首页> 外国专利> Fuselage structure for aircraft or spacecraft has an inner shell system with upper and lower inner shells and a window hinge plate with a window pane device and a grid structure

Fuselage structure for aircraft or spacecraft has an inner shell system with upper and lower inner shells and a window hinge plate with a window pane device and a grid structure

机译:用于飞机或航天器的机身结构具有带有上下内壳的内壳系统以及具有窗玻璃装置和网格结构的窗铰链板

摘要

An upper inner shell in a fuselage inner shell system (20) fits with a clearance in sections from a lower inner shell with a first gap to form a window area. A window hinge plate fits in a window area and has a window pane device, which has a grid structure (10) to retain fuselage forces. An independent claim is also included for a method for a fuselage structure on aircraft or spacecraft.
机译:机身内壳系统(20)中的上内壳与具有第一间隙的下内壳成一定间隔地形成间隙,以形成窗口区域。窗铰链板装配在窗区域中并且具有窗玻璃装置,该窗玻璃装置具有栅格结构(10)以保持机身力。还包括用于飞机或航天器上的机身结构的方法的独立权利要求。

著录项

  • 公开/公告号DE102006025930A1

    专利类型

  • 公开/公告日2007-12-13

    原文格式PDF

  • 申请/专利权人 AIRBUS DEUTSCHLAND GMBH;

    申请/专利号DE20061025930

  • 发明设计人 PAHL GUENTER;

    申请日2006-06-02

  • 分类号B64C1/14;

  • 国家 DE

  • 入库时间 2022-08-21 19:49:56

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