| 摘要 |
FIELD: aeronautical engineering. ^ SUBSTANCE: proposed mechanism consists of command control mechanism, cable run consisting of cable sectors, longitudinally movable part, longitudinal guides and transversely movable base of spherical support. At synchronous and unidirectional rotation of cable sectors, outer cable sets in rotation longitudinal part of mechanism tilting the flying vehicle wing around axis OZ. At synchronous rotation of sectors in opposite directions, inner cable sets in transversal motion base of spherical support tilting the wing around axis OX. During unidirectional but non-synchronous rotation of cable sectors, longitudinally movable part of mechanism and base of spherical support start simultaneous motion over their guides tilting the wing simultaneously around axes OX and OZ. ^ EFFECT: compact assembly. ^ 1 dwg |
