In one embodiment, a tiltrotor aircraft (100, 200, 300, 400, 500) may comprise a fuselage (102, 202, 302, 402, 502); a biplane wing (120, 220, 320, 420, 520, 530) coupled to the fuselage (102, 202, 302, 402, 502), wherein the biplane wing (120, 220, 320, 420, 520, 530) comprises an upper wing structure (121a-b, 221a-b, 231a-b, 241a-b, 251a-b, 321, 331, 341, 421a-b) and a lower wing structure (122a-b, 222a-b, 232a-b, 242a-b, 252a-b, 322, 332, 342, 422a-b); a plurality of tiltrotors (110a-b, 210a-b, 410a-b) coupled to the biplane wing (120, 220, 320, 420, 520, 530); and at least one engine to power the plurality of tiltrotors (110a-b, 210a-b, 410a-b).


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    Title :

    BIPLANE TILTROTOR AIRCRAFT


    Additional title:

    DOPPELDECKER-KIPPROTORFLUGZEUG
    AÉRONEF À ROTORS BASCULANTS BIPLAN


    Contributors:

    Publication date :

    2020-12-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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