directs light downward onto the thrust lever quadrant on the control stand. Variable-intensity controls for these lights are on the control stand and identified as PANEL and FLOOD. 控制台面板整体灯光的控制与主面板灯光相似。另外，有一个白色的泛光灯在顶置面板上，它可直接为控制台上的推力手柄扇形盘提供照明，这些灯光的亮度调节钮在控制台上标识为“FLOOD”。 (8) a variable intensity control for the integral instrument panel lights and for instrument lights on the overhead panels is located on the forward overhead panels and identified as PANEL.

(9) In addition, there are two map lights mounted above each pilot’s seat, two

circuit breaker panel floodlights on the sidewall by each pilot’s seat, two white dome lights on the circuit breaker panels behind the crew provide general flight compartment area illumination.

LESSON 10 737 ELECTRONIC EQUIPMENT BAY 737电子设备舱 一、单词 可以达到的 accessible 排故 装配 大气数据 数字式 温度 飞行管理计算机 适配器 信号 综合飞行系Troubleshooting Assembly Air data Digital Temperature Flight management computer Adapter Signal 发动机 选择呼叫系统 到达 简化 支架 计算机 失速 控制器 惯性基准系统 reach Simplify Rack Computer Stall Controller Inertial reference system Engine Selective calling system Integrated flight 旅客广播 unit 遥控电子装置 空中交通管制 静变流机 整流器 缝翼 失火 继电器 Static inverter Rectifier Slat Fire relay Remote equipment unit Air traffic control 数字飞行数据采集装置 电瓶充电器 减速板 电门 探测器 甚高频 Very frequency Digital flight 测距机 Distance measuring equipment Battery charge Speed break Switch detector 变压器 襟翼 过热 导航 transformer Flap Overheat navigation data acquisition hight 通信 Communication Passenger address 统附件组件 system accessory 振动 偏航阻尼器 放大器 Amplifier Vibration Yaw damper 修改 可移动的 搁板 自动油门 警告 设置 模拟量 modification Removable Shelf Auto throttle Warning Location Analog 二、TEXT

(1) electronic equipments are located in a compartment below the cabin floor aft or the nose gear. This electronic equipment compartment is accessible

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