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Fluid-mechanically effective surface of a moving in a fluid device, in particular an aircraft, in particular wing of an aircraft

机译:在流体装置,特别是飞机,特别是飞机机翼中运动的流体力学有效表面

摘要

A fluid dynamically effective surface of a device moving in a fluid, especially a lifting surface of a flying machine, has an elastic axis extending in the span direction of the surface, and an adjustable control surface. The lifting surface is elastically deformable in a bending direction and/or in a torsion direction about the elastic axis, due to and dependent on the adjustment of the control surface, while changing the induced fluid dynamic drag. A control and/or regulating arrangement is provided for adjusting the control surface in the sense of minimizing the induced fluid dynamic drag of the lifting surface.
机译:在流体中运动的装置的流体动力学有效表面,特别是飞行器的提升表面,具有在该表面的跨度方向上延伸的弹性轴和可调节的控制表面。由于并且依赖于控制面的调节,提升面可在弯曲方向和/或绕弹性轴的扭转方向上弹性变形,同时改变引起的流体动力阻力。提供一种控制和/或调节装置,用于从最小化提升面的感应流体动态阻力的意义上调节控制面。

著录项

  • 公开/公告号DE10302514B4

    专利类型

  • 公开/公告日2008-12-18

    原文格式PDF

  • 申请/专利权人 EADS DEUTSCHLAND GMBH;

    申请/专利号DE20031002514

  • 发明设计人

    申请日2003-01-23

  • 分类号B64C3/10;B64C3/38;B64C5/08;B64C3/42;

  • 国家 DE

  • 入库时间 2022-08-21 19:10:01

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