首页> 外国专利> Method and device for releasing a preload initially applied to a mechanism such as a rolling bearing on board a spacecraft

Method and device for releasing a preload initially applied to a mechanism such as a rolling bearing on board a spacecraft

机译:用于释放预加载的方法和装置,该预加载最初施加于诸如航天器上的滚动轴承之类的机构

摘要

In spacecraft, the mechanisms such as ball bearings 14, 14' are subjected to an initial preload allowing them to withstand the vibrations produced by the launch, without giving rise to play. A member 34 made from a shaped memory material makes it possible, for example under the effect of its extension, to release this preload when the craft is in operational mode. The release command may be effected, in particular, by means of a heating element 36 the powering of which makes the member 34 pass beyond its shape-change temperature. IMAGE
机译:在航天器中,诸如滚珠轴承14、14'之类的机构要承受初始的预紧力,使它们能够承受发射所产生的振动,而不会产生游隙。由形状记忆材料制成的构件34使得例如在飞行器处于操作模式时例如在其延伸的作用下能够释放该预紧力。释放指令尤其可以通过加热元件36来实现,该加热元件的供电使构件34通过其形状变化温度以上。 <图像>

著录项

  • 公开/公告号FR2648200A1

    专利类型

  • 公开/公告日1990-12-14

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE STE NATIONALE INDLE;

    申请/专利号FR19890007666

  • 发明设计人 JEAN-PIERRE SCHOEFFTER;

    申请日1989-06-09

  • 分类号B64G1/22;B64G1/44;B64G1/64;B64G1/66;F16C25/08;F16C41/04;

  • 国家 FR

  • 入库时间 2022-08-22 05:48:28

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