图解直升机英语(以s-92为例) Helicopter English
时间：2011-04-05 09:32来源：蓝天飞行翻译 作者：航空 点击：次
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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 (4) 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 (3) 主旋翼伺服机构 structure and general 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 input 2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 (4) 变距拉杆 C21 Blade lag dampers (4) 桨叶减振器 C22 Elastomeric bearing (4) 柔性轴承 C23 Anti-flap cam (4) 挥舞限动块 C24 Rotating scissors (2) 旋转环扭力臂 C25 Yoke (4) 星型件 C26 Main rotor hub 主旋翼桨毂 C27 Blade cuffs (4) 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。 structure and general 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 (4)变距拉杆，柔性杆和轴承 C43 Tail rotor hub 尾桨毂 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。 structure and general |
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