A system, apparatus, and/or method for an aircraft that provides a novel independent-speed variable-frequency generator for aviation power generation. The generator architecture utilizes a 2-stage generator architecture with a wound rotor PM exciter (PME) that provides excitation to the rotor of a generator. A rotating bidirectional AC/DC/AC electric power converter connects the rotor windings of the exciter and the generator.


    Access

    Download


    Export, share and cite



    Title :

    ARCHITECTURE FOR AN ELECTRIC POWER GENERATOR FOR AVIATION


    Contributors:
    VANNEST JEREMIAH (author) / GAO LIJUN (author) / ZHANG JULIA (author) / LIU SHENGYI (author)

    Publication date :

    2023-07-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



    AVIATION INTEGRATED ELECTRIC POWER PLANT

    KALITKA VLADISLAV SERGEEVICH / SAMOJLENKO SERGEJ VLADIMIROVICH / KORNEEV VYACHESLAV VIKTOROVICH et al. | European Patent Office | 2022

    Free access

    The Aviation Weather Products Generator

    Carmichael, B. | British Library Conference Proceedings | 1993


    Electric energy conversion circuit of aviation electric propulsion power system

    LI MING / HU ZHIQIANG / WANG SHAOBO et al. | European Patent Office | 2021

    Free access

    System and method for aviation electric power production

    DELGADO ADON JR / BUCHHOLZ TODD JAMES / MATHIAS CHRISTOPHER DALE | European Patent Office | 2015

    Free access

    Electric vehicle power generator

    CHEN GUANGZHI | European Patent Office | 2021

    Free access