An aircraft includes a fuselage extending along a first x-axis and a wing assembly including a first wing an a second wing. A first power assembly of the aircraft includes a first propulsion element and a first electric motor while a second power assembly includes a second propulsion element and a second electric motor. The aircraft further includes a third power assembly positioned aft of the first power assembly and the second power assembly. The third power assembly includes a third propulsion element and an internal combustion engine.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Hybrid aircraft and landing launch/recovery system


    Beteiligte:

    Erscheinungsdatum :

    20.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    HYBRID AIRCRAFT AND LANDING LAUNCH/RECOVERY SYSTEM

    HARRIS GORDON L / HARRIS STEPHEN L | Europäisches Patentamt | 2021

    Freier Zugriff

    HYBRID AIRCRAFT AND LANDING LAUNCH/RECOVERY SYSTEM

    HARRIS GORDON L / HARRIS STEPHEN L | Europäisches Patentamt | 2023

    Freier Zugriff

    Hybrid aircraft and landing launch/recovery system

    HARRIS GORDON L / HARRIS STEPHEN L | Europäisches Patentamt | 2023

    Freier Zugriff

    Launch and recovery electrical control system of aircraft landing gear

    YANG BINBIN / KANG RUIPING / GUO PENG et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    METHOD FOR LANDING A TETHERED AIRCRAFT AND LAUNCH AND LAND SYSTEM

    PAZ DUART MARCOS | Europäisches Patentamt | 2020

    Freier Zugriff