首页> 外国专利> Cockpit security method for aircraft involves providing bolt retractor to retract locking bolt to door release direction due to pressure difference between opposing sides of aircraft cockpit door

Cockpit security method for aircraft involves providing bolt retractor to retract locking bolt to door release direction due to pressure difference between opposing sides of aircraft cockpit door

机译:飞机驾驶舱安全方法涉及提供螺栓收起器,以由于飞机驾驶舱门的相对侧之间的压力差而将锁定螺栓缩回至门释放方向

摘要

The method involves providing a door (14) in the door frame (16) of the cockpit of an aircraft. A locking bolt (12) is provided in the door to lock the cockpit door. A bolt retractor (10) retracts the locking bolt to a lock release direction due to the presence of a pressure difference of a predefined magnitude between the opposing sides of the cockpit door.
机译:该方法包括在飞机的驾驶舱的门框(16)中提供门(14)。门上装有一个锁定螺栓(12),用于锁定驾驶舱门。由于在驾驶舱门的相对侧之间存在预定大小的压力差,所以螺栓收紧器(10)将锁定螺栓缩回锁定释放方向。

著录项

  • 公开/公告号FR2829791A1

    专利类型

  • 公开/公告日2003-03-21

    原文格式PDF

  • 申请/专利权人 MUL T LOCK SECURITY PRODUCTS LTD;

    申请/专利号FR20020011437

  • 发明设计人 ARTSIELY EYAL;

    申请日2002-09-16

  • 分类号E05B65/00;B64D11/00;B64D25/00;E05B51/00;E05C5/00;

  • 国家 FR

  • 入库时间 2022-08-21 23:37:54

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