A VTOL vehicle includes a forward rotor, an aft rotor and a fuselage, the forward and aft rotor lying in a longitudinal axis of the vehicle, with the fuselage located axially between the forward and aft rotors. The vehicle has an in-flight configuration wherein the forward rotor is tilted downwardly at a negative tilt angle relative to the fuselage and the aft rotor is tilted upwardly at a positive tilt angle relative to the fuselage.


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    Title :

    VTOL VEHICLE WITH COAXIALLY TILTED OR TILTABLE ROTORS


    Additional title:

    VTOL-FAHRZEUG MIT KOAXIAL GENEIGTEN ODER NEIGBAREN ROTOREN
    VÉHICULE VTOL À ROTORS COAXIALEMENT BASCULÉS OU BASCULANTS


    Contributors:

    Publication date :

    2017-09-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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