A Cruise Efficient aircraft capable of Vertical or Short Takeoff and Landing aircraft comprising an RLD assembly comprising a concentric gimbaled RLD hub plenum and support assembly, a RLD notatably and lockably coupled with the concentric RLD and a hub plenum and support assembly wherein the RLD comprising a trailing edge and a leading edge substantially symmetric to the trailing edge, as well as an upper and lower surface, each comprising a profile adjustment feature. The aircraft further comprises a RLD control system operably coupled with the RLD assembly configured to selectively control angular velocity of the RLD, selectively lock and selectively unlock the RLD, selectively reorient the RLD in relation to the hub plenum and support assembly, selectively adjust the profile of the leading edge, the trailing edge, and the upper surface, and selectively lock and selectively unlock the RLD in relation to the RLD, wherein the RLD control system is reorientable through the gimbal and whereby the RLD is respectively configurable as an auxiliary transformable main wing for transforming the aircraft.


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    Title :

    CRUISE EFFICIENT VERTICAL AND SHORT TAKE-OFF AND LANDING AIRCRAFT


    Additional title:

    AERONEF A DECOLLAGE ET ATTERRISSAGE VERTICAUX ET COURTS EFFICACE EN VOL DE CROISIERE


    Contributors:

    Publication date :

    2018-08-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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