An aerial vehicle adapted for vertical takeoff and landing using a set of wing mounted thrust producing elements and a set of tail mounted rotors for takeoff and landing. An aerial vehicle which is adapted to vertical takeoff with the rotors in a rotated, take-off attitude then transitions to a horizontal flight path, with the rotors rotated to a typical horizontal configuration. The aerial vehicle uses different configurations of its wing mounted rotors and propellers to reduce drag in all flight modes.


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    Title :

    IMPACT RESISTANT PROPELLER SYSTEM


    Additional title:

    SCHLAGFESTES PROPELLERSYSTEM
    SYSTÈME DE PROPULSION RÉSISTANT AUX CHOCS


    Contributors:
    BEVIRT JOEBEN (author) / STOLL ALEX (author)

    Publication date :

    2020-11-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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