BALANCE-TYPE AIRCRAFT WITHOUT HORIZONTAL TAIL AND WITH TILTABLE WING Russian patent published in 2006 - IPC B64C3/38

Abstract RU 2277496 C1

FIELD: aeronautical engineering.

SUBSTANCE: proposed aircraft has fuselage, ailerons 3, flap 2, fins 5 with rudders 6, aileron, rudder and wing turn control systems. Aircraft is also provided with pylon on which tiltable wing 1 is mounted on axle 4 for change of angle of attack. Axle 4 is located vertically at distance from aircraft CG 8, thus ensuring longitudinal stabilization of aircraft. Fins 5 and rudders 6 are mounted on tiltable wing tips.

EFFECT: enhanced efficiency of stabilization of control.

3 dwg

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RU 2 277 496 C1

Authors

Gajnutdinov Vladimir Grigor'Evich

Rusakovskij Evgenij Ionovich

Dates

2006-06-10—Published

2004-09-20—Filed