A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust in horizontal flight and a delta-wing shaped fuselage disposed along the wing between the nacelles.

    La présente invention concerne un aéronef à décollage et atterrissage verticaux (VTOL). L'aéronef comprend une aile, des nacelles disposées en appui au niveau des extrémités opposées de l'aile, des rotors orientables respectivement fixés sur chacune des nacelles, chaque rotor orientable pouvant pivoter pour générer une portance en vol vertical et une poussée en vol horizontal et un fuselage en forme d'aile delta disposé le long de l'aile, entre les nacelles.


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    Title :

    DELTA FUSELAGE FOR VERTICAL TAKE-OFF AND LANDING (VTOL) AIRCRAFT


    Additional title:

    FUSELAGE DELTA POUR AÉRONEF À DÉCOLLAGE ET ATTERRISSAGE VERTICAUX (VTOL)


    Contributors:

    Publication date :

    2016-09-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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