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Releasable locking device of a flying vehicle intended for being launched from a platform

机译:用于从平台发射的飞行器的可释放锁定装置

摘要

The device (20) has a frame (40) fixed on a platform, and a releasable locking assembly (42) for locking a flying vehicle in a locked position. The assembly has front and rear gripping units (60, 62) mounted to move with respect to the frame for passing between a closed configuration to grip a retaining unit (30) of the vehicle and an open configuration to release the vehicle. The assembly has an elastic stressing mechanism (64) to stress the front gripping unit toward the rear gripping unit in the closed configuration for grasping the retaining unit between the gripping units. Independent claims are also included for the following: (1) a launching assembly (2) a method for launching a flying vehicle from a platform.
机译:装置(20)具有固定在平台上的框架(40)和用于将飞行器锁定在锁定位置的可释放锁定组件(42)。该组件具有被安装成相对于框架移动的前握持单元和后握持单元(60、62),以在用于握住车辆的保持单元(30)的闭合构造与用于释放车辆的打开构造之间通过。该组件具有弹性应力机构(64),以在闭合构造中将前握持单元朝向后握持单元施力,以将保持单元握在握持单元之间。还包括以下方面的独立权利要求:(1)发射组件(2)一种用于从平台发射飞行器的方法。

著录项

  • 公开/公告号EP2511178A1

    专利类型

  • 公开/公告日2012-10-17

    原文格式PDF

  • 申请/专利权人 DASSAULT AVIATION;

    申请/专利号EP20120163966

  • 发明设计人 CAPETTA THIERRY;

    申请日2012-04-12

  • 分类号B64D1/06;B64D7/08;B64D47/06;

  • 国家 EP

  • 入库时间 2022-08-21 17:11:31

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