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Process and device for accelerating the destruction of at least two vortices in the wake of a moving body, particularly an aircraft

机译:用于在移动物体,特别是飞机后加速加速至少两个涡流破坏的方法和装置

摘要

A device for accelerating the destruction of contra-rotating vortices formed at the rear of wings of a moving body by the merging of at least two co-rotating eddies includes, on each of the wings, at least one perturbator which is positioned in the vicinity of the area of creation of one of the co-rotating eddies associated with the wing. Each of the perturbators generates a periodic perturbation of the flow, which has a wavelength capable of exciting at least one of the instability modes of the corresponding eddy in such a way as to increase the core of the contra-rotating vortex which is created from this eddy, in such a way that the diameter of the core becomes greater than a predetermined proportion of the inter-vortex distance.
机译:通过合并至少两个共同旋转的涡流来加速破坏在移动物体的机翼后部形成的反向旋涡的装置,在每个机翼上均包括至少一个扰动器,该扰动器位于附近与机翼相关的同向旋转涡旋之一的产生面积的示意图。每个扰动器都会产生周期性的扰动,该扰动的波长能够激发相应涡流的至少一种不稳定性模式,从而增加由此产生的反向旋转涡旋的核心涡流,以使核的直径大于涡旋距离的预定比例。

著录项

  • 公开/公告号US6719246B2

    专利类型

  • 公开/公告日2004-04-13

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE;

    申请/专利号US20020080407

  • 申请日2002-02-25

  • 分类号B64C13/80;

  • 国家 US

  • 入库时间 2022-08-21 23:14:55

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