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Stabilization system for astronauts in space, comprises sectored flywheel with correctors controlling angles arising between flywheel plane and main axis

机译:太空宇航员稳定系统,包括扇形飞轮,带有校正器,可控制飞轮平面和主轴之间的角度

摘要

A sectored (A, B, C, N) flywheel mass rotates rapidly about its center of gravity which coincides with the main axis (6). Sectors can swing in a plane at right angles to the main axis, and tend to adopt a position at right angles to it. When the direction of the main axis is varied, the sectors rotate in a different plane, at an angle to it. Correctors deliver short impulses to the sectors, returning them to their former position, or causing controlled rotation through an angle, with respect to the main plane.
机译:扇形(A,B,C,N)飞轮质量绕其重心快速旋转,该重心与主轴(6)重合。扇区可以在与主轴成直角的平面内摆动,并且倾向于采用与主轴成直角的位置。当主轴方向改变时,扇形体在不同的平面中旋转,并与之成一定角度。校正器会向这些扇形施加短暂的脉冲,使它们返回到原来的位置,或者使它们相对于主平面旋转一定角度。

著录项

  • 公开/公告号DE10251274A1

    专利类型

  • 公开/公告日2004-05-19

    原文格式PDF

  • 申请/专利权人 MERLAKU KASTRIOT;

    申请/专利号DE2002151274

  • 发明设计人 MERLAKU KASTRIOT;

    申请日2002-11-04

  • 分类号B64G9/00;

  • 国家 DE

  • 入库时间 2022-08-21 22:43:45

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