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某航空液电阀主密封结构密封性能分析及优化
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Analysis and Optimization of the Sealing Performance of the Main Sealing Structure of an Aviation Hydraulic Valve
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    摘要:

    针对液电阀阀芯处密封结构,采用组合式密封结构的设计思路,通过压缩波簧提供预紧力和补偿力。建立密封结构数值模型,对液电阀动密封面的接触应力和转动摩擦力矩进行分析。根据不同的影响因素模拟动密封面间的接触应力分布以及峰值接触应力的变化情况,通过施加流体压力,研究各因素对液电阀转动摩擦力矩的影响规律。设计正交试验并进行直观分析和方差分析,确定最优密封结构。结果显示:优化后主密封副间接触应力增大,转动摩擦力矩减小,有效提升了主密封结构的密封性能。

    Abstract:

    For the sealing structure at the spool of the hydraulic valve,the design idea of the combined sealing structure was adopted,and the pre-tightening force and compensation force were provided by the compression wave spring.A numerical model of the sealing structure was established,and the contact stress and rotational friction torque of the dynamic sealing surface of the hydraulic valve were analyzed.According to different influencing factors,the contact stress distribution between the dynamic sealing surfaces and the change of the peak contact stress were simulated.And by applying fluid pressure,the influence of each factor on the rotational friction torque of the hydraulic valve was studied.Orthogonal experiments were designed and intuitive analysis and variance analysis were carried out to determine the optimal sealing structure parameters.The results show that after optimization,the contact stress between the main seal pair increases and the rotational friction torque decreases,which effectively improves the sealing performance of the main seal structure.

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王东川.某航空液电阀主密封结构密封性能分析及优化[J].机床与液压,2023,51(16):184-193.
WANG Dongchuan. Analysis and Optimization of the Sealing Performance of the Main Sealing Structure of an Aviation Hydraulic Valve[J]. Machine Tool & Hydraulics,2023,51(16):184-193

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  • 在线发布日期: 2023-09-13
  • 出版日期: 2023-08-28