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航空液压管路连接式单向阀不同结构形式泄露机理研究

唐杰 钟安凯

重庆理工大学学报2025,Vol.39Issue(1):148-154,7.
重庆理工大学学报2025,Vol.39Issue(1):148-154,7.DOI:10.3969/j.issn.1674-8425(z).2025.01.019

航空液压管路连接式单向阀不同结构形式泄露机理研究

Research on leakage mechanism of different structural forms of aviation hydraulic pipeline connected check valve

唐杰 1钟安凯1

作者信息

  • 1. 中国民航大学 航空工程学院,天津 300300
  • 折叠

摘要

Abstract

In the aircraft hydraulic system,the check valve is an indispensable hydraulic component crucial for ensuring circuit stability and reliable performance.The spool,as the central element of the check valve,is pivotal in determining the valve's performance and reliability.One of its critical impacts is leakage,which significantly undermines the operational efficiency and flow characteristics of the check valve.We explore various contact configurations and cone hole angles concerning the spool and the body of spring-loaded check valves.To thoroughly analyze these factors,a three-dimensional model of the valve body is built along with a mathematical model focusing on leakage.Through simulations and comparisons based on the mathematical model,the optimal structural design for minimizing leakage is made.The results of these simulations are corroborated through fluid-solid coupling techniques.This comprehensive approach helps to determine the optimal spool cone angle and the most suitable spool end face contact form,thereby ensuring enhanced performance and reliability of the check valve in applications.

关键词

单向阀/流体仿真/正交试验法/流固耦合

Key words

check valve/fluid simulation/orthogonal experimental/fluid-solid coupling

分类

机械制造

引用本文复制引用

唐杰,钟安凯..航空液压管路连接式单向阀不同结构形式泄露机理研究[J].重庆理工大学学报,2025,39(1):148-154,7.

基金项目

国家自然科学基金民航联合重点项目(U2233212) (U2233212)

中国民航大学实验创新基金项目(2023YJSKC01019) (2023YJSKC01019)

重庆理工大学学报

OA北大核心

1674-8425

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