B - Operations – Transporting – 64 – D
Patent
B - Operations, Transporting
64
D
B64D 27/20 (2006.01)
Patent
CA 2603823
The invention concerns an aircraft comprising: a rear vertical tail unit consisting of at least two tail fins (5, 6) forming, with the rear part (7) of said fuselage (4), a channel (8) arranged on the back thereof; and at least one turbine engine (9, 10) arranged on the back of said fuselage (4) so that the gas streams generated by said turbine engine (9, 10) penetrate into said channel (8); and moreover, the main landing gear of said aircraft is arranged integrally beneath the fuselage (in 11); said wings (2, 3) have a slight sweep angle(.phi.); and said wings have a large fineness ratio.
Selon l'invention, l'aéronef comporte : ~ un empennage vertical arrière constitué d'au moins deux dérives (5, 6) et formant, avec la partie arrière (7) dudit fuselage (4), un canal (8) disposé sur le dos de celui-ci ; et ~ au moins un turbomoteur (9, 10) disposé sur le dos dudit fuselage (4) de façon que les flux de gaz engendrés par ledit turbomoteur (9, 10) pénètrent dans ledit canal (8) ; et, de plus, ~ le train d'atterrissage principal dudit aéronef est disposé intégralement sous le fuselage (en 11) ; ~ lesdites ailes (2, 3) présentent une faible flèche (.phi.) ; et ~ lesdites ailes présentent un grand allongement.
Airbus France
Airbus Operations Sas
Robic
LandOfFree
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