An aircraft hydraulic
braking system with an independent anti-skid function, which consists of an automatic
brake switch K, a pressure reducing valve, a hydraulic valve, a first switching valve, a
throttle, a one-way valve, a speed sensor and an anti-skid control box. Automatic
brake system: composed of the first automatic
brake switch K1, the second automatic brake switch K2, the first pressure reducing valve, the second pressure reducing valve, the first hydraulic valve, the second hydraulic valve, the
electrohydraulic servo valve, the first The switching valve, the second switching valve, the
throttle, the one-way valve, the speed sensor and the anti-skid control box form the
automatic braking system of the secondary braking. The invention uses independent or shared anti-skid valves to perform anti-skid control, so that the normal
braking system of the aircraft has
automatic braking capability, improves and expands the operating range of the normal
braking system, provides the driver with the choice of
automatic braking methods, and shortens the landing roll distance by 35%. , which ensures the safety of aircraft
takeoff and landing, improves the
utilization rate of airport runways and equipment utilization, and has obvious economic, social and military benefits.