首页> 外国专利> Aircraft, has fluid duct system connected to pumping device that is driven, by cabin exhaust air, for production of low pressure for suction of boundary layer though valve, where device is jet pump whose driving jets are generated by air

Aircraft, has fluid duct system connected to pumping device that is driven, by cabin exhaust air, for production of low pressure for suction of boundary layer though valve, where device is jet pump whose driving jets are generated by air

机译:飞机具有连接至泵送装置的流体导管系统,该泵送装置由机舱排气驱动,以产生低压以通过阀吸入边界层,其中该装置是喷射泵,其驱动射流由空气产生

摘要

The aircraft has a fluid duct system (26) for suction of a boundary layer and cleaning of fluid in endangered places of an outer skin of the aircraft. The duct system is connected to a pumping device that is driven, by cabin exhaust air, for production of desired low pressure for suction of the boundary layer though a stop valve (6). The pumping device is a jet pump (3), whose driving jets are generated by the exhaust air.
机译:飞机具有流体管道系统(26),用于抽吸边界层并清洁飞机外蒙皮的濒危位置中的流体。管道系统连接至泵送装置,该泵送装置由机舱排气驱动,以产生所需的低压,以通过截止阀(6)吸入边界层。该泵送装置是喷射泵(3),其驱动喷射是由废气产生的。

著录项

  • 公开/公告号DE102004024057B3

    专利类型

  • 公开/公告日2005-09-15

    原文格式PDF

  • 申请/专利权人 AIRBUS DEUTSCHLAND GMBH;

    申请/专利号DE20041024057

  • 发明设计人 MEISTER JUERGEN;

    申请日2004-05-13

  • 分类号B64C21/00;B64D13/00;B64D47/00;B64D41/00;

  • 国家 DE

  • 入库时间 2022-08-21 22:00:46

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