The invention belongs to the technical field of
airplane electromechanical control, and discloses an electric dual-redundancy electro-hydrostatic
airplane wheel
brake system which comprises a left
brake oil cup, a right
brake oil cup, a left
electric control brake combination valve, a right
electric control brake combination valve, a left
airplane wheel brake device, a right airplane wheel brake device, a left
wheel speed sensor, a right
wheel speed sensor and a control box for redundancy switching. The left brake oil cup is connected with a left airplane wheel brake device through a left
electric control brake combination valve, the right brake oil cup is connected with a right airplane wheel brake device through a right electric control brake combination valve, and the left electric control brake combination valve and the right electric control brake combination valve are both combinations of
piston structures driven by motors and electromagnetic valves. The left electric control brake combination valve and the right electric control brake combination valve are connected with a fly
pipe computer through
signal lines and are controlled by the fly
pipe computer. The left
wheel speed sensor and the right wheel speed sensor are used for monitoring the rotating speed of an aircraft left wheel and the rotating speed of an aircraft right wheel respectively; the control box for redundancy switching switches the control relation of the right electric control brake combination valve and the left electric control brake combination valve to the left airplane wheel brake device and the right airplane wheel brake device respectively. The device can realize power
telex, adopts pressure closed-
loop control, is high in precision, and has the advantages of relatively high integration level, small size, convenience in installation and maintenance and the like. The dual-redundancy design of an electrical part is adopted, redundancy switching is achieved through independent equipment, the reliability of a
braking system is guaranteed, synchronous skid resistance can be achieved, and
safe operation of an airplane is guaranteed.