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Publishing Language: Chinese

Dynamic flow characteristics of digital hydraulic circuit based on high speed solenoid valve

Xiaoming CHEN1,2,3( )Yuchuan ZHU2Cheng QIN1Yangmin LI3Yuan FANG1
Aviation Industry Corporation of China Xi’an Aircraft Design Institute,Xi’an 710089,China
College of Mechanical and Electrical Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China
Faculty of Engineering,Hong Kong Polytechnic University,Hong Kong 999077,China
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Abstract

High-speed solenoid valves are the key control element of digital hydraulic circuits, and their dynamic properties directly affect the circuit's flow performance. To improve the computational accuracy of the flow characteristics in digital hydraulic circuits, a flow calculation model incorporating a controllable duty cycle correction module is proposed in this article. The accuracy of the proposed model was validated using measured flow data within the linear duty cycle region. Experimental results demonstrate that, compared to the ideal switch model without delay, the dynamic flow characteristics model with actual switching delay enables the maximum and average relative error of the instantaneous flow to decrease by 20.3%, 9.3% and the maximum average error of the steady-state flow decreased by 73%, significantly improving computational accuracy. The average output flow rate of the hydraulic circuit at the operating frequency of f = 100 Hz typically increases by 40% of the rated flow in comparison to that at f = 50 Hz when the effective opening time tse is between 2 ms and 7.43 ms. It is confirmed that fluid inertance has a significant impact on the delivery flow of digital hydraulic circuits.

CLC number: TH137 Document code: A Article ID: 1001-5965(2026)08-2836-09

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Journal of Beijing University of Aeronautics and Astronautics
Pages 2836-2844

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Cite this article:
CHEN X, ZHU Y, QIN C, et al. Dynamic flow characteristics of digital hydraulic circuit based on high speed solenoid valve. Journal of Beijing University of Aeronautics and Astronautics, 2026, 52(8): 2836-2844. https://doi.org/10.13700/j.bh.1001-5965.2025.0332

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Received: 28 May 2025
Published: 28 September 2025
© Journal of Beijing University of Aeronautics and Astronautics