AIRCRAFT Russian patent published in 2008 - IPC B64C3/40 B64C39/08 

FIELD: aviation.

SUBSTANCE: proposed aircraft has fuselage, wings, engines and landing gear. Fuselage is provided with fairings (2) in its front and rear parts; fairings (2) are also used as stabilizers; fuselage is provided with rudders and axles (5) vertically secured in upper and lower parts of fuselage along its axial line; wings 4 articulated on these axles have plates (7) articulated on their upper and lower sides with jet engine nozzles located in between them. Wings are turned with the aid of connecting rods (8) articulated on axles (9) which are also articulated on wings; other ends of connecting rods are articulated on axles secured on lateral sides of slide block (10) for motion over guides found of fuselage lateral sides. Secured on slide block is axle with connecting rod (13) articulated on it; other end of connecting rod is secured on crank (14) of gear (15) having gear coaxially secured on it and thrown into engagement with gear engaged with gear secured on shaft of electric motor mounted in lower part of fuselage. Gear with crank is thrown into engagement with similar gear (23) provided with the same attachment and mechanical linkage setting the tiltable wings of second raw in motion.

EFFECT: increased speed of aircraft; reduction of noise and consumption of fuel.

3 cl, 3 dwg