
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 @article{title="Flow analysis of asymmetric clearance and optimization of pressure equalization grooves to mitigate hydraulic spool valve sticking", %0 Journal Article TY - JOUR
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: Darkslateblue:Affiliate; Royal Blue:Author; Turquoise:Article
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CLC number: On-line Access: 2026-05-26 Received: 2025-11-17 Revision Accepted: 2026-01-07 Crosschecked: 2026-05-26 Cited: 0 Clicked: 928 Citations: Bibtex RefMan EndNote GB/T7714 https://orcid.org/0000-0002-5438-0833 https://orcid.org/0000-0002-8063-709X https://orcid.org/0000-0003-3040-7656 Journal of Zhejiang University-SCIENCE, 38 Zheda Road, Hangzhou
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