Hybrid Power System for an Aircraft
    32.
    发明申请

    公开(公告)号:US20170275009A1

    公开(公告)日:2017-09-28

    申请号:US15077178

    申请日:2016-03-22

    发明人: Hao Huang

    IPC分类号: B64D27/24 B64D27/10

    摘要: Systems and methods for distributing in an aircraft are provided. More particularly, in one embodiment, a system can include one or more gas turbine engines configured to provide propulsion and electrical power to an aircraft. The system can further include one or more electrical engines configured to provide propulsion for the aircraft. The system can include one or more first electrical power systems configured to provide power to the one or more electrical engines for one or more electrical power propulsion loads for the aircraft. The system can further include one or more second electrical power systems configured to provide power for one or more non-propulsion electrical power loads of the aircraft.

    POWER GENERATION SYSTEM
    38.
    发明申请

    公开(公告)号:US20190257211A1

    公开(公告)日:2019-08-22

    申请号:US15902430

    申请日:2018-02-22

    摘要: A power generation system includes an electric generator mechanically driven by a variable speed kinetic source, a first power conversion system connected with an output of the electric generator, and a second power conversion system connected with the output of the electric generator, wherein the electric generator and power conversion systems are adapted to convert the output of the electric generator to a predetermined direct current (DC) voltage.

    Method and assembly of an electric machine

    公开(公告)号:US10381900B2

    公开(公告)日:2019-08-13

    申请号:US15468879

    申请日:2017-03-24

    摘要: An electric machine assembly having a main machine stator core having at least one stator post, a set of stator windings wound about the at least one stator post and having a first end and an opposing second end, a coolant inlet housing defining an inlet passage, a coolant outlet housing defining an outlet passage, proximate to the coolant inlet housing, and wherein the coolant inlet passage and the coolant outlet passage define a coolant circuit configured to receive a supply of coolant to remove heat generated in the set of stator windings.

    METHOD AND ASSEMBLY OF AN ELECTRIC MACHINE
    40.
    发明申请

    公开(公告)号:US20180278125A1

    公开(公告)日:2018-09-27

    申请号:US15468849

    申请日:2017-03-24

    IPC分类号: H02K7/20 H02K9/197

    摘要: A method and assembly of a dry cavity oil cooled electric machine includes a housing, a shaft configured to operably couple with a source of rotational force and rotate about a rotational axis, and an exciter rotor and a permanent magnet generator rotor carried by the shaft, wherein the exciter rotor and the permanent magnet generator rotor rotate relative to the housing, which provides such a construction of dry cavity generators that have high efficiency and high power density.