An aircraft comprising a hybrid electric aircraft propulsion system. The system comprises a first sub-assembly having a first electric propulsor assembly and a first thermal propulsor assembly, the first thermal propulsor assembly having a first thermal engine, a first generator and a first rotating propulsor, the first electric propulsor assembly attached to the aircraft at a first location and the first thermal propulsor assembly attached to the aircraft at a second location. The system also comprises a second sub-assembly having a second electric propulsor assembly and a second thermal propulsor assembly, the second thermal propulsor assembly having a second thermal engine, a second generator and a second rotating propulsor, the second electric propulsor assembly attached to the aircraft at a third location and the second thermal propulsor assembly attached to the aircraft at a fourth location.


    Access

    Download


    Export, share and cite



    Title :

    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM


    Contributors:

    Publication date :

    2020-03-12


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen



    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    RAZAK AHMED M Y / HUSBAND STEPHEN M | European Patent Office | 2020

    Free access

    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    BACIC MARKO | European Patent Office | 2022

    Free access

    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    LATULIPE ERIC / FREER RICHARD | European Patent Office | 2020

    Free access

    HYBRID ELECTRIC AIRCRAFT PROPULSION SYSTEM

    LATULIPE ERIC / FREER RICHARD | European Patent Office | 2020

    Free access

    HYBRID-ELECTRIC PROPULSION SYSTEM FOR AIRCRAFT

    SRIDHAR ADIBHATLA / ROBERT CHARLES HON / MICHAEL THOMAS GANSLER | European Patent Office | 2019

    Free access