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Captive cable coil and its application to a regulator for deploying a lengthening piece of a space instrument

机译:束缚电缆线圈及其在用于部署空间仪器的加长件的调节器中的应用

摘要

So as to adjust the deployment of a lengthening piece of a space instrument, a captive cable coil (34) coupled to a centrifugal brake by a speed multiplier is used. The cable (40) is wound onto the coil (34) in the form of a single strand imprisoned in a roughly helical- shaped throat (38) formed, for example by machining, on the outer surface of the coil. One outer portion (42a) of the partition separating two adjacent spires of the throat is folded down onto the cable so as to prevent its volume from swelling.
机译:为了调节空间仪器的加长件的展开,使用了通过倍增器连接到离心制动器的俘获电缆线圈(34)。电缆(40)以单股形式缠绕在线圈(34)上,该单股形式被束缚在大致螺旋形的喉管(38)中,该喉管例如通过机械加工形成在线圈的外表面上。将分隔喉的两个相邻尖头的隔板的一个外部部分(42a)向下折叠到电缆上,以防止其体积膨胀。

著录项

  • 公开/公告号US5253820A

    专利类型

  • 公开/公告日1993-10-19

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE;

    申请/专利号US19910692154

  • 发明设计人 JEAN-PIERRE HENRY;

    申请日1991-04-26

  • 分类号B65H75/02;

  • 国家 US

  • 入库时间 2022-08-22 04:57:37

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