The invention relates to the field of supersonic inlets of aircrafts, in particular to an anti-surge structure for a supersonic inlet. The anti-surge structure comprises the inlet and an anti-surge
actuator mechanism, a vent port is arranged nearby the exit position of the inlet, and the anti-surge
actuator mechanism is located beside the vent port in the inlet and can close the vent port. The anti-surge
actuator mechanism comprises an actuator cylinder base body, an actuator
piston, a stop pin, a compression spring, a blind pin, a socket and a cover plate. A
piston cylinder is formed in the actuator cylinder base body, the space between the socket and the actuator
piston is filled with
gunpowder, the cover plate is installed at one end of the actuator piston, a stop pin hole is formed in the side face of the
piston cylinder, the stop pin is pressed on the side face of the actuator piston through the blind pin and the compression spring, and the socket is linked with an
ignition control signal. The anti-surge structure solves the surge problem of the inlet, overflow resistance of the inlet is reduced, an extra lift effect is provided for an aircraft, no
projectile exists in the vent port, other parts on the aircraft cannot be threatened, the structure is compact and simple, and influence on performance of the inlet is small.