首页> 外国专利> Rotor flapping hinge for use in rotor arrangement of e.g. helicopter, has rotor holder arranged at support part such that angle between longitudinal axis of rotor and pivoting axis is in preset range after attaching rotor at rotor holder

Rotor flapping hinge for use in rotor arrangement of e.g. helicopter, has rotor holder arranged at support part such that angle between longitudinal axis of rotor and pivoting axis is in preset range after attaching rotor at rotor holder

机译:用于例如转子布置的转子拍打铰链。直升飞机,在支座上安装了旋翼支架后,将旋翼安装在旋翼支架上后,旋翼的纵轴和枢轴之间的角度在预设范围内

摘要

The hinge (1) has a support part (3) provided with a rotor holder (4) and pivotable relative to a base body (2) around a pivoting axis (5). A rotor is attached to the rotor holder. The rotor holder is arranged at the support part such that an angle between a longitudinal axis of the rotor and the pivoting axis ranges from 30 to 50 degrees after attaching the rotor at the rotor holder. The rotor holder comprises longitudinal sides that extend parallel to the longitudinal axis of the rotor after mounting the rotor.
机译:铰链(1)具有设置有转子支架(4)的支撑部分(3),并且该支撑部分(3)可绕枢转轴线(5)相对于基体(2)枢转。转子附接到转子保持器。转子保持器布置在支撑部处,使得在将转子附接到转子保持器之后,转子的纵向轴线与枢转轴线之间的角度在30度至50度的范围内。转子支架包括在安装转子之后平行于转子的纵向轴线延伸的纵向侧。

著录项

  • 公开/公告号DE102009012903A1

    专利类型

  • 公开/公告日2010-09-16

    原文格式PDF

  • 申请/专利权人 WIGGERICH BURKHARD;

    申请/专利号DE20091012903

  • 发明设计人 WIGGERICH BURKHARD;

    申请日2009-03-12

  • 分类号B64C27/39;

  • 国家 DE

  • 入库时间 2022-08-21 18:28:21

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