一种控制器双余度的电控刹车阀

The invention relates to the technical field of aircraft braking systems, in particular to a double-redundancy electric control brake valve of a controller, which comprises a brake valve body, a support, an electric mechanism, a pressure sensor module and a controller component, wherein the brake valve body is positioned at the front end of the support, the electric mechanism is arranged in the support, the electric mechanism is connected with the brake valve body and is used for driving the brake valve body to work, the pressure sensor module is arranged on the brake valve body and is used for collecting hydraulic pressure signals of the brake valve, the pressure sensor module is connected with the controller component, the controller component is arranged at the top end of the support, the controller component comprises a power supply information processing plate and two information calculating plates, the controller component is in communication connection with a flight control computer, and the controller component is provided with two information calculating plates, so that under the condition that one information calculating plate fails, the other information calculating plate controls the operation, the stability of products is improved, the failure rate is effectively reduced, and the braking performance and the safety are improved.