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 bi-directional 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 :

    2025-06-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



    ARCHITECTURE FOR AN ELECTRIC POWER GENERATOR FOR AVIATION

    VANNEST JEREMIAH / GAO LIJUN / ZHANG JULIA et al. | European Patent Office | 2023

    Free access

    AVIATION INTEGRATED ELECTRIC POWER PLANT

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

    Free access

    Aviation fuel-electric hybrid power system

    OUYANG XING | European Patent Office | 2024

    Free access

    The Aviation Weather Products Generator

    Carmichael, B. | British Library Conference Proceedings | 1993


    Nuclear power aviation electric propulsion system for long-endurance aircraft and aviation aircraft

    CHENG KUNLIN / LI JIAHUI / QIN JIANG et al. | European Patent Office | 2024

    Free access