A multi-copter lift body aircraft has a push or pull propeller (26) and a lift body (70) that has a first airfoil shape (71) on a front to rear cross-section and a second airfoil shape (72) on a left to right cross-section. The lift body (70) is made from a top shell and a bottom shell. The lift body (70) has a nose (22) and a tail (25). Multi-copter propellers (60) are attached to the lift body. The multi-copter propellers (60) provide a lift at low speeds and the lift body (70) provides a lift at high speeds. Avionics (68) can be stored in a hollow cavity of the lift body. The avionics (68) may include a control circuit (65), batteries (66), and a radio receiver. The multi-copter has a lift body (70) made from an upper shell (36, 38) and a lower shell (37, 39). The lift body (70) has an optimum attack angle (91) at a cruising speed, and the lift body provides a combined lift mode.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    MULTI-COPTER LIFT BODY AIRCRAFT WITH TAIL PUSHER


    Weitere Titelangaben:

    MULTI-COPTER-LIFT-BODY-FLUGZEUG MIT HECKPUSHER
    AÉRONEF À CORPS HYPERSUSTENTÉ MULTICOPTÈRE COMPORTANT UN POUSSOIR À LA QUEUE


    Beteiligte:
    TU HAOFENG (Autor:in)

    Erscheinungsdatum :

    10.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



    Multi-copter lift body aircraft with tail pusher

    TU HAOFENG | Europäisches Patentamt | 2018

    Freier Zugriff

    MULTI-COPTER LIFT BODY AIRCRAFT WITH TILT ROTORS

    TU HAOFENG | Europäisches Patentamt | 2019

    Freier Zugriff

    MULTI-COPTER LIFT BODY AIRCRAFT WITH TILT ROTORS

    TU HAOFENG | Europäisches Patentamt | 2018

    Freier Zugriff

    COMPOUND MULTI-COPTER AIRCRAFT

    WEEKES TERIK / BELARDO SEAN / COPE CLINT et al. | Europäisches Patentamt | 2019

    Freier Zugriff

    COMPOUND MULTI-COPTER AIRCRAFT

    WEEKES TERIK / BELARDO SEAN / COPE CLINT et al. | Europäisches Patentamt | 2019

    Freier Zugriff