A multi-copter lift body aircraft has a lift body that has a first airfoil shape on a front to rear cross-section. The lift body has a nose and a tail. A multi-copter propeller is attached to the lift body. The multi-copter propellers provide a lift at low speeds, and the lift body provides a lift at high speeds. The multi-copter propeller is mounted to a shaft. A shaft angle is formed on the multi-copter propeller, and the shaft angle provides a forward thrust. The shaft angle is angled upward and forward and the shaft angle is not perpendicular to a chord line of the lift body. Avionics are stored in a hollow cavity of the lift body. The avionics include a control circuit, batteries, and a radio receiver.


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    Title :

    MULTI-COPTER LIFT BODY AIRCRAFT WITH TILT ROTORS


    Contributors:
    TU HAOFENG (author)

    Publication date :

    2019-01-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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