Manufacturing Technology 2026, 26(3):372-379 | DOI: 10.21062/mft.2026.032
Research on Flow and Erosion Characteristics of Supercritical Regulating Valve
- Aviation Equipment Manufacturing Industry College, Chengdu Aeronautic Polytechnic University, Chengdu, 610100, China
The regulating valve is a key component of the hydraulic control system. The flow characteristics of the regulating valve are an important parameter for the structural design of the regulating valve. The flow coefficient of the regulating valve directly reflects its flow characteristics, so it is significant to calculate the flow coefficient of the regulating valve accurately. Generally, the flow coefficient is determined by the empirical formula method or experimental method, and the accuracy and efficiency of the calculation are relatively low. In this study, a method for calculating the flow coefficient of the regulating valve com-bined with numerical simulation using CFX is proposed, and the correctness of the method is verified by experiments. Taking the measured flow coefficient as reference, the maximum error is 4.3%. In addition, the cavitation numerical simulation of the regulating valve pipeline system based on CFX is carried out. Under inlet pressures of 1.96 MPa, 2.46 MPa, and 2.96 MPa, the volume fraction of liquid water de-creased to 94.8%, 92.1%, and 88.1%, respectively. At an inlet pressure of 1.96 MPa, the maximum liquid flow exit velocity reached 400 m/s. A prediction method for the erosion amount of the bottom plate is proposed. The predicted erosion amount of the regulating valve reached 10.88 kg after 110 hours of opera-tion. The effectiveness of the proposed method is verified by calculating the actual erosion amount. In this study, the calculation method of flow coefficient and the prediction method of erosion amount can assist in improving the structural design method of regulating valve and its pipeline system, and shorten the design cycle of regulating valve.
Keywords: Regulating valve, Flow coefficient, Cavitation, erosion
Grants and funding:
This research was funded by the Key Natural Science Research Project of Chengdu Aeronautic Polytechnic University in 2024 (ZZX0624087)
Received: November 25, 2025; Revised: May 6, 2026; Accepted: May 12, 2026; Prepublished online: May 14, 2026; Published: June 29, 2026 Show citation
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