The aircraft (10) comprises a fuselage (11) and a rhombohedral wing structure (12) comprising front wings (13, 14) mounted on a front wing-root support (17) and rear wings (15, 16) mounted on a rear wing-root support (18).At least two wings (13, 14) support an engine (24, 26) provided with a propeller (25, 27).The rear end of the fuselage supports an engine (21) provided with a propeller (22).The aircraft comprises means (28 to 35) for tilting said engines, the rotary shaft of each of the propellers being tilted between an orientation parallel to the main axis of the fuselage and an orientation perpendicular to the main axis of the fuselage and to an axis extending through the ends of the front wings.


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    Title :

    AÉRONEF À VOILURE RHOMBOÉDRIQUE À DÉCOLLAGE ET/OU ATTERRISSAGE VERTICAL


    Additional title:

    RHOMBOHEDRAL-WING AIRCRAFT FOR VERTICAL TAKE-OFF AND/OR LANDING
    FLUGZEUG MIT RHOMBOEDRISCHER FLÜGELSTRUKTUR FÜR SENKRECHTES STARTEN UND/ODER LANDEN


    Contributors:

    Publication date :

    2021-05-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    French


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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