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该文介绍了某型飞机防滑刹车系统的工作原理和故障模式,并重点对电液伺服阀和刹车控制盒的工作特点进行了论述,分析了导致故障的原因。在此基础上,得出了有益的结论,并提出相应的建议和改进措施。
This paper introduces the working principle and failure mode of an anti-skid braking system for a certain type of aircraft. The working characteristics of the electro-hydraulic servo valve and brake control box are emphatically discussed. The causes of the fault are analyzed. On this basis, draw useful conclusions, and put forward corresponding suggestions and improvement measures.