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Device for coupling and uncoupling missiles to or from other missiles or carrier aircraft

机译:用于将导弹与其他导弹或运载飞机耦合和解耦的装置

摘要

The invention relates to a mechanical and electrical coupling device for loads, in particular military. Such coupling consists of the combination of hooking means (70), wedging (12) and electrical connection agencies so that the locking of the hooking means leads simultaneously and automatically without the need to do call for adjustment operations, setting in all positions of the load carried with respect to the carrier load as well as their electrical connection. A plurality of loads can thus be made integral with one another with a view to carrying them under an aircraft and then be ejected one by one, starting with the one which is furthest from this aircraft.
机译:本发明涉及一种用于负载,特别是军用的机械和电气的耦合装置。这种联接包括钩挂装置(70),楔形件(12)和电连接机构的组合,因此钩挂装置的锁定同时自动进行,而无需进行任何调整操作,将负载设置在所有位置关于载具负载及其电连接。因此,可以将多个负载彼此整合为一体,以将其承载在飞机下面,然后从距飞机最远的那一个开始逐一弹出。

著录项

  • 公开/公告号EP0021870A1

    专利类型

  • 公开/公告日1981-01-07

    原文格式PDF

  • 申请/专利权人 THOMSON-BRANDT;

    申请/专利号EP19800400672

  • 发明设计人 ROUGET JEAN-PIERRE;ROUSTANT EDMOND;

    申请日1980-05-14

  • 分类号B64D1/06;F41F3/04;

  • 国家 EP

  • 入库时间 2022-08-22 15:39:07

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