| 摘要 |
FIELD: aviation. SUBSTANCE: proposed mechanism is provided with command rods, longitudinally movable base, immovable guides, toothed sector, transversal tooth rack, main lever with spherical support and wing hinge, as well as rods transmitting control moment from control mechanism to wing. At synchronous and unidirectional motion of command rods, wing turns around axis OZ. At synchronous motion of command rod in different directions, wing turns around axis OX. At simultaneous longitudinal and opposite direction of motion of command rods, wing performs simultaneous turn around axes OX and OZ. EFFECT: enhanced aerodynamic efficiency of flying vehicle. 3 cl, 1 dwg |
