A dual drive hybrid electric power plant to power an aircraft comprises a propulsion assembly, an internal combustion engine having an output shaft configured to drive the propulsion assembly, and an electric motor configured to drive the propulsion assembly and to be selectively coupled to the output shaft. The power plant may be configured such that the electric motor alone drives the propulsion assembly, or such that the internal combustion engine and the electric motor drive the propulsion assembly.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Dual Drive Hybrid Electric Power Plant for Aircraft


    Beteiligte:
    ROBERTS SHANE (Autor:in)

    Erscheinungsdatum :

    12.05.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / F02B INTERNAL-COMBUSTION PISTON ENGINES , Brennkraftmaschinen mit innerer Verbrennung mit Verdrängerwirkung / F02N STARTING OF COMBUSTION ENGINES , Anlassen von Brennkraftmaschinen



    DUAL DRIVE HYBRID ELECTRIC POWER PLANT FOR AIRCRAFT

    ROBERTS SHANE | Europäisches Patentamt | 2022

    Freier Zugriff

    Dual drive hybrid electric power plant for aircraft

    ROBERTS SHANE | Europäisches Patentamt | 2024

    Freier Zugriff

    DUAL ENGINE HYBRID-ELECTRIC AIRCRAFT

    THOMASSIN JEAN / SPIERLING TODD A | Europäisches Patentamt | 2021

    Freier Zugriff

    Dual engine hybrid-electric aircraft

    THOMASSIN JEAN / SPIERLING TODD A | Europäisches Patentamt | 2023

    Freier Zugriff

    DUAL ENGINE HYBRID-ELECTRIC AIRCRAFT

    THOMASSIN JEAN / SPIERLING TODD A | Europäisches Patentamt | 2021

    Freier Zugriff