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AIRCRAFT FUEL TRANSFER PUMP WITH AUXILIARY FUEL LINE SCAVENGE PUMP

机译:辅助燃油管路清除泵的飞机燃油输送泵

摘要

An improved fuel transfer pump (10) is provided for relatively high flow transfer of fuel from one aircraft to another during an inflight refueling procedure, wherein the fuel transfer pump (10) includes a jet-type scavenge pump (12) for evacuating residual fuel from a fuel line (14) or manifold (15). The scavenge pump (12) comprises a venturi element (56) connected along a recirculation conduit (48) through which a small fuel flow is diverted from the high pressure discharge side of the fuel transfer pump (10) for return to the fuel tank (20). The recirculation fuel flow induces a vacuum in a suction throat of the venturi element (56), and this vacuum is coupled by a suction line (58) to evacuate residual fuel from the fuel line (14) or manifold (15) to the fuel tank (20). A flow baffle (62) is mounted along the recirculation conduit (48) downstream from the venturi element (56) to ensure flooding and priming of the scavenge pump (12).
机译:提供了一种改进的燃油输送泵(10),用于在空中加油过程中将较高的燃油从一个飞机流向另一架飞机,其中燃油输送泵(10)包括用于排出残留燃油的喷射式扫气泵(12)。来自燃油管路(14)或歧管(15)。扫气泵(12)包括沿再循环管道(48)连接的文丘里管元件(56),少量燃料流通过该文丘里管元件从燃料输送泵(10)的高压排放侧分流,返回燃料箱( 20)。再循环燃料流在文丘里管元件(56)的吸入喉中产生真空,该真空通过吸入管线(58)耦合,以将残留的燃料从燃料管线(14)或歧管(15)排空到燃料坦克(20)。流动挡板(62)沿着文丘里元件(56)下游的再循环导管(48)安装,以确保扫气泵(12)的注满和注水。

著录项

  • 公开/公告号EP0934449B1

    专利类型

  • 公开/公告日2004-04-28

    原文格式PDF

  • 申请/专利权人 CARTER CO J C;

    申请/专利号EP19970947827

  • 申请日1997-09-23

  • 分类号E03B5/00;F04D9/06;

  • 国家 EP

  • 入库时间 2022-08-21 22:57:52

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