首页> 外国专利> Method for assembling outer shell of aircraft with cab window, involves connecting window frame to outer shell portion in hardened condition for definition of window section, where window section is detached from window frame

Method for assembling outer shell of aircraft with cab window, involves connecting window frame to outer shell portion in hardened condition for definition of window section, where window section is detached from window frame

机译:带有驾驶室窗户的飞机外壳的组装方法,涉及在硬化状态下将窗框连接到外壳部分以限定窗段,其中窗段与窗框分离。

摘要

The method involves connecting a window frame (8) made of a fiber reinforced composite material to an outer shell portion (16) in hardened condition for defining a window section (4) that is detached from the window frame. An outer shell (6) is made of fiber reinforced plastic-based composite material. A supporting frame (26) is inserted into the window section for receiving a window pane package (28) and supported to the window frame, where the window pane package is tensioned by a pressure frame (30). Independent claims are also included for the following: (1) a cabin window for assembling an outer shell of an aircraft with a window frame, comprising a window section (2) an aircraft comprising a body.
机译:该方法包括在硬化条件下将由纤维增强复合材料制成的窗框(8)连接到外壳部分(16),以限定从窗框分离的窗部分(4)。外壳(6)由纤维增强的塑料基复合材料制成。支撑框架(26)被插入到窗部中以接收窗玻璃包装(28)并被支撑到窗框架,其中窗玻璃包装被压力框架(30)张紧。还包括以下方面的独立权利要求:(1)用于将飞机的外壳与窗框组装在一起的机舱窗,其包括窗部分(2)包括主体的飞机。

著录项

  • 公开/公告号DE102010013714A1

    专利类型

  • 公开/公告日2011-10-06

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号DE20101013714

  • 发明设计人 PASPIRGILIS BERND DIPL.-ING.;

    申请日2010-04-02

  • 分类号B64C1/14;

  • 国家 DE

  • 入库时间 2022-08-21 17:47:19

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