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Helicopter security seat, particularly for helicopters used for aerial work.

机译:直升机安全座椅,特别是用于高空作业的直升机。

摘要

The seat comprises a base support (12) with a first set of rear attachment points (13) and second attachment points at the rear (17) for a seat shell (11) situated opposite to the transverse plane holding the pilot-seat unit's vertical barycentre. Corresponding to the first set of attachment points is a hinge on the transverse axis inside which the seat shell is free to rotate in relation to the support. The second attachment points are equipped with supports and reversers, with prefixed resistance, to allow the shell to rotate, through subsidence, inside the hinge axis and setting it down sub-horizontally.
机译:座椅包括基座支撑件(12),该基座支撑件具有第一组后部附接点(13)和位于后部(17)的第二附接点,用于座椅壳(11),该座椅壳与保持飞行员座椅单元垂直方向的横向平面相对重心。与第一组附接点相对应的是横轴上的铰链,座椅壳体在铰链内相对于支撑件自由旋转。第二个连接点配备了带有前缀阻力的支撑和反向器,以允许壳体通过沉降在铰链轴内部旋转并使其在水平方向下放。

著录项

  • 公开/公告号IT1237270B

    专利类型

  • 公开/公告日1993-05-27

    原文格式PDF

  • 申请/专利权人

    申请/专利号IT19890068010

  • 发明设计人

    申请日1989-11-16

  • 分类号5B64DA;

  • 国家 IT

  • 入库时间 2022-08-22 05:09:59

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