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System for separating separable spacecraft and shuttle elements

机译:分离可分离航天器和航天飞机元件的系统

摘要

A separation system for separable elements of spacecraft and launchers includes an upper ring, a lower ring and a band with an inner channel which houses slidable clamps, which are applied against the upper ring and the lower ring that form the connection interface between the two separable elements. A device joins/separates the ends of the band, both the upper ring and the lower ring including an outer protruding element with a wedged section to be lodged in the clamps. The upper ring also has an inner protruding element with a wedged section that matches a channel shaped section in the lower ring, the lower ring also has an outer portion including the outer protruding element with a wedged section and the channel shaped section, the outer portion protruding from a main part of the lower ring and being spaced from it creating a groove.
机译:用于航天器和发射器可分离元件的分离系统,包括一个上环,一个下环和一个带内部通道的带,该带内装有可滑动的夹具,这些夹具紧靠在上环和下环上,形成了两个可分离部件之间的连接界面元素。一种装置将带子的端部连接/分离,上环和下环均包括具有突出部分的外部突出元件,该突出部分具有楔形部分以放置在夹具中。上环还具有带有与下环中的通道形截面匹配的楔形截面的内部突出元件,下环还具有包括带有楔形截面的外部突出元件和通道形截面的外部的外部部分,该外部部分从下环的主要部分突出并与其间隔开以形成凹槽。

著录项

  • 公开/公告号US10343795B2

    专利类型

  • 公开/公告日2019-07-09

    原文格式PDF

  • 申请/专利权人 AIRBUS DEFENCE AND SPACE S.A.;

    申请/专利号US201415528470

  • 发明设计人 FRANCISCO JAVIER RIVAS SÁNCHEZ;

    申请日2014-11-25

  • 分类号B64G1/64;F42B15/36;

  • 国家 US

  • 入库时间 2022-08-21 12:13:48

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