首页> 外国专利> Aircraft part e.g. strut fairing, for holding e.g. heat exchanger, has air inlet arranged on wall of part to locally form line of leading edge of part, where air inlet has radius equal to curvature radius of leading edge

Aircraft part e.g. strut fairing, for holding e.g. heat exchanger, has air inlet arranged on wall of part to locally form line of leading edge of part, where air inlet has radius equal to curvature radius of leading edge

机译:飞机零件撑杆整流罩,用于例如热交换器,在零件壁上布置有进气口,以局部形成零件前缘线,其中进气口的半径等于前缘的曲率半径

摘要

The part (100) has a cylindrical shaped air inlet (102) such as vertical open cylinder, and an air transmitting conduit (107 for transmitting airflow from the exterior of the part into an internal volume of the part. The air inlet is arranged on a wall (116) of the part to locally form a line of a leading edge of the part. The longitudinal axis of the air inlet is parallel to the line of the leading edge of the part. The air inlet has a radius equal to the curvature radius of the leading edge. The air inlet is provided with a cone shaped air passage jet pipe.
机译:零件(100)具有圆筒形的进气口(102),例如垂直开口的圆柱体;以及空气传输管道(107),用于将气流从零件的外部传输到零件的内部空间中。零件的壁(116)以局部地形成零件的前缘的线,进气口的纵向轴线平行于零件的前缘的线,进气口的半径等于进气口设有圆锥形的空气通道喷射管。

著录项

  • 公开/公告号FR2905672A1

    专利类型

  • 公开/公告日2008-03-14

    原文格式PDF

  • 申请/专利权人 AIRBUS FRANCE SOCIETE ANONYME;

    申请/专利号FR20060053716

  • 发明设计人 STEVENS THOMAS;HORMIERE ARNAUD;

    申请日2006-09-13

  • 分类号B64C7;

  • 国家 FR

  • 入库时间 2022-08-21 19:47:09

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