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Aircraft, has central flight controller adapted such that individual auxiliary wings are adjusted in position independent of other auxiliary wings, where position of auxiliary wings is adjusted to each other and to main wings

机译:飞机具有中央飞行控制器,其适于使各个辅助机翼的位置独立于其他辅助机翼而被调节,其中,辅助机翼的位置彼此之间以及与主翼的位置均被调节。

摘要

The aircraft has left and right auxiliary wings (2L, 2R) movably and actively arranged at an outer end of left and right main wings (1L, 1R). Left and right outer auxiliary wings (3L, 3R) are connected to the auxiliary wings in a wing span direction of the main wings. A position of the auxiliary wings is adjusted to each other and to the main wings in degrees of freedom of movement at axes running parallel to an aircraft longitudinal axis (Xf). A central flight controller (F) is adapted such that individual auxiliary wings are adjusted in a position independent of the other auxiliary wings.
机译:飞机在左右主翼(1L,1R)的外端活动地且主动地配置有左右副翼(2L,2R)。左右的外部辅助机翼(3L,3R)在主翼的翼展方向上连接至辅助机翼。辅助机翼的位置在与飞机纵向轴线(Xf)平行的轴线上的运动自由度上相互调整,在主翼上也是如此。中央飞行控制器(F)被适配成使得各个辅助机翼被调节在独立于其他辅助机翼的位置。

著录项

  • 公开/公告号DE102008022452A1

    专利类型

  • 公开/公告日2009-12-03

    原文格式PDF

  • 申请/专利权人 BAUHAUS LUFTFAHRT E.V.;

    申请/专利号DE20081022452

  • 发明设计人 WITTMANN JUERGEN;

    申请日2008-05-08

  • 分类号B64C5/10;B64C5/08;

  • 国家 DE

  • 入库时间 2022-08-21 18:29:00

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