Electrical power system for an aircraft

    公开(公告)号:US09963095B2

    公开(公告)日:2018-05-08

    申请号:US14266940

    申请日:2014-05-01

    CPC classification number: B60R16/03 F01D15/10 H02J1/10 Y02T50/671

    Abstract: An electrical power system for an aircraft having electrical loads and at least one jet engine with a high pressure spool and a low pressure spool, the electrical power system includes a first electrical machine driven by a first pressure spool and outputting a first voltage, a second electrical machine driven by a second pressure spool and outputting a second voltage, and an electrical distribution bus receiving the first and second voltages and supplying the voltages to the loads.

    ELECTRICAL POWER SYSTEM FOR AN AIRCRAFT
    3.
    发明申请
    ELECTRICAL POWER SYSTEM FOR AN AIRCRAFT 有权
    用于飞机的电力系统

    公开(公告)号:US20150123463A1

    公开(公告)日:2015-05-07

    申请号:US14266940

    申请日:2014-05-01

    CPC classification number: B60R16/03 F01D15/10 H02J1/10 Y02T50/671

    Abstract: An electrical power system for an aircraft having electrical loads and at least one jet engine with a high pressure spool and a low pressure spool, the electrical power system includes a first electrical machine driven by a first pressure spool and outputting a first voltage, a second electrical machine driven by a second pressure spool and outputting a second voltage, and an electrical distribution bus receiving the first and second voltages and supplying the voltages to the loads.

    Abstract translation: 一种用于具有电负载的飞行器的电力系统和具有高压阀芯和低压阀芯的至少一个喷气发动机,所述电力系统包括由第一压力阀驱动并输出第一电压的第一电机, 由第二压力阀驱动并输出第二电压的电机,以及接收第一和第二电压并将电压提供给负载的配电总线。

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