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AIRCRAFT AERODYNAMIC PROFILE ON OPEN ATTACK, MAT AND AIRCRAFT HAVING SUCH AERODYNAMIC PROFILE

机译:飞机有气动特性时,飞机在空袭,垫子和飞机上的气动特性

摘要

The invention relates to an aerodynamic aircraft profile comprising a profile (1) constituting a leading edge (BA) of the aerodynamic profile. The profile (1) comprises an opening at said leading edge (BA) allowing the entry of air into the thickness of said aerodynamic profile, an air outlet, and shaped guiding means for guiding the air towards the air outlet. The opening at the leading edge makes it possible to introduce air into the thickness of the profile, limiting the aerodynamic turbulence at said leading edge. The invention also relates to a mast carrying an aircraft propulsion unit and having such an aerodynamic profile. The invention finally relates to an aircraft equipped with such a profile.
机译:本发明涉及一种空气动力学飞机轮廓,其包括构成空气动力学轮廓的前缘(BA)的轮廓(1)。型材(1)包括在所述前缘(BA)处的开口,空气出口以及用于将空气朝着空气出口引导的成形的引导装置,所述开口允许空气进入所述空气动力学型材的厚度。前缘处的开口使得可以将空气引入型材的厚度,从而限制了所述前缘处的空气动力学湍流。本发明还涉及一种带有飞机推进装置并具有这种空气动力学轮廓的桅杆。最后,本发明涉及一种具有这种轮廓的飞机。

著录项

  • 公开/公告号FR3044292A1

    专利类型

  • 公开/公告日2017-06-02

    原文格式PDF

  • 申请/专利权人 AIRBUS OPERATIONS;

    申请/专利号FR20150061435

  • 发明设计人 JEROME COLMAGRO;WOLFGANG BROCHARD;

    申请日2015-11-26

  • 分类号B64C3/28;B64C3/14;B64D27/20;B64D29/04;

  • 国家 FR

  • 入库时间 2022-08-21 13:21:17

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