Aircraft (1, 1 ') with rear mounted engines (2, 2'), comprising a vertical tail plane (3) and a horizontal tail plane (4), in which the engines (2, 2') are mounted on top of the horizontal tail plane (4), such that the horizontal tail plane (4) comprises an inner fixed part (5) attached to the fuselage (8) of the aircraft (1, 1 '), the inner fixed part (5) comprising an elevator (7), and two outer movable parts (6), each one of the outer movable parts (6) being located at each side end of the horizontal tail plane (4) which is furthest away from the fuselage (8) of the aircraft (1, 1 '), such that both the inner fixed part (5) and the outer movable parts (6) are at least partially subjected to the flow coming from the engines (2, 2') when they are in use.

    L'invention concerne un aéronef (1, 1') doté de moteurs montés à l'arrière (2, 2'), comprenant un plan fixe vertical (3) et un plan fixe horizontal (4), dans lequel les moteurs (2, 2') sont montés sur le dessus du plan fixe horizontal (4) de telle sorte que le plan fixe horizontal (4) comprend une partie fixe interne (5) fixée au fuselage (8) de l'aéronef (1, 1'), la partie fixe interne (5) comprenant une profondeur (7) et deux parties mobiles externes (6), chacune des parties mobiles externes (6) étant située au niveau de chaque extrémité latérale du plan fixe horizontal (4) qui est la plus éloignée du fuselage (8) de l'aéronef (1, 1'), de telle sorte que la partie fixe interne (5) et les parties mobiles externes (6) sont au moins partiellement soumises à l'écoulement provenant des moteurs (2, 2') lorsqu'ils sont utilisés.


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    Title :

    AIRCRAFT WITH REAR MOUNTED ENGINES


    Additional title:

    AÉRONEF DOTÉ DE MOTEURS MONTÉS À L'ARRIÈRE


    Contributors:

    Publication date :

    2017-07-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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