Aircraft electrical network
    1.
    发明授权

    公开(公告)号:US10131441B2

    公开(公告)日:2018-11-20

    申请号:US15136074

    申请日:2016-04-22

    Abstract: An electrical network for an aircraft. The aircraft includes at least one variable pitch propulsor. The electrical network includes a wound field synchronous AC electrical generator having a wound rotor driven by an internal combustion engine. The network further includes a voltage regulator configured to regulate output voltage of the electrical generator by regulating rotor winding magnetic field strength, and a synchronous AC drive motor coupled to a respective variable pitch propulsor and provided with power from the output of the electrical generator.

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