A turboelectric vehicle may include a fuselage and a wing coupled to the fuselage. A wing propulsor may be coupled to the wing. A rear propulsor may be positioned at a rear portion of the fuselage and may be electrically coupled to the wing propulsor. The rear propulsor may be configured to receive power extracted from the wing propulsor.


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    Titel :

    Turboelectric Aircraft with Aft Propulsion


    Beteiligte:
    WELSTEAD JASON R (Autor:in) / FELDER JAMES L (Autor:in)

    Erscheinungsdatum :

    10.05.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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