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.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT ELECTRICAL NETWORK


    Contributors:

    Publication date :

    2016-11-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



    Aircraft electrical network

    MOXON MATTHEW | European Patent Office | 2019

    Free access

    AIRCRAFT ELECTRICAL NETWORK

    MOXON MATTHEW | European Patent Office | 2017

    Free access

    AIRCRAFT ELECTRICAL NETWORK

    MOXON MATTHEW | European Patent Office | 2020

    Free access

    AIRCRAFT ELECTRICAL NETWORK

    MOXON MATTHEW | European Patent Office | 2019

    Free access

    Aircraft electrical network

    EDWARDS HUW L / SMITH ALEXANDER C / APSLEY JUDITH M et al. | European Patent Office | 2018

    Free access