Lifting-type aeroplane fuselage

Details Lifting-type aeroplane fuselage Lifting-type aeroplane fuselage

B - Operations, Transporting

64

C

B64C 1/00 (2006.01) B64C 5/02 (2006.01)

Patent

CA 2596429

The invention relates to an aeroplane having a lifting-type fuselage which comprises a wing provided with engines mounted on the hands thereof and whose width is substantially larger than the height thereof and the front section gradually transforms, in the plane view, from the narrow nose part into a large main section, wherein the tail assembly is provided with two stabilisers which are remote along the fuselage width away from the aeroplane vertical symmetry plane, are placed at an angle with respect thereto and are provided with a control surfaces. Each stabiliser is provided with an all-movable arrow- type rudder which forms a T-shaped fin and whose axis of rotation is situated on the stabiliser on the rudder plane. The stabiliser construction planes cross each other on the aeroplane symmetry plane on the main longitudinal axis of the aeroplane or bellow said axis.

Cette invention concerne un avion à fuselage porteur comprenant une aile comportant des moteurs disposés sur les plans alaires de l'aile, un fuselage dont la largeur est substantiellement supérieure à sa hauteur et dont la partie avant dans le plan passe progressivement d'une partie nez étroite à une partie principale plus large, et un empennage comportant deux stabilisateurs qui s'écartent, sur la largeur du fuselage, du plan de symétrie vertical longitudinal de l'avion, qui forment un angle avec celui-ci et qui comprennent des gouvernes. Chacun des stabilisateurs comprend un gouvernail de direction en forme de flèche entièrement mobile formant un empennage en forme de T et présentant un axe de rotation situé sur un stabilisateur dans le plan du gouvernail de direction. Les plans de construction des stabilisateurs se croisent dans le plan de symétrie de l'avion sur l'axe longitudinal principal de l'avion ou en dessous de cet axe.

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