The utility model discloses a pneumatic-electric
hybrid drive
actuator. Comprising a supporting cylinder, a driving spline shaft, a driving motor, a sleeve sealing sleeve, a sleeve, an unlocking direct
drive motor, an unlocking lead screw, an unlocking nut, a disc spring, a lock
piston, an inner cylinder, a lock block, a lock block inner supporting sleeve, a nut, a lead screw, a needle roller
thrust bearing, a disc spring, a sleeve output lug, a bearing supporting sleeve, a first proximity switch, a second proximity switch, an electric connector and a
pipe nozzle. After pneumatic emergency
landing gear extension is completed,
landing gear extension can be completed through the driving motor and the unlocking direct-
drive motor, no part needs to be replaced, and the problems that emergency extension cannot be tested on the ground and parts need to be replaced after emergency extension when the explosion bomb is used for driving the
landing gear to perform emergency extension can be effectively solved; and meanwhile, the problem that the unmanned aerial vehicle needs to be controlled to carry out overload flight to guarantee emergency putting-down and locking of the undercarriage when the undercarriage is driven by gravity and outer spring tension during emergency putting-down of the undercarriage is effectively solved.