Improved Aircraft horizontal stabilizer surface having a free end and an end by which the horizontal stabilizer surface is connected to an aircraft fuselage. The sweep angle of this surface formed by the projection of the reference line of points located at 25% of the local chord of the horizontal stabilizer surface on a plane perpendicular to the airplane plane of symmetry, is less than 90 degrees, as measured in the flight direction of the aircraft; the horizontal stabilizer surface having an aerodynamic centre aligned with the point at which the stabilizer is connected to the fuselage.

    La présente invention concerne une surface stabilisatrice horizontale (8) d'un aéronef qui est telle que l'angle de flèche (40) de ladite surface (8), ledit angle (40) étant celui qui forme la projection de la ligne de référence de points à 25% de la corde locale (19) de la surface stabilisatrice horizontale (8) sur un plan perpendiculaire au plan de symétrie (21) de l'aéronef, ledit plan contenant également la direction de vol dudit aéronef, par rapport au plan de symétrie (21) de l'aéronef, est inférieur à 90 degrés, ledit angle (40) étant mesuré dans la direction de vol de l'aéronef. De plus, la liaison structurelle de ladite surface stabilisatrice horizontale (8) au fuselage (1) de l'aéronef est réalisée au moyen d'un couple (13) dudit fuselage (1).


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    Title :

    AIRCRAFT HORIZONTAL STABILIZER SURFACE


    Additional title:

    SURFACE STABILISATRICE HORIZONTALE POUR AERONEF


    Contributors:

    Publication date :

    2018-01-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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