Abstract
Wheel braking devices is some of the most widely used landing deceleration devices in modern aircraft. Jet pipe pressure servo valves are widely used in large aircraft wheel brake control systems because of their high anti-pollution ability, high sensitivity and fast dynamic response. However, most brake systems suffer vibration phenomena during the braking process. The pressure servo valve is an important part of the hydraulic brake system, and also an important factor affecting the vibration of the system. In order to solve the vibration problem in the brake system this paper present a two-stage brake pressure servo valve design. We place feedback channels at both ends of the main spool to stabilize the output pressure. In addition, modeling, simulation and experimental verifications are carried out. Firstly, the principle and structure of the pressure servo valve are described. An accurate mathematical model of the two-stage brake pressure servo valve and the testing system is established. Then a simulation analysis is carried out. Finally, a two-stage brake pressure servo valve testing experimental platform system is built for experimental verification. The experimental results show that the mathematical model of the two-stage brake pressure servo valve and the test system established in this paper have high accuracy, and the designed servo valve structure can restrain vibrations. The above research results provide a useful theoretical reference for performance optimization, stability analysis and valve body structure improvement of brake pressure servo valves.
Highlights
With the progress of science and technology, large aircraft technology has become an important field leading the development of modern industry, which involves a wide range of technical fields and rich content, attracting a large number of scholars for research
In In view thevibration vibration phenomenon existing in brake aircraft brake servo system, a viewof of the phenomenon existing in aircraft servo system, a two-stage brake pressure servo valve (TSBPSV)
The modeling of the TSBPSV testing system consists of three key parts, namely, the two-stage pressure servo valve dynamic model, the load actuator dynamic model and the two-stage pressure servo valve dynamic model, the load actuator dynamic model and oil return channel dynamic model composed of the oil return pipe and the oil return relief valve
Summary
With the progress of science and technology, large aircraft technology has become an important field leading the development of modern industry, which involves a wide range of technical fields and rich content, attracting a large number of scholars for research. In order to analyze and verify the vibration, it is necessary to establish a high-precision modeling analysis of the servo valve, which is helpful to the development of jet pipe servo valves in the field of high-precision control. According to the principle of the TSBPSV designed in this paper, a matching mathematical model is established, the effect of vibration suppression of the valve is simulated and analyzed, and an experimental platform is built to verify the simulation results.
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