首页> 外国专利> Boundary layer aspiration device for e.g. propeller, has conduits in which depression is created, when propeller is in rotation, for aspirating boundary layer across porous layer and diverting air towards end of blade tip

Boundary layer aspiration device for e.g. propeller, has conduits in which depression is created, when propeller is in rotation, for aspirating boundary layer across porous layer and diverting air towards end of blade tip

机译:边界层抽吸装置,例如螺旋桨具有一些导管,螺旋桨旋转时会在其中产生凹陷,以抽吸边界层穿过多孔层并使空气流向叶尖末端

摘要

The device has a porous layer (1), conduits (2) and an end opening directed in a thrust axis. Depression is created in the conduits, when a propeller is in rotation, for aspirating a boundary layer across the porous layer and diverting the air towards an end of a blade tip. The air is evacuated by the blade tip and directed backwards to blow vortices of the blade tip.
机译:该装置具有多孔层(1),导管(2)和指向推力轴的端部开口。当螺旋桨旋转时,在导管中产生低压,以抽吸穿过多孔层的边界层并使空气流向叶片尖端的一端。空气由叶尖排出,并向后引导以吹出叶尖的旋涡。

著录项

  • 公开/公告号FR2866931A1

    专利类型

  • 公开/公告日2005-09-02

    原文格式PDF

  • 申请/专利权人 GUTH CLAUDE;

    申请/专利号FR20040002084

  • 发明设计人 GUTH CLAUDE;

    申请日2004-03-01

  • 分类号F15D1/12;

  • 国家 FR

  • 入库时间 2022-08-21 21:58:14

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