圖解直升機(jī)英語(yǔ)(以s-92為例) Helicopter English
時(shí)間：2011-04-05 09:32來(lái)源：藍(lán)天飛行翻譯 作者：航空 點(diǎn)擊：次
|
Al5 cabin ejectors for warm air 客艙熱空氣出口 A16 Air conditioning service port 空調(diào)維修孔 A17 Electrically heated inlet 電加溫進(jìn)氣口 A18 Cabin supply line 客艙供氣管路 Flying controls/Rotor systems/Drivetrain飛行操縱系統(tǒng)/旋翼系統(tǒng)/傳動(dòng)系統(tǒng) C1 Yaw control pedals 偏航控制踏板（腳蹬）C2 Yaw control pedal adjuster 偏航控制踏板（腳蹬）調(diào)節(jié)器 C3 Cyclic stick 周期變距桿（駕駛桿）C4 Collective stick 總距桿 C5 Control linkage for yaw 偏航控制連桿 C6 Control linkage for pitch 俯仰控制連桿 C7 Control linkage for collective 總距控制連桿 C8 Control linkage for roll 橫滾控制連桿 C9 Trim servos - electro mechanical (4) 配平伺服機(jī)構(gòu)-電機(jī) C10 SAS/boost modules 增穩(wěn)/助力組件 C11 Flight control mixer 飛行控制混合器 C12 Main rotor servos (3) 主旋翼伺服機(jī)構(gòu) structure and general C13 Main transmission gearbox 主減齒輪箱 C14 Accessory module 附件箱 C15 Input module 輸入組件 C16 No 2 engine input 2號(hào)發(fā)動(dòng)機(jī)輸入 C17 Stationary swashplate 非旋轉(zhuǎn)傾斜盤(pán) C18 Rotating swashplate 旋轉(zhuǎn)傾斜盤(pán) C19 Stationary scissors 非旋轉(zhuǎn)環(huán)扭力臂 C20 Pitch control roads (4) 變距拉桿 C21 Blade lag dampers (4) 槳葉減振器 C22 Elastomeric bearing (4) 柔性軸承 C23 Anti-flap cam (4) 揮舞限動(dòng)塊 C24 Rotating scissors (2) 旋轉(zhuǎn)環(huán)扭力臂 C25 Yoke (4) 星型件 C26 Main rotor hub 主旋翼槳轂 C27 Blade cuffs (4) 槳葉連接襯套 C28 Main rotor vibration absorbing system (Bifilar) 主旋翼減振系統(tǒng) 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。 structure and general 主旋翼槳葉是鎳、鈦復(fù)合材料制成，有可拆卸槳尖罩。槳葉表面覆蓋金屬網(wǎng)以防止雷擊。前緣有摩擦帶和可選的防冰帶，使用6個(gè)連接螺絲。 C30 Trim tabs 調(diào)整片 C31 Droop stop 下限動(dòng)塊 C32 Blade retention pin, shown removed 槳葉固定銷(xiāo)，圖示已拆除 C33 Transmission oil cooler 主減滑油散熱器 C34 Drive shaft to tail rotor 尾傳動(dòng)軸 C35 Drive shaft snubber damper 尾傳動(dòng)軸減震器 C36 Elastomeric support bearing 柔性支撐軸承 C37 intermediate geatbox 中介齒輪箱 C38 Tail rotor control tables 尾槳操縱拉桿 C39 Tail gear box drive shaft 尾減驅(qū)動(dòng)軸 C40 Tail gear box 尾減 C41 Pitch beam 變距梁 C42 Pitch change links - elastomeric rod end bearings (4)變距拉桿，柔性桿和軸承 C43 Tail rotor hub 尾槳轂 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/ fibreglass flexbeam。 尾槳槳葉，有內(nèi)部扭距管和外部襯套及石墨/玻璃纖維復(fù)合材料梁組成。 structure and general |
上一篇：直升機(jī)全方位講述
下一篇：直升機(jī)原理詳解
推薦內(nèi)容
熱點(diǎn)內(nèi)容
