首页> 外国专利> Releasable mounting of docker under pressure to an aircraft.The method of docking mode of a releasable mounting docker under pressure to a side wall of an aircraft assembly and docker under pressure to an aircraft

Releasable mounting of docker under pressure to an aircraft.The method of docking mode of a releasable mounting docker under pressure to a side wall of an aircraft assembly and docker under pressure to an aircraft

机译:在压力下可释放地将码头工人安装到飞机上。可压力地将可释放地安装码头工人到飞机组件侧壁的对接方式和在压力下可将码头工人对飞机的对接方式。

摘要

"Releasable assembly of docker under pressure to an aircraft.The method of docking mode of a releasable mounting docker under pressure to a side wall of an aircraft assembly and docker under pressure to an aircraft.A window assembly with a readily fixu00e1vel aircraft assembly for easy and efficient installation and maintenance of the windows of the aircraft is provided.The aircraft has a side wall has an inner perimeter that defines an opening. An internal frame window is easily fixu00e1vel to the side wall adjacent to the inner perimeter.The inner window frame defines a first opening.A frame of external window is easily fixu00e1vel to internal window frame adjacent to the first opening and the exterior frame of the window defines a second opening.The exterior frame of window and the window frame are coupled to internal releasable mode within the first opening of the inner frame of the window.The assembly of docker under pressure is easily separable from the side wall adjacent to the inner perimeter.
机译:“在压力作用下将码头工人可释放地组装到飞机上。将压力下的可释放安装码头工人到飞机组件的侧壁上并在压力作用下将码头工人对接到飞机上的对接方式。具有易于固定的飞机的窗组件该飞机具有侧壁,该侧壁具有限定开口的内周长;内部框架窗口可容易地固定到邻近于内周长的侧壁上。内窗框定义了一个第一开口。外窗框很容易固定到与该第一开口相邻的内窗框上,窗的外框定义了一个第二开口。窗的外框和窗框在窗口的内部框架的第一个开口内与内部可释放模式耦合。在压力下,泊坞窗的组件易于与相邻的侧壁分离内周。

著录项

  • 公开/公告号BR0204325A

    专利类型

  • 公开/公告日2003-09-16

    原文格式PDF

  • 申请/专利权人 THE BOEING COMPANY;

    申请/专利号BR20020204325

  • 发明设计人 GARY E. JONES;

    申请日2002-10-22

  • 分类号B64C1/14;

  • 国家 BR

  • 入库时间 2022-08-22 00:03:42

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