FIELD: transport.
SUBSTANCE: invention relates to landing gears, particularly, to device intended for control the landing gear in lift and direction. Landing gear led comprises pole composed of two crossbars to make pivot point for leg lifting, rotary pipe and sliding rod translating in rotary pipe in turn axis and provided with wheels at its one end. Rotary pipe is arranged inside said pole to turn relative to pivot axis and to extend beyond lift axis relative to position of wheels. Besides, it comprises the drive of leg rotation relative to lift axis at interaction with airframe and, on opposite side, with thrust point of lift located at a distance from lift axis. Note here that thrust point located at rotary pipe on the side opposite the wheels relative to lift axis.
EFFECT: decreased weight and number of hardware components required for landing gear lift and turn.
11 cl, 1 dwg
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