The invention relates to a hydraulic ejection
system for an unmanned aerial vehicle. The hydraulic ejection
system comprises a hydraulic driving part, a hydraulic
energy storage part, a hydraulic starting part, a hydraulic buffering part, a
hydraulic brake part, a hydraulic
oil tank and a hydraulic pipeline for being connected between the hydraulic drive part, the hydraulic
energy storage part, the hydraulic starting part, the hydraulic buffering part, the hydraulic braking part and the hydraulic
oil tank, wherein the hydraulic driving part comprises a motor, a
variable capacity pump, hydraulic motors and an electro-hydraulic directional control valve 18; the
energy storage part comprises energy accumulators, an electromagnetic
relief valve and a pressure gage; the hydraulic starting part comprises a starting
hydraulic cylinder and an electro-hydraulic directional control valve 6; the hydraulic
cushioning part comprises a
cushioning hydraulic cylinder and an electro-hydraulic directional control valve 7; the hydraulic braking part comprises a braking
hydraulic cylinder and an electro-hydraulic directional control valve 5; the energy accumulators are connected with the hydraulic motors in series, and besides, a control valve group is connected to the hydraulic pipeline between the energy accumulators and the hydraulic motors in series; besides, a
brake valve group and a prefill valve are arranged on the hydraulic motors; besides, the control valve group is connected with the
brake valve group. The hydraulic ejection
system disclosed by the invention is high in drive force, rapid in
cushioning and braking, stable and reliable in properties, and adaptive to operating requirements for different take-off weights and different take-off speeds of different unmanned aerial vehicles.