首页> 外国专利> DEVICE FOR REDUCING AERODYNAMIC DISTURBANCES IN THE WAKE OF AN AERODYNAMIC PROFILE BY VARIABLE-DISTRIBUTION BLOWING ON THE TOP SIDE AND THE UNDERSIDE

DEVICE FOR REDUCING AERODYNAMIC DISTURBANCES IN THE WAKE OF AN AERODYNAMIC PROFILE BY VARIABLE-DISTRIBUTION BLOWING ON THE TOP SIDE AND THE UNDERSIDE

机译:通过在顶侧和底侧吹动可变分布来减少空气动力学轮廓中的空气动力学扰动的装置

摘要

A device for reducing aerodynamic disturbances in the wake of an aerodynamic profile. The device comprises a first air ejection nozzle arranged on the top side of the profile and a second air ejection nozzle arranged on the underside of the profile. A first blowing chamber is fluidically connected to the first nozzle and a second blowing chamber is fluidically connected to the second nozzle. Air supply means are configured to vary the distribution of air between said first blowing chamber and second blowing chamber. The distribution of the blown air can thus be adapted depending on the situation in which the profile is used, for example depending on the flight phase of an aircraft equipped with such a profile. Also, an aerodynamic profile, a pylon supporting a propulsion assembly for an aircraft comprising such an aerodynamic profile, and an aircraft.
机译:一种用于减少空气动力学轮廓中的空气动力学干扰的装置。该装置包括布置在轮廓的顶侧上的第一空气喷嘴和布置在轮廓的底侧上的第二空气喷嘴。第一吹风室流体连接到第一喷嘴,第二吹风室流体连接到第二喷嘴。空气供应装置构造成改变在所述第一吹风室和第二吹风室之间的空气分布。因此,吹气的分布可以根据使用轮廓的情况来调整,例如根据配备有该轮廓的飞机的飞行阶段来调整。而且,空气动力学轮廓,支撑用于包括这种空气动力学轮廓的飞机的推进组件的吊架以及飞机。

著录项

  • 公开/公告号US2017313412A1

    专利类型

  • 公开/公告日2017-11-02

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS (S.A.S);

    申请/专利号US201715499230

  • 发明设计人 JEROME COLMAGRO;

    申请日2017-04-27

  • 分类号B64C21/04;B64D27/26;B64D29/04;B64D27/14;B64D27;

  • 国家 US

  • 入库时间 2022-08-21 13:50:31

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