首页> 外国专利> FLOW BODY, HIGH-LIFT FLAP OR MAIN WING OR FIN OF AN AIRCRAFT, AS WELL AS A STRUCTURE COMPONENT HAVING SUCH A FLOW BODY

FLOW BODY, HIGH-LIFT FLAP OR MAIN WING OR FIN OF AN AIRCRAFT, AS WELL AS A STRUCTURE COMPONENT HAVING SUCH A FLOW BODY

机译:流动体,飞机的高升襟翼或主翼或鳍,以及具有这种流动体的结构部件

摘要

An aerodynamic body with an aerodynamic body surface that creates a contoured surface for a fluid to stream around, with a device to influence the flow of the fluid streaming around the aerodynamic surface. The flow-influencing device includes a passage to link the fluid streaming around the aerodynamic surface with an actuator space of an aspirating and purging device situated in the aerodynamic body, and an indentation that is situated next to the passage, which is formed by a recessed section of the aerodynamic surface on a flow-influencing region within the contoured surface of the aerodynamic surface, so that a boundary wall is configured as part of the recessed surface lying opposite the indentation. The aspirating and purging device can generate a swirl in the flow of the fluid streaming around the aerodynamic surface, the rotational axis of which is directed along the assumed aerodynamic body chord direction.
机译:一种具有空气动力学主体表面的空气动力学主体,该空气动力学主体表面形成了使流体围绕其流动的轮廓表面,并且具有影响围绕该空气动力学表面流动的流体的流动的装置。所述流量影响装置包括:通道,其将围绕所述空气动力学表面流动的流体与位于所述空气动力学本体中的抽吸和吹扫装置的致动器空间相连接;以及凹口,所述凹口位于所述通道旁边,所述凹口由凹口形成。空气动力学表面的轮廓在空气动力学表面的轮廓表面内的流动影响区域上的横截面,使得边界壁被构造为凹入表面的与凹口相对的一部分。抽吸和吹扫装置可以在围绕气动表面流动的流体的流动中产生涡旋,该涡旋的旋转轴线沿假定的气动体弦方向指向。

著录项

  • 公开/公告号EP2473404B1

    专利类型

  • 公开/公告日2017-04-05

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS GMBH;

    申请/专利号EP20100750068

  • 发明设计人 RIST ULRICH;KNOLL ANDREAS;

    申请日2010-09-02

  • 分类号B64C21/02;B64C21/08;

  • 国家 EP

  • 入库时间 2022-08-21 14:06:29

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