Improved aerobatic aircraft

Details Improved aerobatic aircraft Improved aerobatic aircraft

B - Operations, Transporting

64

D

B64D 33/00 (2006.01) B64C 39/04 (2006.01) B64D 27/08 (2006.01)

Patent

CA 2398903

An improved aerobatic aircraft design having a first engine (18) located in the nose portion (14) of the fuselage (12) and a second engine (22) located in the tail portion (16) of the fuselage (12). The thrust components of both the first (18) and second (22) engines are coaxial along the long axis (70) of the fuselage (12). Both engines can individually provide sufficient power for the aircraft to takeoff, maintain altitude, and/or land.

Cet avion de voltige perfectionné est caractérisé en ce qu'il comprend un premier moteur (18) placé dans la portion avant (14) du fuselage (12), et un second moteur (22) placé dans la portion arrière (16) du fuselage (12). Les composants de poussée de ces deux moteurs (18, 22) sont montés de manière coaxiale le long de l'axe long (70) du fuselage (12), ces deux moteurs pouvant fournir une puissance suffisante à l'avion pour que celui-ci puisse décoller, conserver son altitude et/ou atterrir.

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