首页> 外国专利> Cabin-door airplane assembly e.g. civil aviation, has autonomous passenger cabin arranged from rear part toward front part and from bottom side toward top side in fuselage of airplane part constituting complete airplane at time of flight

Cabin-door airplane assembly e.g. civil aviation, has autonomous passenger cabin arranged from rear part toward front part and from bottom side toward top side in fuselage of airplane part constituting complete airplane at time of flight

机译:机舱门飞机组件民航,飞行时在构成完整飞机的飞机机身中具有从后部到前部以及从底侧到顶侧布置的自主客舱

摘要

The assembly has an autonomous passenger cabin arranged from a rear part toward a front part and from a bottom side toward a top side in a fuselage of an airplane part constituting a complete airplane at a time of flight. The front part of the cabin is slightly reduced by thickness of an upper fuselage (4) for permitting fitting of the cabin. A wedging type locking system assures connection between components. Two parallel fuselages are joined together by a wing beam to receive the cabin and a control cabin.
机译:该组件具有在飞行时从构成完整飞机的飞机部分的机身的后部朝向前部并且从底侧朝向顶侧布置的自主客舱。机舱的前部因允许安装机舱的上机身(4)的厚度而略有减小。楔入式锁定系统可确保组件之间的连接。两个平行的机身通过翼梁连接在一起,以容纳机舱和控制舱。

著录项

  • 公开/公告号FR2943618A1

    专利类型

  • 公开/公告日2010-10-01

    原文格式PDF

  • 申请/专利权人 DESTOUCHES MICHEL;

    申请/专利号FR20090001393

  • 发明设计人 DESTOUCHES MICHEL;

    申请日2009-03-25

  • 分类号B64C1/22;B64C1/32;

  • 国家 FR

  • 入库时间 2022-08-21 18:26:37

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