An unmanned aerial vehicle (UAV) that provides increased operational flight endurance and efficiency. The UAV includes a power generation system, which includes an internal combustion engine and one or more batteries (batteries). The power generation system is configured to generate power for propulsion of the UAV. The internal combustion engine is configured to power a lift propeller, generating vertical lift of the UAV, and the batteries are configured to power a micro-propeller assembly, propelling the UAV in a forward direction or multiple additional directions.


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    Titel :

    LONG RANGE ENDURANCE AERO PLATFORM SYSTEM


    Beteiligte:
    BECK STEVEN (Autor:in) / CALDWELL DAVID (Autor:in) / HARTNEY CHRISTOPHER (Autor:in) / JEFFERSON JR BERNARD HARRIS (Autor:in) / LANG JEFFREY (Autor:in) / MORALES JOHN (Autor:in) / PANEVSKY MARTIN (Autor:in) / SIRI KASEMSAN (Autor:in) / ULRICH EVAN (Autor:in) / WELLE RICHARD (Autor:in)

    Erscheinungsdatum :

    2021-08-19


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    Long range endurance aero platform system

    BECK STEVEN / CALDWELL DAVID / HARTNEY CHRISTOPHER et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    REQUIREMENTS FOR LONG RANGE -LONG ENDURANCE AIRCRAFT

    Feder, A. / Bogdanovic, J.A. / Wheaton, R.J. | SAE Technical Papers | 1964


    Requirements for long range -- Long endurance aircraft

    Wheaton, R.J. / Bogdanovic, J.A. / Feder, A. | Engineering Index Backfile | 1964


    Aircraft for Long Range and Long Endurance Missions

    Barnett, Lane / Boyles, Richard Q. | SAE Technical Papers | 1964


    Aircraft for long range and long endurance missions

    Boyles, Jr., R.Q. / Barnett, L. | Engineering Index Backfile | 1964