首页> 外国专利> Rotor blade track adjustment for helicopters - using control rod coordinated with each rotor blade, with adjustment carried out in flight and indicated in cockpit

Rotor blade track adjustment for helicopters - using control rod coordinated with each rotor blade, with adjustment carried out in flight and indicated in cockpit

机译:直升机的旋翼轨迹调整-使用与每个旋翼叶片协调的控制杆,在飞行中进行调整并在驾驶舱中显示

摘要

The installation adjusts the running track of helicopter rotor blades. Each rotor blade is coordinated with a length adjustable control rod with an adjusting motor connected to the supply unit for the rotor blade control. The adjustment of each control rod may be carried out during flight by remote control from a command console in the cockpit of the helicopter through a receiver section for the adjustment motor positioned on the rotatable head of the rotor. Indicators are provided which confirm the degree of rotor blade adjsutment on the cockpit instrumentation.
机译:该安装可调整直升机旋翼桨叶的运行轨迹。每个转子叶片都与一个长度可调的控制杆配合,控制杆带有一个调节电机,该调节电机连接到用于转子叶片控制的供应单元上。每个控制杆的调节可以在飞行期间通过从直升机驾驶舱中的命令控制台通过接收器部分进行遥控来进行,该接收器部分用于位于转子的可旋转头上的调节马达。提供的指示器可确认驾驶舱仪器上转子叶片的贴合程度。

著录项

  • 公开/公告号DE2757617A1

    专利类型

  • 公开/公告日1979-06-28

    原文格式PDF

  • 申请/专利权人 HENSCHEL FLUGZEUG-WERKE AG;

    申请/专利号DE19772757617

  • 发明设计人 THOMELMAR;

    申请日1977-12-23

  • 分类号B64C27/54;

  • 国家 DE

  • 入库时间 2022-08-22 19:47:28

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