| 摘要 |
FIELD: heavier-than-air flying vehicles. SUBSTANCE: vehicle has cabin with aerodynamic rotors whose set includes two cantilever wings articulated on single struts-carriers whose inner ends are rigidly secured on end of drive shaft mounted in immovable tubular cantilevers of cabin. Outer butts of cantilevers are provided with control washers which are movable vertically and horizontally and are engageable with control rods mounted on struts-carriers for longitudinal motion. Each wing is articulated with outer forked end of strut-carrier in front of focus of profile in line of chord. EFFECT: enhanced strength and controllability. 2 cl, 2 dwg |
