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Double configuration emergency exit to abandon the aircraft after landing on ground or water

机译:双配置紧急出口,在地面或水降落后放弃飞机

摘要

In order to satisfy the regulations, an emergency exit is proposed which is able to take up two different configurations, according to whether it is used for a land or ditching evacuation from an aircraft. The door of the emergency exit is formed by an upper element (20), able to pivot towards the inside of the cabin (12), and by a lower element (22), able to pivot towards the outside of the cabin. A main locking system (64), accessible from the inside and the outside of the cabin, and normally locked, controls the opening of the upper element (20), then of the lower element (22), during a land evacuation. A secondary locking system (26), normally unlocked, is actuated before ditching, in such a way that the lower element (22) then remains closed when the main locking system (64) is actuated. IMAGE
机译:为了满足规定,提出了一种紧急出口,根据其是用于陆地降落还是从飞机上撤离,该紧急出口可以采用两种不同的配置。紧急出口的门由能够朝机舱(12)的内部枢转的上部元件(20)和能够朝机舱的外部枢转的下部元件(22)形成。主锁定系统(64)可从机舱的内部和外部进入,并且通常被锁定,在陆地疏散期间控制上部元件(20),然后下部元件(22)的打开。在开沟之前,通常被解锁的第二锁定系统(26)被致动,使得当主锁定系统(64)被致动时,下部元件(22)随后保持关闭。 <图像>

著录项

  • 公开/公告号EP0592317B1

    专利类型

  • 公开/公告日1996-09-18

    原文格式PDF

  • 申请/专利权人 AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE;

    申请/专利号EP19930402471

  • 发明设计人 POCCARD JACQUES;

    申请日1993-10-07

  • 分类号B64C1/14;

  • 国家 EP

  • 入库时间 2022-08-22 03:47:37

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