Anti-skid braking system of carrier-based aircraft

The utility model relates to the field of airplane braking systems, in particular to an anti-skid braking system of a carrier-based airplane, which is characterized in that a braking instruction sensor is connected with a braking pedal and is used for acquiring a braking instruction, and an anti-skid function closing signal input interface of an anti-skid braking control box is connected with a power supply through an anti-skid function closing switch; an unlocking signal output end of the anti-skid brake control box is connected with a control end of the electromagnetic hydraulic lock; a servo valve current control signal output end of the anti-skid brake control box is connected with a control end of the electro-hydraulic pressure servo valve; oil return ports of the electromagnetic hydraulic lock and the electro-hydraulic pressure servo valve are communicated with the oil tank, and an oil inlet of the electromagnetic hydraulic lock is communicated with a hydraulic source; a working oil port of the electrom