Wing-fuselage section of an aircraft

Details Wing-fuselage section of an aircraft Wing-fuselage section of an aircraft

B - Operations, Transporting

64

C

B64C 1/26 (2006.01)

Patent

CA 2681854

A wing-fuselage section of an aircraft, which wing-fuselage section comprises a wing root (7, 8) at which the wing (1) of the aircraft is connected to the fuselage (2), a fuselage region (3) with fuselage frame elements (11-15, 21-25) that extent across the longitudinal direction of the aircraft, and a wing region (5, 6) with spars (16-19, 26-29) that extend in the direction of the wingspan. According to the invention, the spars (16- 19, 26-29) of the wing region (5, 6) and the fuselage frame elements (11-15, 21-25) of the fuselage region (3) form part of an integral assembly (40) that extends at least over a middle part of the wing (1) and the fuselage region (3), including the wing roots (7, 8).

L'invention concerne une section aile-fuselage d'un avion, laquelle section aile-fuselage comprend une emplanture d'aile (7, 8) au niveau de laquelle l'aile (1) de l'avion est reliée au fuselage (2), une région de fuselage (3) avec des éléments de cadre de fuselage (11-15, 21-25) qui s'étendent en travers de la direction longitudinale de l'avion, et une région d'aile (5, 6) avec des longerons (16-19, 26-29) qui s'étendent dans la direction de l'envergure de l'aile. Selon l'invention, les longerons (16-19, 26-29) de la région d'aile (5, 6) et les éléments de cadre de fuselage (11-15, 21-25) de la région de fuselage (3) font partie d'un ensemble d'un seul tenant (40) qui s'étend au moins sur une partie médiane de l'aile (1) et de la région de fuselage (3), comprenant les emplantures d'aile (7, 8).

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