Multi-engine aircraft

B - Operations – Transporting – 64 – D

Patent

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Details

B64D 27/20 (2006.01) B64D 27/26 (2006.01)

Patent

CA 2563815

The invention relates to a multi-engine aircraft whose at least two engines (2, 3) are fixed to the fuselage wings symmetrically with respect to the longitudinal vertical plane of symmetry thereof, respectively and the third engine (7) is provided for the tail of the fuselage which comprises tail-planes in the view of said longitudinal plane. The tail-planes (9, 10) define a channel (11) symmetrical with respect to the longitudinal plane of the fuselage and the third engine (7) is disposed on the plane of symmetry of the channel corresponding to the longitudinal plane and mounted on the top part of the fuselage in an elevated manner and before the tail-planes in such a way that output of said third engine is arranged substentially upon the input of the channel (11) defined by said tail-planes.

L'invention concerne un avion multimoteur, dont au moins deux moteurs (2, 3) sont associés aux ailes du fuselage respectivement symétriquement par rapport au plan longitudinal vertical de symétrie de ce dernier et dont un troisième (7) est prévu au niveau de la queue dudit fuselage, qui comporte les empennages arrière, selon ledit plan longitudinal.les empennages arrière (9, 10) définissent un canal (11), symétrique par rapport audit plan longitudinal du fuselage, et le troisième moteur (7) est agencé dans le plan de symétrie dudit canal correspondant audit plan longitudinal et est monté sur la partie supérieure dudit fuselage de façon surélevée et devant les empennages, pour que la sortie de ce troisième moteur se trouve sensiblement à l'entrée du canal (11) défini par lesdits empennages.

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