• 热门标签

当前位置: 主页 > 航空资料 > 航空英语 >

时间:2010-09-02 16:13来源:蓝天飞行翻译 作者:admin
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

48 部分包括辅助动力装置和水平安定面桁架。可以通过左侧口盖接
近。在它们的后面是APU 检修口和APU 排气口。
(7) The 737-300 is the same basic design as the 737-200, with a body stretch
of 104 inches, a wing tip extension of 14 inches, a horizontal tail extention
of 36 inches, a larger dorsal fin and strengthened stabilizer.
737-300 与737-200 具有相同的基本设计,机体伸长了104 英寸,翼
尖延伸了14 英寸,水平尾翼延伸了36 英寸,还多了个大的脊鳍和增
强的水平尾翼。
(8) The 737-400, relative to the 737-300, has body stretch of 120 inches, tow
additional overwing exit, tail skid, and strengthened landing gear.
737-400 与737-300 相比较,机身伸长了120 英寸,多了两个逃生出
口,尾部滑轨及加强了起落架。
(9) The 737-500 uses the 737-300 basic structure with a 94 inches shorter
body and a revised forward and aft fairing (wing to body).
737-500 使用了737-300 的基本结构,机身短了94 英寸,并且修改了
前后整流罩(机翼到机体)。
LESSON 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appropriate
二、TEXT
(1) the purpose of the pneumatic sysytem is to supply compressed air for a
controlled temperature and pressure environment during all phases of
flight and ground operation .air is obtained from engine bleeds. APU、or
from an extermal ground cart through a connector located on the fuselage.
增压系统的作用是为飞行及地面所有阶段的温度和压力控制提供压
缩空气。压缩空气的来源可以是发动机引气、APU、或通过机身上的
连接头与地面气源车相连供气。
(2) The pneumatic system controls the temperature and the pressure of engine
bleed air source. The pneumatic system provides high temperature, high
pressure air for the air conditioning .pressurization, wing and cowl
thermal anti-icing .also, the pneumatic system provides pressure for the
potable water system, hydraulic system and engine starters. The engine
bleed air systems are located on the engine and within the support strut.
增压引气控制发动机引气的温度和压力。增压系统为空调、增压系统、
机翼及整流罩热防冰系统提供高温、高压引气。同时,增压系统还给
饮用水系统、液压系统和发动机起动系统提供压力。发动机引气系统
位于支架内部发动机上。
(3) The normal cabin air source is obtained from the 5th-stage of the engines
at low –engine power, 9th-stage air automatically substitutes to meet user
system needs.
正常情况下,客舱空气来自于发动机低能量的第5 级,9 级空气自动
分配以满足用户系统的需要。
(4) On the top of figure 2-1, the isolation valve separates the left and right
halves of the system. On the left side of the isolation valve, the APU bleed
air duct joins the left side crossover duct; on the right side ,the pneumatic
ground service connector joins the right side crossover duct. From these
ducts the user system are supplied with pressurized air ,governed by the
appropriate control valves.
在图2-1 的上方,隔离活门将左右系统分隔成独立的两部分。在隔离
活门的左边,APU 引气管道立连接着左交输管道;在右边,压缩空
气地面接头连接右交输管道。用户系统可以从这些管道获得压缩空
气,通过适当的控制活门进行控制。
LESSON 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V Expand 膨胀N Expansion 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
 
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)(80)