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Electro-hydraulic Brake System of Unmanned Machine Based on High-speed on-off Valve Group
Author(s) -
Yanjun Jiang,
Renming Li,
Yanfeng Jiang,
Yuan Qiu,
Benqin Jing,
Xiaofeng Tang,
Zheng Liu
Publication year - 2025
Publication title -
ieee access
Language(s) - English
Resource type - Magazines
SCImago Journal Rank - 0.587
H-Index - 127
eISSN - 2169-3536
DOI - 10.1109/access.2025.3595441
Subject(s) - aerospace , bioengineering , communication, networking and broadcast technologies , components, circuits, devices and systems , computing and processing , engineered materials, dielectrics and plasmas , engineering profession , fields, waves and electromagnetics , general topics for engineers , geoscience , nuclear engineering , photonics and electrooptics , power, energy and industry applications , robotics and control systems , signal processing and analysis , transportation
To solve the problems of heavy volume, low integration and slow response of the existing industrial unmanned aerial vehicle (UAV) braking system, an aircraft electro-hydrostatic braking system with integrated function and structure, high integration and adaptability to extreme environment was designed and developed based on the high-speed switch valve group. The system uses a single hydraulic pump source and four high-speed on-off valves to control the braking pressure, and a pair of high-speed on-off valves control the braking pressure of all the way, and an overflow valve is added to the circuit to realize the safety redundancy of the hydraulic circuit. The high-speed on-off valve gives the system high precision and high response. Under the condition of target pressure of 6 MPa, the pressure error can be controlled within 0.1 MPa and the response time is less than 0.25s. The differential anti-skid control of two braking pressures can be realized by four switch valve groups, and the steering movement and parking behavior of the aircraft can be completed.

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