首页> 外国专利> Brief description of embodiments of an envelope, in particular for space balloons, envelope completed, and the use of that - in the field aerospace

Brief description of embodiments of an envelope, in particular for space balloons, envelope completed, and the use of that - in the field aerospace

机译:信封实施例的简要说明,特别是用于太空气球的信封,已完成信封的信封及其在野外航空航天中的用途

摘要

A stress control mechanism for a space balloon is comprised of an axial tie member extending from the upper pole of a load carrying space balloon envelope, the tie member passing from the upper pole of the space balloon envelope through the balloon to an aperture located in a slideable member attached to the lower pole of the space balloon, a stopping member positioned at a pre-selected point on the axial tie member as a member for stopping the slideable member and thereby permitting the space balloon to assume a pre-selected shape upon inflation of the space balloon.
机译:一种用于太空气球的应力控制机构,其包括从承载太空气球外壳的上极延伸的轴向束缚构件,该束缚构件从太空气球外壳的上极穿过气球到达位于外壳中的孔。可滑动构件附接到空间气球的下杆,止动构件定位在轴向系紧构件上的预选点处,作为用于使可滑动构件停止的构件,从而允许空间气球在膨胀时呈现预选形状太空气球

著录项

  • 公开/公告号FR2472971B1

    专利类型

  • 公开/公告日1982-10-01

    原文格式PDF

  • 申请/专利权人 CENTRE NAL ETUDES SPATIALES;

    申请/专利号FR19800000343

  • 发明设计人

    申请日1980-01-04

  • 分类号B31B41/60;B64B1/40;

  • 国家 FR

  • 入库时间 2022-08-22 12:30:07

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