Automatic detection method for hydraulic pressure boosting time and pressure reducing time of airplane brake system

The automatic detection method for the hydraulic pressure boosting time and the hydraulic pressure reducing time of the airplane braking system is characterized in that when an airplane is subjected to BIT maintenance, the braking system automatically measures the hydraulic pressure boosting time and the hydraulic pressure reducing time and then sends a detection result to a comprehensive management computer; and when the hydraulic pressure boosting time and the hydraulic pressure reducing time exceed normal technical index requirements, fault warning is carried out. According to the method, the detection errors of the hydraulic pressure boosting time and the pressure reducing time of the aircraft brake system are reduced, the measurement consistency of the hydraulic pressure boosting time and the pressure reducing time of the aircraft brake system is improved, the detection process is simplified, human factor interference is avoided, the measurement is accurate, and the consistency is high. 一种飞机刹车系统液压升压时间和降压