首页> 外国专利> Annular airfoil for missiles, airplanes and helicopters, has radial profile, and air is sucked upwards by radial blower and blown radially inwards at annular blade, which has classical wing profile running from inwards to outwards

Annular airfoil for missiles, airplanes and helicopters, has radial profile, and air is sucked upwards by radial blower and blown radially inwards at annular blade, which has classical wing profile running from inwards to outwards

机译:导弹,飞机和直升机的环形翼型具有径向轮廓,径向鼓风机将空气向上吸入,并在环形叶片上向内径向吹送,环形叶片具有从内向外的经典机翼轮廓

摘要

The annular airfoil has a radial profile. Air is aspirated and flown radially on the annular airfoil. The profile of the annular airfoil is designed for optimal tire load. Air is sucked upwards by a radial blower and blown radially inwards at an annular blade, which has a classical wing profile running from inwards to outwards.
机译:环形翼型具有径向轮廓。空气被吸入并径向流到环形翼型上。环形翼型的轮廓设计用于最佳轮胎负载。空气由一台径向鼓风机向上吸入,并在一个环形叶片上径向向内吹,该叶片具有经典的机翼轮廓,从内向外延伸。

著录项

  • 公开/公告号DE102007052288A1

    专利类型

  • 公开/公告日2009-05-20

    原文格式PDF

  • 申请/专利权人 LANGKITSCH RAINER;

    申请/专利号DE20071052288

  • 发明设计人 LANGKITSCH RAINER;

    申请日2007-11-02

  • 分类号B64C29;B64C39/06;

  • 国家 DE

  • 入库时间 2022-08-21 19:09:29

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