首页> 外国专利> Aircraft e.g. twin-beam twin-engine aircraft, has cockpit mounted rotationally around longeron in order to allow temporary rotation of cockpit toward bottom by voluntary action of pilot in order to retract nose for sight of pilot

Aircraft e.g. twin-beam twin-engine aircraft, has cockpit mounted rotationally around longeron in order to allow temporary rotation of cockpit toward bottom by voluntary action of pilot in order to retract nose for sight of pilot

机译:飞机例如双梁双引擎飞机,具有围绕纵轴旋转安装的座舱,以便在飞行员的自愿作用下允许座舱暂时向底部旋转,以便缩回机头以供飞行员看见

摘要

The aircraft has two wings (3) supported by a traversing longeron (4). A cockpit (5) includes a nose (6) projecting forward, and is separated from a fuselage (1). The cockpit is mounted rotationally around the longeron in order to allow temporary rotation of the cockpit toward bottom by voluntary action of a pilot using actuation units in order to retract the nose for sight of the pilot. A wheel (18) of a landing gear is located at a front part of the cockpit. The wings are equidistance from each other. The cockpit is placed in an intermediate position between the wings. The actuation units are jacks, wheels and endless screws.
机译:该飞机有两个机翼(3),由横梁(4)支撑。驾驶舱(5)包括向前突出的机鼻(6),并与机身(1)分开。驾驶舱围绕纵梁可旋转地安装,以便允许飞行员通过驾驶员使用致动单元的自愿动作暂时向底部旋转,以便缩回机头以看到飞行员。起落架的车轮(18)位于驾驶舱的前部。翅膀彼此等距。驾驶舱位于机翼之间的中间位置。操纵单元是千斤顶,车轮和环形螺钉。

著录项

  • 公开/公告号FR2945787A1

    专利类型

  • 公开/公告日2010-11-26

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号FR20090002467

  • 发明设计人 DURAND YVES;

    申请日2009-05-20

  • 分类号B64C1/28;B64C39/04;

  • 国家 FR

  • 入库时间 2022-08-21 17:45:58

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