首页> 外国专利> Airplane e.g. civil transport aircraft, has wing mounted movably with respect to fuselage along longitudinal direction parallel to axis of fuselage between front extreme position and rear extreme position of reference point of wing

Airplane e.g. civil transport aircraft, has wing mounted movably with respect to fuselage along longitudinal direction parallel to axis of fuselage between front extreme position and rear extreme position of reference point of wing

机译:飞机,例如民用运输机,其机翼沿平行于机身轴线的纵向方向相对于机身可移动地安装在机翼参考点的前极端位置和后极端位置之间

摘要

The airplane (1) has a wing (3) integrated with a fuselage (2) on a level of a central box. An assembly (4) of tail empennages is integrated with the fuselage. The wing is mounted movably with respect to the fuselage along a longitudinal direction (X) parallel to an axis of the fuselage between a front extreme position and a rear extreme position of a reference point of the wing. A guiding unit is integrated to the central box and supported on parallel beams allowing movement of the wing.
机译:飞机(1)在中央箱体的水平上具有与机身(2)集成的机翼(3)。尾部尾翼的组件(4)与机身集成在一起。机翼沿着平行于机身轴线的纵向方向(X)相对于机身可移动地安装在机翼的参考点的前极端位置和后极端位置之间。导向单元集成到中央箱中,并支撑在平行梁上,以允许机翼移动。

著录项

  • 公开/公告号FR2946013A1

    专利类型

  • 公开/公告日2010-12-03

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号FR20090053577

  • 发明设计人 CAZALS OLIVIER;DRUOT THIERRY;

    申请日2009-05-29

  • 分类号B64C17;B64C3/38;

  • 国家 FR

  • 入库时间 2022-08-21 17:45:55

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