Journal of Zhejiang University SCIENCE  A

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Flow analysis of asymmetric clearance and optimization of pressure equalization grooves to mitigate hydraulic spool valve sticking


Author(s):  Zhen-hao LIN, Yu-wei WANG, Zhe-hui MA, Tian-xiao ZHANG, Zhi-jiang JIN, Jin-yuan QIAN

Affiliation(s):  Institute of Advanced Equipment, College of Energy Engineering, Zhejiang University, Hangzhou 310027, China; more

Corresponding email(s):  qianjy@zju.edu.cn

Key Words:  Spool valve; Flow characteristics; Multi-objective optimization; Solid–liquid two-phase flow; Aerospace hydraulic systems; Valve sticking


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Zhen-hao LIN, Yu-wei WANG, Zhe-hui MA, Tian-xiao ZHANG, Zhi-jiang JIN, Jin-yuan QIAN. Flow analysis of asymmetric clearance and optimization of pressure equalization grooves to mitigate hydraulic spool valve sticking[J]. Journal of Zhejiang University Science A,in press.Frontiers of Information Technology & Electronic Engineering,in press.https://doi.org/10.1631/jzus.A2500604

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journal="Journal of Zhejiang University Science A",
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publisher="Zhejiang University Press & Springer",
doi="https://doi.org/10.1631/jzus.A2500604"
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%T Flow analysis of asymmetric clearance and optimization of pressure equalization grooves to mitigate hydraulic spool valve sticking
%A Zhen-hao LIN
%A Yu-wei WANG
%A Zhe-hui MA
%A Tian-xiao ZHANG
%A Zhi-jiang JIN
%A Jin-yuan QIAN
%J Journal of Zhejiang University SCIENCE A
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doi="https://doi.org/10.1631/jzus.A2500604"

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T1 - Flow analysis of asymmetric clearance and optimization of pressure equalization grooves to mitigate hydraulic spool valve sticking
A1 - Zhen-hao LIN
A1 - Yu-wei WANG
A1 - Zhe-hui MA
A1 - Tian-xiao ZHANG
A1 - Zhi-jiang JIN
A1 - Jin-yuan QIAN
J0 - Journal of Zhejiang University Science A
SP - 493
EP - 505
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PB - Zhejiang University Press & Springer
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doi="https://doi.org/10.1631/jzus.A2500604"


Abstract: 
The hydraulic spool valve is a critical control component in aerospace hydraulic systems. However, complex working environments can cause the valve core to become stuck, thus severely restricting the performance of such valves. This in turn can hinder the precise control of hydraulic oil, reduce the stability of the hydraulic system, and lead to serious accidents in aerospace systems. The unbalanced radial force and solid particle intrusion into the fit clearance are the main factors behind this sticking. To better understand these issues, in this study, we simulated the fluid dynamics and particle behavior within the clearance of the valve core and analyzed the effects of inclination angle, clearance size, particle diameter, and pressure equalization groove (PEG) properties. The mechanism behind valve core sticking was revealed, and it was found that the PEG has an inhibitory effect on the unbalanced radial force and particle intrusion. Furthermore, we proposed an optimized structure for a triangular pressure equalization groove with an arc-shaped bottom (Tri-PEG). The structural parameters were determined through multi-objective optimization, with the objectives of minimizing the leakage at the clearance and maximizing the particle volume fraction at the bottom of the Tri-PEG. The optimal parameters were an arc-shaped radius of 0.200 mm, a groove depth of 0.392 mm, and a half groove width of 0.215 mm. Comparing Tri-PEG with a rectangular PEG, the leakage was reduced by 12%, and the particle concentration was increased by 6%. Overall, these findings serve as an important reference for alleviating spool valve sticking.

液压滑阀阀芯均压槽非对称间隙流动分析及防卡滞结构优化

作者:林振浩1,2,王雨薇1,马哲辉1,张天晓1,金志江1,3,钱锦远1
机构:1浙江大学,能源工程学院,特种装备研究所,中国杭州,310027;2阀源智能科技(杭州)有限公司,中国杭州,310058;3浙江大学,温州研究院,中国温州,325036
目的:液压滑阀是航空航天液压系统中的关键控制部件。然而,复杂的工作环境会导致阀芯卡滞,从而限制此类阀门的性能。这会阻碍液压油的精确控制,降低液压系统的稳定性,从而导致航空航天系统发生严重事故。不平衡的径向力和固体颗粒侵入配合间隙是导致这种粘附的主要因素。本文旨在通过分析阀芯间隙内的流体动力学和颗粒行为揭示阀芯卡滞的机理,并提出可有效缓解滑阀卡滞的结构参数。
创新点:1.提出一种弧形底部的三角形均压槽(Tri-PEG)优化结构;2.通过多目标优化确定结构参数,以间隙处的泄漏量最小化和Tri-PEG底部的颗粒体积分数最大化为优化目标。
方法:1.通过数值模拟分析倾斜角度、间隙尺寸、颗粒直径和均压槽(PEG)特性对阀芯间隙内的流体动力学和颗粒行为的影响;2.采用多目标优化方法,以间隙处的泄漏量最小化和Tri-PEG底部的颗粒体积分数最大化为优化目标,确定最优结构参数。
结论:1.径向流体力与倾斜角呈正相关,与配合间隙呈负相关。2.Tri-PEG的最佳参数为0.2 mm的弧形半径、0.392 mm的槽深和0.215 mm的半槽宽;与矩形PEG相比,其泄漏量减少了12%,而颗粒浓度增加了6%。

关键词组:滑阀;流量特性;多目标优化;固液两相流;航空航天液压系统;阀门卡滞

Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article

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On-line Access: 2026-05-26

Received: 2025-11-17

Revision Accepted: 2026-01-07

Crosschecked: 2026-05-26

Cited: 0

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Citations:  Bibtex RefMan EndNote GB/T7714

 ORCID:

Jin-yuan Qian

https://orcid.org/0000-0002-5438-0833

Zhi-jiang Jin

https://orcid.org/0000-0002-8063-709X

Zhen-hao LIN

https://orcid.org/0000-0003-3040-7656

Yu-wei WANG

https://orcid.org/0009-0000-7935-4765

Zhe-hui MA

https://orcid.org/0009-0008-9552-4873

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