B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/26 (2006.01) B64C 5/02 (2006.01)
Patent
CA 2747689
Aircraft horizontal stabilizer surface (8) in which the sweep angle (40) of this surface (8), where this angle (40) is the one formed by the projection of the reference line of points located at 25% of the local chord (19) of the horizontal stabilizer surface (8) on a plane perpendicular to the aircraft plane of symmetry (21), and which also contains this plane to the flight direction of the aircraft with respect to the aircraft plane of symmetry (21), is less than 90 degrees, with this angle (40) being measured in the flight direction of the aircraft. In addition, the structural connection of this horizontal stabilizer surface (8) to the aircraft fuselage (1) is located at a closing frame (13) of this fuselage (1).
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).
Llamas Sandin Raul Carlos
Luque Buzo Miguel
Airbus Operations S.l.
Ridout & Maybee Llp
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