首页> 外国专利> Arrangement for controlling of rotor blades of helicopter has controlled actuator, for collective and cyclic adjustment of blade setting angle of rotor blades, which are mechanically forcibly coupled among themselves

Arrangement for controlling of rotor blades of helicopter has controlled actuator, for collective and cyclic adjustment of blade setting angle of rotor blades, which are mechanically forcibly coupled among themselves

机译:用于控制直升机旋翼的装置具有受控的致动器,用于集体和周期性地调节旋翼的叶片设定角度,旋翼在机械上彼此强制耦合。

摘要

Arrangement has controlled actuator (3), for collective and cyclic adjustment of blade setting angle of rotor blades (1), which are connected with rotor blade in such a way that its longitudinal axis runs parallel to the longitudinal axis (4) of the rotor blade. Actuators are mechanically forcibly coupled among themselves.
机译:该装置具有受控的致动器(3),用于集体和周期性地调节转子叶片(1)的叶片设定角度,转子叶片(1)的纵向轴线平行于转子的纵向轴线(4)与其连接刀。执行器之间被机械地强制连接。

著录项

  • 公开/公告号DE102005007129A1

    专利类型

  • 公开/公告日2006-08-24

    原文格式PDF

  • 申请/专利权人 ZF FRIEDRICHSHAFEN AG;

    申请/专利号DE20051007129

  • 发明设计人 HAUSBERG ANDRE;

    申请日2005-02-17

  • 分类号B64C27/54;

  • 国家 DE

  • 入库时间 2022-08-21 21:20:26

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