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Electric in-line snorkel pump for helicopter tanker and method of operation

机译:直升机加油机的电动直管式浮潜泵及其操作方法

摘要

A pump system for a helicopter tanker includes an axial flow electric pump coupled to a lower end of a snorkel having a generally tubular pump housing extending along a central axis between an open upper end and an opposite open lower end serving as an inlet of the pump. An in-line electric motor is supported within the housing along the axis and has an output drive shaft mounting an impeller. A filter screen basket is mounted on the lower end of the housing to filter water for filtering the incoming water. An electric power cable extends from the motor through a the housing and is shrouded externally by a protective metal cable guard.
机译:一种用于直升机加油机的泵系统,包括连接到通气管下端的轴流电动泵,该通气管具有大体上管状的泵壳,该泵壳沿中心轴线在敞开的上端和相对的敞开的下端之间用作泵的入口。 。串联电动机沿轴线支撑在壳体内,并具有安装有叶轮的输出驱动轴。滤网篮安装在壳体的下端,以过滤水以过滤进入的水。电力电缆从电动机穿过外壳延伸,并由金属保护电缆罩从外部包裹。

著录项

  • 公开/公告号US6209593B1

    专利类型

  • 公开/公告日2001-04-03

    原文格式PDF

  • 申请/专利权人 CARRY MANUFACTURING;

    申请/专利号US20000635326

  • 发明设计人 DELMAR G. NICHOLS SR.;

    申请日2000-08-09

  • 分类号A62C30/20;

  • 国家 US

  • 入库时间 2022-08-22 01:04:44

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