首页> 外国专利> SINGLE SLOTTED FLAP WITH SLIDING DEFLECTOR FLAP AND LOWERABLE SPOILER

SINGLE SLOTTED FLAP WITH SLIDING DEFLECTOR FLAP AND LOWERABLE SPOILER

机译:单槽襟翼,带导流板襟翼和可降低的扰流板

摘要

The device has a high lift device (2) and spoiler devices (3, 4), where the high lift device is movably fastened at a wing unit (1) and is controlled by an onboard computer. The spoiler devices are movably fastened at the wing unit and/or at the high lift device. The spoiler devices are concealed in a recess and are designed such that size of gap between the wing unit and the high lift device is adjusted. An independent claim is also included for a method for adjusting lift characteristics of an airplane.
机译:该装置具有高升力装置(2)和扰流器装置(3、4),其中高升力装置可移动地固定在机翼单元(1)上,并由车载计算机控制。扰流板装置可移动地固定在机翼单元和/或高升程装置上。扰流板装置隐藏在凹槽中,并设计成可调节机翼单元和高升程装置之间的间隙大小。还包括用于调节飞机的升力特性的方法的独立权利要求。

著录项

  • 公开/公告号EP1868887B1

    专利类型

  • 公开/公告日2011-01-19

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号EP20060724150

  • 发明设计人 BENDER KLAUS;BOETTGER OLE;

    申请日2006-04-07

  • 分类号B64C9/14;

  • 国家 EP

  • 入库时间 2022-08-21 17:58:43

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