曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
3) Pitot static and temperature probes.
4) Alpha vanes.
5) Toilet drains.
防冰、防雨系统用于保护飞机及帮助机组在雨雪天气下操作飞机。此系
统为下列部件提供保护：
1）发动机外前缘缝翼；
2）驾驶舱玻璃窗（加热、雨刷、防雨剂）；
3）皮托静压管及总温探头；
4）迎角叶片；
5）厕所排水。
(2)Wing leading slats use hot air from the pneumatic system. Flight
compartment windows are electrically heated. The wipers and rain
repellent are used for providing clear vision. The pitot static probes, alpha
vanes, drain masts, and toilet drains use electric heaters.
前缘缝翼用增压系统的热引气加温。驾驶舱窗口用电加温。雨刷和防
雨剂用来提供清晰视野。皮托静压探头、迎角叶片、排水管及厕所排
水都是用电加温。
(3) The wing anti-ice system prevents ice buildup on the wing leading edge
slats, this system consists of air supply ducts, valves, terminal switches,
controls and indications.
防冰系统可防止冰在缝翼前缘堆积，此系统包括供气管道、活门、终
端开关、控制及指示器。
(4) The window heat system improves the impact strength of the flight
compartment windows and prevents fog and ice-buildup, this system
consists of conductive coating in the window structure, heat control units,
controls and indications.
窗口加热系统提高了驾驶舱窗口的撞击强度并防止雾和冰的堆积，此
系统包括窗口结构上的导电涂层、加热控制组件、控制及指示器。
(5) The pitot static probes, temperature probe and alpha vanes provide air data
information to the various using system, they are located on the left and
right sides of the forward fuselage. Since all the probes and vanes are
exposed to the airstream, internal heating is provided to prevent ice
formation. Freezing could cause faulty inputs or possible loss of all data.
皮托静压探头、总温探头和迎角叶片用来提供大气数据信息给不同的
应用系统，他们位于前机身在右侧。因为所有的探头及叶片都暴露在
气流里，需要加热以防止结冰。结冰可以导致所有数据的丢失或输入
错误信息。
(6) The drain anti-icing system prevents ice buildup on the drains from the
toilets and lavatory sinks. The aft toilet drain heater is embedded in gasket
between the drain tube and the drain outlet fitting. The lavatory sink drain
heater are integrated with the drain mast. The power supply for the toilet
drain heaters is 115 volts ac and for the lavatory sink drain is 115 volts ac
or 28 volts ac.
排水防冰系统防止在卫生间及其水池的排水装置上积冰。后厕所加热
器用垫片嵌入在排水管道与外流排水装置之间。厕所洗手池加热器与
排水竖管连在一起。为厕所排水管加热用的是115V 直流电，为厕所
洗手池加热用的是115V 直流或28V 直流电。
LESSON 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bracket 3.785 公升U.S. gallon 4.546 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emptiness
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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
航空工程英语基础（中英文对照）(84)
