首页> 外国专利> METHOD FOR ARMING/DISARMING AN AIRCRAFT DOOR EVACUATION SLIDE AND IMPLEMENTATION MECHANISM

METHOD FOR ARMING/DISARMING AN AIRCRAFT DOOR EVACUATION SLIDE AND IMPLEMENTATION MECHANISM

机译:武装/撤离飞机门撤离滑道的方法及实施机制

摘要

The objective of the invention is to replace the rope bar of the door evacuation slide with individual connections. According to a preferred embodiment, the mechanism for arming/disarming an aircraft door evacuation slide (1, 15, 16) includes two releasable connectors (21) disposed to either side of the base of the door and each includes two half connectors (21s, 21i), a so-called upper half connector (21s, 41, 4a, 42) rigidly connected to the door (1) and having an attachment device (33) for attachment to the slide, and a so-called lower half connector (21i) fixed to the cabin floor (6). Each upper half connector (21s) includes a movable inner part controlled by a ring (43) and housed in the corresponding lower half-connector (21i). The mechanism can also include an electric motor coupled to two rods (31), each rod (31) being capable of rotating the control ring (43) of each upper half connector (21s) between two angular positions: an armed position and a disarmed position.
机译:发明内容本发明的目的是用单独的连接代替门疏散滑道的绳索杆。根据一个优选实施例,用于武装/撤离飞机门疏散滑道(1、15、16)的机构包括两个可释放的连接器(21),该两个可释放的连接器(21)设置在门底部的任一侧,每个都包括两个半连接器(21s 21i),刚性连接到门(1)并具有用于连接到滑块的连接装置(33)的所谓的上半部连接器(21s,41、4a,42)和所谓的下半部连接器(21i) 21i)固定在机舱地板(6)上。每个上半部连接器(21s)包括由环(43)控制并容纳在相应的下半部连接器(21i)中的可移动内部。该机构还可以包括联接至两个杆(31)的电动机,每个杆(31)能够使每个上半部连接器(21s)的控制环(43)在两个角度位置(布防位置和撤防位置)之间旋转。位置。

著录项

  • 公开/公告号EP3007976A1

    专利类型

  • 公开/公告日2016-04-20

    原文格式PDF

  • 申请/专利权人 LATECOERE;

    申请/专利号EP20140736655

  • 申请日2014-06-13

  • 分类号B64D25/14;

  • 国家 EP

  • 入库时间 2022-08-21 14:49:35

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