AIRCRAFT Russian patent published in 2003 - IPC

FIELD: heavier-than-air flying vehicles. SUBSTANCE: proposed aircraft includes fuselage with tail unit, wing, two fins with rudders and rudder control system. Provision is made for two cable tension control mechanisms located symmetrically relative to longitudinal axis of fuselage. Each mechanism secured in wing cavity has body with two longitudinal slots located one above other, two seats located in body wall, roller with axle and bushes at ends, two springs received by seats of body and by seat of bush of roller axle. Each fin is located symmetrically relative to longitudinal axis of fuselage on lower surface of wing panel section. Control system is independent for each rudder. EFFECT: improved service properties. 8 dwg