首页> 外国专利> Fabrication process for an envelope, in particular for space balloons, envelope thus made, and its application to the aerospace domain

Fabrication process for an envelope, in particular for space balloons, envelope thus made, and its application to the aerospace domain

机译:信封的制造工艺,特别是用于太空气球的信封,由此制成的信封,及其在航空领域的应用

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US4420130A

    专利类型

  • 公开/公告日1983-12-13

    原文格式PDF

  • 申请/专利权人 CENTRE NATIONAL DETUDES SPATIALES;

    申请/专利号US19800218749

  • 发明设计人 ROBERT REGIPA;

    申请日1980-12-22

  • 分类号B64B1/40;

  • 国家 US

  • 入库时间 2022-08-22 08:40:19

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