首页> 外国专利> HIGH-LIFT SYSTEM FOR AN AIRCRAFT, METHOD FOR DISPLACING A LIFT FLAP, AND AIRCRAFT HAVING A HIGH-LIFT SYSTEM

HIGH-LIFT SYSTEM FOR AN AIRCRAFT, METHOD FOR DISPLACING A LIFT FLAP, AND AIRCRAFT HAVING A HIGH-LIFT SYSTEM

机译:飞机的高升降系统,移位襟翼的方法以及具有高升降系统的飞机

摘要

A high lift system is provided for an aircraft. The high lift system includes, but is not limited to a lift flap arranged on a wing and coupled to the wing so as to be movable relative to the wing, between a retracted position and at least one extended position. In the retracted position the lift flap rests against the wing, and in an extended position forms an air gap to the wing. The lift flap directed towards its trailing edge comprises at least one region of variable curvature, which region in an extended position of the lift flap extends towards the wing.
机译:为飞机提供了高升力系统。高升力系统包括但不限于布置在机翼上并连接至机翼以便相对于机翼可在缩回位置和至少一个伸出位置之间移动的举升翼片。在缩回位置,升力襟翼靠在机翼上,而在伸出位置,机翼与机翼形成气隙。指向其后缘的升力襟翼包括至少一个可变曲率的区域,该区域在升力襟翼的延伸位置朝机翼延伸。

著录项

  • 公开/公告号EP2509859B1

    专利类型

  • 公开/公告日2014-05-21

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号EP20100784812

  • 发明设计人 SCHRÖDER KARSTEN;

    申请日2010-12-02

  • 分类号B64C9/24;

  • 国家 EP

  • 入库时间 2022-08-21 15:49:15

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