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图解直升机英语(以s-92为例) [复制链接]

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1#
发表于 2009-3-10 22:05:26 |只看该作者 |倒序浏览

图解直升机英语(以s-92为例)

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2#
发表于 2009-3-10 22:06:25 |只看该作者

图解直升机英语(s-92为例)fficeffice" />

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Powertrain schematic 动力系统示意图

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Tail gear box 尾减

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Intermediate gearbox 中介减速器

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main rotor shaft 主旋翼轴

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Tail take-off 尾输出轴

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structure and general

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Hydraulic utility drive 液压系统驱动装置

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overrunning clutch 超转离合器

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quill shaft 主轴

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sun gear and planet gears 太阳齿轮和行星齿轮

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Hydraulic module shaft gear 液压组件轴齿轮

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ring gear (stationary) 环型齿轮(静止)

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generator shaft gear 发电机齿轮

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主旋翼桨叶示意图

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Leading edge counter weight 前缘配重

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De-ice element 防冰组件

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structure and general

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Titanium/nickel leading edge erosion protection /镍前缘摩擦保护

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Leading edge sheath 前缘蒙皮

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Lower fibreglass skin 下部玻璃纤维蒙皮

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Upper fibreglass skin 上部玻璃纤维蒙皮

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Honeycomb core 蜂窝材料

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Titanium edge stiffener 钛后缘加强件

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Graphite/fibreglass spar 石墨/玻璃纤维大梁

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Instrument panel,central pedestal and side consoles

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仪表板,中央和侧面控制台

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structure and general

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A Standby compass 备用罗盘

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B Backup instruments 备用仪表

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C Master warning panel 主警告面板

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D Collins multi function displays (4) with central optional display

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多功能显示器

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structure and general

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E Cargo hook release 货钩释放

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F Pilot flight director mode select 驾驶员飞行指示器方式选择

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G Copilot flight director mode select 副驾驶飞行指示器方式选择

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H Digital clock 数字时钟

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I Compess unit 罗盘组件

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3#
发表于 2009-3-10 22:06:36 |只看该作者

J Audio controller 音频控制器fficeffice" />

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K FDR/CVR controller 数据记录/话音记录控制器

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L HUMS 使用状态监控系统

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M Pass brief control panel

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N FMS data loader 飞行管理数据输入器

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O Weather radar controller 气象雷达控制器

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P Radio tuning unit 无线电调谐器

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Q Display controller 显示控制器

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R FMS/GPS CDU 飞行管理/全球定位系统控制显示组件

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S AFCS (FCG) contro1 panel 自动飞行控制系统控制面板

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T Backup control panel 控制面板备用

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U Reversionary control 保留控制

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V Remote instrument control 远距离仪表控制

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W Deployable emergency beacon 释放式紧急信标

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structure and general

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X Misc switch panel 其他配电盘

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Y Landing gear contro1s 起落架控制

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Z Parking brake 停机刹车

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Fuel cell and installed system 油箱及安装的系统

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F1 Sponson fuel cells(2) with 35OUS gallon useab1e fuel in each cell

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浮筒油箱

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F2 Rubber bladder tank 气囊箱

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structure and general

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F3 Tank high level sensor 高油面传感器

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F4 Vent valves 通气阀门

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F5 Fuel quantity probes 油量传感器

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F6 Fuel low level sensors 低油面传感器

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F7 Low level shut-off valve 低油面关断阀门

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F8 Engine fuel feed check valve 发动机供油单向阀门

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F9 Fuel sump drain valve 燃油箱放油阀门

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F10 Tank vent lines 油箱通气管

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F11 Access cover to fuel cell 油箱蒙皮盖板

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F12 Gravity retueling point- typical both sponsons (pressure refuel Point on port sponson)

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4#
发表于 2009-3-10 22:06:47 |只看该作者

重力加油口-典型布置两侧都有,压力加油在左侧。fficeffice" />

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F13 Refuel/defuel line - under fuselage floor /放油管

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F14 Engine prime/APU feed line 发动机加油/辅助动力装置供油管

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F15 Auxiliary tank connection 副油箱接头

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F16 Gravity fill port cover 重力加油口盖

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F17 Fuel pickup valve 燃油传感器阀门

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飞行操纵系统

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structure and general

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structure and general

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structure and general 结构和通用设备

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1 upward hinging radome door for access to forward avionics bay

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向上打开的机头电子设备舱罩

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2 Pitot heads - one on stbd side and two on port side

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空速管,一个在右侧,两个在左侧  (stbd = starboard右侧)

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3 Extemal pewer receptacle Panel 外接电源插座

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4 Jettisonable cockpit windows 可抛放座舱玻璃

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5 Hinged clearview Panel 可开启观察窗

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6 Two-crew flightdeck with 4 LCD primary dispplays,optional fiffh display and flight management System

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双人驾驶舱,装有4个主要液晶显示器,可选装第5显示器和飞行管理系统

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7 Side consoles both sides 侧面操纵板,两侧

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8 overhead console 顶部操纵板

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9 Manual rotor brake operating handle 手动旋翼刹车手柄

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10 Martin baker crew seats 马丁贝克驾驶员座椅

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11 Cockpit fire extinguisher 驾驶舱灭火器

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12 Circuit breaker panels - both sides 断路器面板

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structure and general

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13 Downward vision window 下视观察窗

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14 Forward flotation bags- one each side 前漂浮气囊,每侧一个

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15 Map case both sides 地图盒,两侧

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16 Beverage holder 饮料固定器

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17 Composite bird-strike proof canopy and semi-monocoque aluminium alloy cockpit structure with built up structure and machined frames bullt by

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Aerospace Industrial Development Corporation' TaiwanChina

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复合材料防(鸟)撞蒙皮和由中国台湾制造的半硬壳式铝合金结构座舱

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18 Semi-monocoque aluminium alloy cabin structure with machined fuselage frames and floor beams built by Mitsubushi Heavy Industries

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由三菱重工制造的半硬壳式铝合金结构客舱和地板横梁

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5#
发表于 2009-3-10 22:06:58 |只看该作者

19 Rescue hoist 救生绞车fficeffice" />

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20 Silding fairing composite, shown in fully forward Position

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滑动整流罩,图示为最前位置

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21 Access door into sliding fairing composite 整流罩入口

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22 Composite top deck fairings。 复合材料顶部整流罩

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23 Engine cowlingshown fully down 发动机整流罩,图示为完全打开

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24 Work platform 工作台

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25 Strongback Structure composite supports fairings and auxiliary power unit and air conditioning system doors

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复合材料定位板支撑的整流罩和辅助动力装置及空气调节系统舱门

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26 Forward part of sponson composite structure,housing fuel cell and flotation bag

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structure and general

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浮筒前部为复合材料,内装油箱和气囊

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27 Aft sponson aluminum alloy construction with machined frames and composite construction Houses main undercarriage and condenser for air

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conditioning system

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浮筒后部为铝合金,内装主起落架和空调系统的冷凝器。

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28 Jettisonable life rafts in leeding edge compartment of sponson liferafts 14 man 5O% overload capacityboth sides

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浮筒前部的可抛放充气救生船,可承载15人,由5O%超载能力,两侧。

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29 Handhold 手柄

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30 Kick in step 脚蹬

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31 Compressed gas bottles for inflation of forward floatation bageschoice of using nitrogen or helium

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供应前部气囊的压缩气瓶,可选氮气或氦气

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32 Composite cabin floor 复合材料地板

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33 Composite cabin interior side panels 复合材料客舱壁板

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34 Cabin windows also available as push out windows

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客舱窗户,有可推出的窗户

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35 50x70ffice:smarttags" />75in cabin door which slides aft The rear part of the door slides into a slot in the forward part of the sponson

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向后滑动的客舱门,门后部滑入浮筒前面的缝隙里。

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36 Escape panel in cabin door 客舱门护板

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37 Emergency exit, two on Port side 紧急出口,左侧两个。

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38 Compressed gas bottles for inflation of aft floatation bag choice of using nitrogen or helium

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structure and general

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供应后部气囊的压缩气瓶,可选氮气或氦气

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39 Right hand sight glass for float bottle pressure

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压缩气瓶压力观察窗

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40 Rear loading ramp, shown in down position Optional baggage shelf bulkhead and nets which are accessible from the ramp are available (1,000lb

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maxlmum weight, 140ft3

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)

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后部装载斜板,图示为放下位置。可选行李架、防水壁和网。

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41 Rear fuselage of aluminium alloy with composite fairings

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铝合金后机身带复合材料整流罩

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42 Composite fairings covering drive shaft to tail rotor

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尾传动轴复合材料整流罩

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6#
发表于 2009-3-10 22:07:16 |只看该作者

43 Tail Structure of aluminium alloy with machined frames and composite fairings Built by Jingdezhen Helicopter Group' Chinafficeffice" />

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铝合金尾梁结构和复合材料整流罩,有中国景德镇直升机公司制造。

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44 Fixed horizontal stabiliser of composite construction with machined spars  复合材料固定水平安定面,

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45 Support strut for horizontal stabiliser 水平安定面支柱

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46 Pull out maintenance steps 收放维护踏板

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47 Removable composite leading edge fairing 可拆卸尾整流罩前缘

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48 Removable composite trailing edge fairing 可拆卸尾整流罩后缘

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49 Swiveling 2-axis hook1O,Office:smarttags" />00lb capacity

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2轴旋转吊钩,可挂10000

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structure and general

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50 Tie down fittings 系留环

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51 Aft flotaion bag 后部气囊

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52 Manual overhead door composite 复合材料手动舱门

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53 Mixer work plattorm 混合器工作平台

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Air-conditioning/anti-ice systems 空调/防冰系统

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A1 Chin window defog line 机头下部窗除雾管路

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A2 Ejectors for heated air at feet 脚部热空气出口

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A3 Under seat heating ejector 座椅下热空气出口

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A4 Side window defog line 侧窗除雾管路

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A5 Right hand cockpit vent/air conditioning gaspers

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右驾驶舱通风/空调口

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A6 Fresh air intake for cockpit 驾驶舱新鲜空气入口

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A7 Electric evaporator fan - cockpit 蒸发器风扇

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A8 Cockpit evaporator 驾驶舱蒸发器

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A9 Fresh air intake valve - cockpit 驾驶舱新鲜空气入口阀门

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A10 Evaporotor for cabin   客舱蒸发器

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A11 Fresh air inlet for cabin  客舱新鲜空气入口

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A12 Compressors/electric motor drive  压缩器/电机驱动 

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A13 Condenser   冷凝器

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structure and general

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A14 Lines from condenser to compressors 冷凝器至压缩器管路

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Al5 cabin ejectors for warm air   客舱热空气出口

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A16 Air conditioning service port   空调维修孔

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A17 Electrically heated inlet  电加温进气口

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A18 Cabin supply line   客舱供气管路

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Flying controls/Rotor systems/Drivetrain

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飞行操纵系统/旋翼系统/传动系统

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7#
发表于 2009-3-10 22:07:28 |只看该作者

C1 Yaw control pedals  偏航控制踏板(脚蹬)fficeffice" />

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C2 Yaw control pedal adjuster  偏航控制踏板(脚蹬)调节器

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C3 Cyclic stick  周期变距杆(驾驶杆)

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C4 Collective stick  总距杆

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C5 Control linkage for yaw  偏航控制连杆

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C6 Control linkage for pitch  俯仰控制连杆

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C7 Control linkage for collective  总距控制连杆

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C8 Control linkage for roll  横滚控制连杆

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C9 Trim servos - electro mechanical (4)  配平伺服机构-电机  

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C10 SAS/boost modules  增稳/助力组件

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C11 Flight control mixer  飞行控制混合器

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C12 Main rotor servos (3)  主旋翼伺服机构

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structure and general

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C13 Main transmission gearbox  主减齿轮箱

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C14 Accessory module  附件箱

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C15 Input module  输入组件

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C16 No 2 engine input  2号发动机输入

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C17 Stationary swashplate  非旋转倾斜盘

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C18 Rotating swashplate  旋转倾斜盘

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C19 Stationary scissors  非旋转环扭力臂

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C20 Pitch control roads (4)  变距拉杆

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C21 Blade lag dampers (4)   桨叶减振器

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C22 Elastomeric bearing (4)  柔性轴承

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C23 Anti-flap cam (4)     挥舞限动块

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C24 Rotating scissors (2) 旋转环扭力臂

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C25 Yoke (4) 星型件

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C26 Main rotor hub 主旋翼桨毂

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C27 Blade cuffs (4) 桨叶连接衬套

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C28 Main rotor vibration absorbing system (Bifilar) 主旋翼减振系统

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C29 Main rotor blade is all composite with nickel and titanium abrasion strips and a removable tip cap assembly Wire mesh is bonded to the blade surface to

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protect the blade from lightning strikes A leading edge sheath containing an abrasion strip and optional deice mat is bonded to the leading edge of the spar to

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form the forward air foil contour Attaches to the cuff with six fasteners

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structure and general

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主旋翼桨叶是镍、钛复合材料制成,有可拆卸桨尖罩。桨叶表面覆盖金属网以防止雷击。前缘有摩擦带和可选的防冰带,使用6个连接螺丝。

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C30 Trim tabs 调整片

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C31 Droop stop 下限动块

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C32 Blade retention pin shown removed 桨叶固定销,图示已拆除

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C33 Transmission oil cooler 主减滑油散热器

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C34 Drive shaft to tail rotor 尾传动轴

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C35 Drive shaft snubber damper 尾传动轴减震器

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C36 Elastomeric support bearing 柔性支撑轴承

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C37 intermediate geatbox 中介齿轮箱

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C38 Tail rotor control tables 尾桨操纵拉杆

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C39 Tail gear box drive shaft 尾减驱动轴

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C40 Tail gear box 尾减

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C41 Pitch beam 变距梁

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C42 Pitch change links - elastomeric rod end bearings (4)

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变距拉杆,柔性杆和轴承

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8#
发表于 2009-3-10 22:07:39 |只看该作者

C43 Tail rotor hub 尾桨毂fficeffice" />

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C44 Tail rotor blades with titanium pitch horns (4) made up of an inboard torque tube section and an outboard air foil section and a composite graphite/

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fibreglass flexbeam

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尾桨桨叶,有内部扭距管和外部衬套及石墨/玻璃纤维复合材料梁组成。

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structure and general

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Electrics and electronics 电气

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E1 Honeywell Primus 88O weather radar or WX-7O1 weather radar antenna 气象雷达天线

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E2 400 amp converter   400安培变流机

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E3 24 amp battery   24安培电瓶

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E4 WX-701 radio transmitter/receiver   无线电收发机

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E5 Standby indicator auxiliary battery 备份指示器辅助电瓶

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E6 400 amp converter   400安培变流机

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E7 Electric windscreen wipers    电动风档雨刷

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E8 Right hand avionics rack    右侧电子设备架

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E9 Left hand avonics rack     左侧电子设备架

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E10 DME transceiver   测距机收发机

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E11 ADF receiver   无线电罗盘接收机

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E12 VOR/lLS receiver   伏尔/仪表着陆系统接收机

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E13 Data concentrator   数据集中器

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E14 RADALT receiver/transmitter  无线电高度表收发机

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E15 Transponder receiver/transmitter  应答机收发机

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E16 VHF receiver   甚高频接收机

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E17 Battery PDP  电瓶配电盘

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E18 No 2 AFCS computer  2号自动飞行控制系统计算机

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structure and general

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E19 External power AC monitor  外接交流电源监视器

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E20 Active vibration control computer   主动式振动控制计算机

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E21 RADALT receiver/transmitter  无线电高度表收发机

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E22 VHF receiver  甚高频接收机

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E23 VOR/ILS receiver  伏尔/仪表着陆系统接收机

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E24 ADF receiver  无线电罗盘接收机

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E25 DME receiver  测距机收发机

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E26 Transponder receiver/transmitter  应答机收发机

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E27 Hums main processor with FDR/CVR unit alongside

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使用状态监控系统处理器和飞行数据记录器/驾驶舱话音记录器

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E28 Page chime  呼叫铃

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E29 Passenger briefing module  客舱广播组件

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E30 Maintenance date concentrator, Data concentrator 1 and aural waring generator also on this shelf of rack

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维护数据集中器,1号数据集中器和音响告警发生器

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E31 Strapping module  搭接组件

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E32 No 1 AFCS computer   1号自动飞行控制系统计算机

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E33 FLIR  前视红外探测系统

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E34 Emergency locator transmitter (ELT)  紧急定位发射机

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E35 VHF antennae   甚高频天线

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structure and general

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E36 ELT antenna   无线电高度表天线

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E37 VOR/LOC antennae  伏尔/着陆航向信标台天线

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E38 Compass flux valves  罗盘感应式磁传感器

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E39 FDR/CVR no 2   2号飞行数据记录器/驾驶舱话音记录器

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E40 AHRS  姿态航向基准系统

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E41 AHRS  姿态航向基准系统

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E42 Battery for deployable emergency beacon  释放式紧急信标电瓶

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E43 Anti-collision light  防撞灯

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E44 Nav lights  航行灯

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Effice:smarttags" />45 AC genether on each accessory drive (2)

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每个附件传动箱一台交流发电机

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E46 APU electronic sequence unit  辅助动力装置起动顺序器

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E47 GPS antenna provisions  全球定位系统天线

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E48 Right hand aft emergency exit light  右后紧急出口灯

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E49 Outside air temperature gauge  外界大气温度表

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E50 FCC gauge  飞行控制中心指示器

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9#
发表于 2009-3-10 22:07:50 |只看该作者

E51 DC power contactors  直流电源接触器fficeffice" />

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E52 Ramp control pendant storage - optional  

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structure and general

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斜板控制悬吊装置存放处-可选

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E53 Static discharge wicks  静电放电刷

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Powerplant  动力装置

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P1 General Electric CT7-8 turboshaft engines (2)  涡轴发动机

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P2 Engine exhaust jet pipe   发动机排气管

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P3 Engine bay with titanium firewalls  带钛合金防火墙的发动机舱

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P4 HoneyWell 36-15O auxiliary Power unit (APU)  辅助动力装置

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P5 Air inlet plenum for APU  辅助动力装置进气口

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P6 APU hot section enclosure  辅助动力装置热段舱

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P7 Hinged door for access to engine fire bottles

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去发动机灭火瓶的铰接门

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P8 Main and reserve engine/APU fire bottles

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发动机/辅助动力装置灭火瓶

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Undercarriage/hydraulics  起落架/液压系统

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U1 Retractable nose landing gear, hydraulically actuated, Free castors through 360°。

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液压收放前起落架,可360°旋转。

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U2 Retractable main landing gear hydraulically actuated

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液压收放主起落架

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U3 Main landing gear retract actuator  主起落架收放作动筒

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structure and general

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U4 Hydraulic pump, one on each accessory drive (2)

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液压泵,每个附件箱一个

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U5 Hydraulic utility supply module  公用液压供给组件

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U6 Hydraulic hand fiffice:smarttags" />1l pump  手动加油泵

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U7 Selective valve for U6  手动加油泵选择阀门

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U8 Hydraulic actuators for rear loading ramp   货物装载斜板作动筒

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U9 Main landing gear servicing access panel   主起落架维修盖板

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U10 Ramp actuator control valve  斜板作动筒控制阀门

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U11 Ramp control panel  斜板控制面板

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U12 No 2 transfer module No 1 other side

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2号转换组件,1号在另一侧

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Rank: 1

10#
发表于 2009-10-11 12:34:04 |只看该作者
学习一下,谢谢

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