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Aircraft landing wheels pre-rotator - has aerodynamic projections sliding in radial wheel channels and biassed by springs

机译:飞机起落架预旋转器-具有在径向轮通道中滑动并受弹簧偏置的空气动力学突起

摘要

The device for pre-rotating aircraft landing wheels comprises two or more aerodynamic projections (2) carried radially, movably in channels formed in wheel spokes. The obstructions slide on guide rails (3) in the channel sides. The guide rails slope relative to spoke thickness so that the obstructions are progressively withdrawn into the spokes as they move outwards. The centrifugal force causing this movement is opposed by a spring (4) so that it is arrested when the wheels are turning at the right speed.
机译:用于使飞机起落架预旋转的装置包括两个或更多个径向地可移动地承载在形成于轮辐中的通道中的空气动力学突起(2)。障碍物在通道侧的导轨(3)上滑动。导轨相对于轮辐厚度倾斜,以使障碍物在向外移动时逐渐缩回到轮辐中。导致该运动的离心力被弹簧(4)抵消,因此当车轮以正确的速度旋转时,离心力会被阻止。

著录项

  • 公开/公告号DE2711123A1

    专利类型

  • 公开/公告日1978-09-28

    原文格式PDF

  • 申请/专利权人 WEBERHANS-DIETER;

    申请/专利号DE19772711123

  • 发明设计人 WEBERHANS-DIETER;

    申请日1977-03-15

  • 分类号B64C25/40;

  • 国家 DE

  • 入库时间 2022-08-22 21:58:07

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