首页> 外国专利> DEVICE FOR REDUCING AERODYNAMIC DISTURBANCES IN THE WAKE OF AN AERODYNAMIC BLOW PROFILE WITH VARIABLE DISTRIBUTION TO EXTRADOS AND INTRADOS

DEVICE FOR REDUCING AERODYNAMIC DISTURBANCES IN THE WAKE OF AN AERODYNAMIC BLOW PROFILE WITH VARIABLE DISTRIBUTION TO EXTRADOS AND INTRADOS

机译:减少气动冲击波轮廓中的气动扰动的装置

摘要

The invention relates to a device for reducing aerodynamic disturbances in the wake of an aerodynamic profile. The device comprises a first nozzle (51) of air ejection disposed on the extrados (EX) of the profile and a second nozzle (52) of air ejection disposed on the intrados (IN) of the profile. A first blowing chamber (41) is fluidly bonded to the first nozzle (51) and a second blowing chamber (42) is fluidly bonded to the second nozzle (52). Air supply means are configured so as to be able to vary the distribution of air between said first blowing chamber (41) and second blowing chamber (42). The distribution between the first and second nozzles (51,52) of the blown air can thus be adapted according to the use situation of the profile, for example according to the flight phase of an aircraft equipped with such a profile. The invention also relates to an aerodynamic profile, a mast supporting an aircraft propulsion assembly comprising such an aerodynamic profile, and an aircraft.
机译:本发明涉及一种用于减少空气动力学轮廓后的空气动力学干扰的装置。该装置包括设置在轮廓的外凸(EX)上的空气的第一喷嘴(51)和设置在轮廓的内凸(IN)上的空气的第二喷嘴(52)。第一吹风室(41)流体结合到第一喷嘴(51),第二吹风室(42)流体结合到第二喷嘴(52)。空气供应装置构造成能够改变在所述第一吹风室(41)和第二吹风室(42)之间的空气分配。因此,吹气的第一和第二喷嘴(51,52)之间的分布可以根据轮廓的使用情况,例如根据配备有该轮廓的飞机的飞行阶段来调整。本发明还涉及一种空气动力学轮廓,支撑包括这种空气动力学轮廓的飞机推进组件的桅杆以及飞机。

著录项

  • 公开/公告号FR3050781A1

    专利类型

  • 公开/公告日2017-11-03

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS;

    申请/专利号FR20160053720

  • 发明设计人 JEROME COLMAGRO;

    申请日2016-04-27

  • 分类号F15D1/12;B64C21/08;

  • 国家 FR

  • 入库时间 2022-08-21 13:21:07

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