首页> 外国专利> Propulsive unit for aircraft, has muffler, and compressed air reservoir that allows input of compressed air on impact surface via small holes pierced on cylinder and that produces one strike of compressed air per second from water hammers

Propulsive unit for aircraft, has muffler, and compressed air reservoir that allows input of compressed air on impact surface via small holes pierced on cylinder and that produces one strike of compressed air per second from water hammers

机译:飞机推进装置,具有消音器和压缩空气储存器,该压缩空气储存器允许通过气缸上的小孔将压缩空气输入到冲击面上,并每秒从水锤中产生一击压缩空气

摘要

The unit has a compressed air impact surface (b), an opening or closing valve (1) for striking the compressed air on the surface, a muffler, and a compressed air reservoir (7) around the valve. The reservoir allows an input of compressed air on the surface via small holes pierced on a cylinder and produces 1 strike of compressed air per second from water hammers.
机译:该单元具有压缩空气冲击表面(b),用于将压缩空气撞击到该表面上的打开或关闭阀(1),消音器以及围绕该阀的压缩空气储存器(7)。储气罐允许通过气缸上的小孔将压缩空气输入地面,并每秒从水锤中产生1次冲击。

著录项

  • 公开/公告号FR2883840A1

    专利类型

  • 公开/公告日2006-10-06

    原文格式PDF

  • 申请/专利权人 GIL NOEL;

    申请/专利号FR20050003257

  • 发明设计人 GIL NOEL;

    申请日2005-03-31

  • 分类号B64D27/02;

  • 国家 FR

  • 入库时间 2022-08-21 21:17:11

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