直升机部件.doc

_Tail gear box 尾减Intermediate gearbox 中介减速器main rotor shaft 主旋翼轴Tail take-off 尾输出轴Hydraulic utility drive 液压系统驱动装置overrunning clutch 超转离合器quill shaft 主轴sun gear and planet gears 太阳齿轮和行星齿轮Hydraulic module shaft gear 液压组件轴齿轮ring gear (stationary) 环型齿轮(静止)generator shaft gear 发电机齿轮Leading edge counter weight 前缘配重De-ice element 防冰组件Titanium/nickel leading edge erosion protection 钛/镍前缘摩擦保护Leading edge sheath 前缘蒙皮Lower fibreglass skin 下部玻璃纤维蒙皮Upper fibreglass skin 上部玻璃纤维蒙皮Honeycomb core 蜂窝材料Titanium edge stiffener 钛后缘加强件Graphite/fibreglass spar 石墨/玻璃纤维大梁A Standby compass 备用罗盘B Backup instruments 备用仪表C Master warning panel 主警告面板D Collins multi function displayswith central optional display多功能显示器E Cargo hook release 货钩释放F Pilot flight director mode select 驾驶员飞行指示器方式选择G Copilot flight director mode select 副驾驶飞行指示器方式选择H Digital clock 数字时钟I Compess unit 罗盘组件J Audio controller 音频控制器K FDR/CVR controller 数据记录/话音记录控制器L HUMS 使用状态监控系统M Pass brief control panelN FMS data loader 飞行管理数据输入器O Weather radar controller 气象雷达控制器P Radio tuning unit 无线电调谐器Q Display controller 显示控制器R FMS/GPS CDU 飞行管理/全球定位系统控制显示组件S AFCS (FCG) contro1 panel 自动飞行控制系统控制面板T Backup control panel 控制面板备用U Reversionary control 保留控制V Remote instrument control 远距离仪表控制W Deployable emergency beacon 释放式紧急信标X Misc switch panel 其他配电盘Y Landing gear contro1s 起落架控制Z Parking brake 停机刹车F1 Sponson fuel cells with 35OUS gallon useab1e fuel in each cell浮筒油箱F2 Rubber bladder tank 气囊箱F3 Tank high level sensor 高油面传感器F4 Vent valves 通气阀门F5 Fuel quantity probes 油量传感器F6 Fuel low level sensors 低油面传感器F7 Low level shut-off valve 低油面关断阀门F8 Engine fuel feed check valve 发动机供油单向阀门F9 Fuel sump drain valve 燃油箱放油阀门F10 Tank vent lines 油箱通气管F11 Access cover to fuel cell 油箱蒙皮盖板F12 Gravity retueling point- typical both sponsons (pressure refuel Point on port sponson)重力加油口-典型布置两侧都有，压力加油在左侧。F13 Refuel/defuel line - under fuselage floor 加/放油管F14 Engine prime/APU feed line 发动机加油/辅助动力装置供油管F15 Auxiliary tank connection 副油箱接头F16 Gravity fill port cover 重力加油口盖F17 Fuel pickup valve 燃油传感器阀门1 upward hinging radome door for access to forward avionics bay向上打开的机头电子设备舱罩2 Pitot heads - one on stbdside and two on port side空速管,一个在右侧，两个在左侧(stbd=starboard右侧)3 Extemal pewer receptacle Panel 外接电源插座4 Jettisonable cockpit windows 可抛放座舱玻璃5 Hinged clearview Panel 可开启观察窗6 Two-crew flightdeck with 4 LCD primary dispplays,optional fiffh display and flight management System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7 Side consoles both sides 侧面操纵板，两侧8 overhead console 顶部操纵板9 Manual rotor brake operating handle 手动旋翼刹车手柄10 Martin baker crew seats 马丁贝克驾驶员座椅11 Cockpit fire extinguisher 驾驶舱灭火器12 Circuit breaker panels - both sides 断路器面板13 Downward vision window 下视观察窗14 Forward flotation bags- one each side 前漂浮气囊，每侧一个15 Map case both sides 地图盒，两侧16 Beverage holder 饮料固定器17 Composite bird-strike proof canopy and semi-monocoque aluminium alloy cockpit structure with built up structure and machined frames bullt by Aerospace Industrial Development Corporation Taiwan，China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18 Semi-monocoque aluminium alloy cabin structure with machined fuselage frames and floor beams built by Mitsubushi Heavy Industries由三菱重工制造的半硬壳式铝合金结构客舱和地板横梁19 Rescue hoist 救生绞车20 Silding fairing composite, shown in fully forward Position。滑动整流罩，图示为最前位置21 Access door into sliding fairing composite 整流罩入口22 Composite top deck fairings。 复合材料顶部整流罩23 Engine cowling，shown fully down 发动机整流罩，图示为完全打开24 Work platform 工作台25 Strongback Structure composite supports fairings and auxiliary power unit and air conditioning system doors。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26 Forward part of sponson composite structure,housing fuel cell and flotation bag浮筒前部为复合材料，内装油箱和气囊27 Aft sponson aluminum alloy construction with machined frames and composite construction。 Houses main undercarriage and condenser for air conditioning system。浮筒后部为铝合金，内装主起落架和空调系统的冷凝器。28 Jettisonable life rafts in leeding edge compartment of sponson。 liferafts 14 man， 5O% overload capacity，both sides。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。29 Handhold 手柄30 Kick in step 脚蹬31 Compressed gas bottles for inflation of forward floatation bages，choice of using nitrogen or helium供应前部气囊的压缩气瓶，可选氮气或氦气32 Composite cabin floor 复合材料地板33 Composite cabin interior side panels 复合材料客舱壁板34 Cabin windows also available as push out windows客舱窗户，有可推出的窗户35 50x70.75in cabin door which slides aft。 The rear part of the door slides into a slot in the forward part of the sponson向后滑动的客舱门，门后部滑入浮筒前面的缝隙里。36 Escape panel in cabin door 客舱门护板37 Emergency exit, two on Port side 紧急出口，左侧两个。38 Compressed gas bottles for inflation of aft floatation bag， choice of using nitrogen or helium供应后部气囊的压缩气瓶，可选氮气或氦气39 Right hand sight glass for float bottle pressure压缩气瓶压力观察窗40 Rear loading ramp, shown in down position。 Optional baggage shelf， bulkhead and nets which are accessible from the ramp are available (1,000lb maxlmum weight, 140ft3)后部装载斜板，图示为放下位置。可选行李架、防水壁和网。41 Rear fuselage of aluminium alloy with composite fairings。铝合金后机身带复合材料整流罩42 Composite fairings covering drive shaft to tail rotor尾传动轴复合材料整流罩43 Tail Structure of aluminium alloy with machined frames and composite fairings。 Built by Jingdezhen Helicopter Group China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。44 Fixed horizontal stabiliser of composite construction with machined spars复合材料固定水平安定面45 Support strut for horizontal stabiliser 水平安定面支柱46 Pull out maintenance steps 收放维护踏板47 Removable composite leading edge fairing 可拆卸尾整流罩前缘48 Removable composite trailing edge fairing 可拆卸尾整流罩后缘49 Swiveling 2-axis hook，1O,O00lb capacity2轴旋转吊钩，可挂10，000磅。50 Tie down fittings 系留环51 Aft flotaion bag 后部气囊52 Manual overhead door composite 复合材料手动舱门53 Mixer work plattorm 混合器工作平台Air-conditioning/anti-ice systems 空调/防冰系统A1 Chin window defog line 机头下部窗除雾管路A2 Ejectors for heated air at feet 脚部热空气出口A3 Under seat heating ejector 座椅下热空气出口A4 Side window defog line 侧窗除雾管路A5 Right hand cockpit vent/air conditioning gaspers右驾驶舱通风/空调口A6 Fresh air intake for cockpit 驾驶舱新鲜空气入口A7 Electric evaporator fan - cockpit 蒸发器风扇A8 Cockpit evaporator 驾驶舱蒸发器A9 Fresh air intake valve - cockpit 驾驶舱新鲜空气入口阀门A10 Evaporotor for cabin 客舱蒸发器A11 Fresh air inlet for cabin客舱新鲜空气入口A12 Compressors/electric motor drive压缩器/电机驱动A13 Condenser冷凝器A14 Lines from condenser to compressors 冷凝器至压缩器管路Al5 cabin ejectors for warm air客舱热空气出口A16 Air conditioning service port空调维修孔A17 Electrically heated inlet电加温进气口A18 Cabin supply line 客舱供气管路Flying controls/Rotor systems/Drivetrain飞行操纵系统/旋翼系统/传动系统C1 Yaw control pedals偏航控制踏板(脚蹬)C2 Yaw control pedal adjuster偏航控制踏板(脚蹬)调节器C3 Cyclic stick周期变距杆(驾驶杆)C4 Collective stick总距杆C5 Control linkage for yaw偏航控制连杆C6 Control linkage for pitch俯仰控制连杆C7 Control linkage for collective总距控制连杆C8 Control linkage for roll横滚控制连杆C9 Trim servos - electro mechanical 配平伺服机构-电机C10 SAS/boost modules增稳/助力组件C11 Flight control mixer飞行控制混合器C12 Main rotor servos主旋翼伺服机构C13 Main transmission gearbox主减齿轮箱C14 Accessory module附件箱C15 Input module输入组件C16 No 2 engine input2号发动机输入C17 Stationary swashplate非旋转倾斜盘C18 Rotating swashplate旋转倾斜盘C19 Stationary scissors非旋转环扭力臂C20 Pitch control roads 变距拉杆C21 Blade lag dampers桨叶减振器C22 Elastomeric bearing柔性轴承C23 Anti-flap cam 挥舞限动块C24 Rotating scissors 旋转环扭力臂C25 Yoke星型件C26 Main rotor hub 主旋翼桨毂C27 Blade cuffs桨叶连接衬套C28 Main rotor vibration absorbing system (Bifilar) 主旋翼减振系统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 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 form the forward air foil contour。 Attaches to the cuff with six fasteners。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。C30 Trim tabs 调整片C31 Droop stop 下限动块C32 Blade retention pin， shown removed 桨叶固定销，图示已拆除C33 Transmission oil cooler 主减滑油散热器C34 Drive shaft to tail rotor 尾传动轴C35 Drive shaft snubber damper 尾传动轴减震器C36 Elastomeric support bearing 柔性支撑轴承C37 intermediate geatbox 中介齿轮箱C38 Tail rotor control tables 尾桨操纵拉杆C39 Tail gear box drive shaft 尾减驱动轴C40 Tail gear box 尾减C41 Pitch beam 变距梁C42 Pitch change links - elastomeric rod end bearings 变距拉杆，柔性杆和轴承C43 Tail rotor hub 尾桨毂C44 Tail rotor blades with titanium pitch hornsmade up of an inboard torque tube section and an outboard air foil section and a composite graphite/fibreglass flexbeam。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。Electrics and electronics 电气E1 Honeywell Primus 88O weather radar or WX-7O1 weather radar antenna 气象雷达天线E2 400 amp converter 400安培变流机E3 24 amp battery 24安培电瓶E4 WX-701 radio transmitter/receiver 无线电收发机E5 Standby indicator auxiliary battery 备份指示器辅助电瓶E6 400 amp converter 400安培变流机E7 Electric windscreen wipers 电动风档雨刷E8 Right hand avionics rack 右侧电子设备架E9 Left hand avonics rack 左侧电子设备架E10 DME transceiver 测距机收发机E11 ADF receiver 无线电罗盘接收机E12 VOR/lLS receiver 伏尔/仪表着陆系统接收机E13 Data concentrator 数据集中器E14 RADALT receiver/transmitter 无线电高度表收发机E15 Transponder receiver/transmitter应答机收发机E16 VHF receiver甚高频接收机E17 Battery PDP电瓶配电盘E18 No 2 AFCS computer2号自动飞行控制系统计算机E19 External power AC monitor外接交流电源监视器E20 Active vibration control computer主动式振动控制计算机E21 RADALT receiver/transmitter无线电高度表收发机E22 VHF receiver甚高频接收机E23 VOR/ILS receiver伏尔/仪表着陆系统接收机E24 ADF receiver无线电罗盘接收机E25 DME receiver测距机收发机E26 Transponder receiver/transmitter应答机收发机E27 Hums main processor with FDR/CVR unit alongside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E28 Page chime呼叫铃E29 Passenger briefing module客舱广播组件E30 Maintenance date concentrator, Data concentrator 1 and aural waring generator also on this shelf of rack维护数据集中器，1号数据集中器和音响告警发生器E31 Strapping module搭接组件E32 No 1 AFCS computer 1号自动飞行控制系统计算机E33 FLIR前视红外探测系统E34 Emergency locator transmitter (ELT)紧急定位发射机E35 VHF antennae 甚高频天线E36 ELT antenna无线电高度表天线E37 VOR/LOC antennae伏尔/着陆航向信标台天线E38 Compass flux valves罗盘感应式磁传感器E39 FDR/CVR no 22号飞行数据记录器/驾驶舱话音记录器E40 AHRS姿态航向基准系统E41 AHRS姿态航向基准系统E42 Battery for deployable emergency beacon释放式紧急信标电瓶E43 Anti-collision light防撞灯E44 Nav lights航行灯E45 AC genether on each accessory drive 每个附件传动箱一台交流发电机E46 APU electronic sequence unit辅助动力装置起动顺序器E47 GPS antenna provisions全球定位系统天线E48 Right hand aft emergency exit light右后紧急出口灯E49 Outside air temperature gauge外界大气温度表E50 FCC gauge飞行控制中心指示器E51 DC power contactors直流电源接触器E52 Ramp