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Aero-engine low pressure pump

机译:航空发动机低压泵

摘要

An aero-engine low pressure pump is provided for supplying fuel at a raised pressure to a high pressure pump. The low pressure pump has a pumping mechanism which raises the pressure of fuel flowing though the mechanism. The low pressure pump further has electrical motor which drives the pumping mechanism. The low pressure pump further has a variable frequency motor drive which supplies electrical power to the electrical motor. The variable frequency motor drive measures the electrical power supplied to the electrical motor. The low pressure pump further has a control unit which compares the measured electrical power to a reference power, and, when the measured electrical power is less than the reference power by a predetermined amount, controls the motor drive to increase the power supplied to the electrical motor thereby increasing the pressure rise produced by the pumping mechanism.
机译:提供一种航空发动机低压泵,用于以升高的压力向高压泵供应燃料。低压泵具有泵送机构,该泵浦机构升高流过该机构的燃料的压力。低压泵还具有驱动泵送机构的电动机。低压泵还具有变频电动机驱动器,该变频电动机驱动器向电动机供应电力。变频电动机驱动器测量提供给电动机的电能。低压泵还具有控制单元,该控制单元将测得的电功率与参考功率进行比较,并且当测得的电功率比参考功率小预定量时,控制电动机驱动器以增加提供给电的功率。从而增加了由泵送机构产生的压力上升。

著录项

  • 公开/公告号US10197062B2

    专利类型

  • 公开/公告日2019-02-05

    原文格式PDF

  • 申请/专利权人 ROLLS-ROYCE PLC;

    申请/专利号US201615256108

  • 发明设计人 DAVID BROOKES;MARTIN K. YATES;

    申请日2016-09-02

  • 分类号F04D15/00;F02C7/236;F02C9/30;F02C7/22;F02K3/06;F04D1/00;F04D13/06;F04D29/22;

  • 国家 US

  • 入库时间 2022-08-21 12:09:10

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