首页|双滑阀副活门卡滞分析与试验验证

双滑阀副活门卡滞分析与试验验证

扫码查看
针对双滑阀副活门的卡滞现象,应用流固耦合的仿真方法,分析了双滑阀副活门的内部流动和关键零件的受力,总结了不同进油口尺寸、阀套油口结构对阀腔内流场和阀芯径向力的影响规律,获得了活门开启过程中弹簧座倾覆角度的范围.结果表明,增大进油口尺寸和阀套孔数量、减小阀套孔直径和弹簧座的运动自由度,可以降低油液的流速和液压冲击,使阀芯圆周方向的压力分布更加均匀,提高阀芯所受径向力的平衡性.据此对活门结构进行改进,并通过试验进行验证.验证结果表明,将双滑阀副活门的进油口直径改为8 mm、阀套孔数量改为6个、阀套孔直径改为4 mm、取消阀芯与弹簧座的点接触形式后,阀芯在2种工况下至少能够经过600次反复切换,且阀芯表面无任何划痕,改进后的双滑阀副活门完全满足设计要求.
Stuck analysis and test verification of a double slide valve auxiliary valve
To solve the problem of stuck phenomenon for a double slide valve,the internal flow field of the slide valve and the force of key parts were analyzed by the fluid-structure interaction(FSI)simulation.The influence law of different inlet size and valve sleeve oil port structure on the flow field in the valve chamber and the radial force of the spool were summarized,and the range of overturning angle of the spring seat during the spool opening was obtained.The results show that the oil velocity and hydraulic impact can be reduced by increasing the size of the inlet port and the number of holes in the valve sleeve,as well as reducing the diameter of valve sleeve holes and the freedom of movement of the spring seat,so that the circumferential pressure distribution of spool is more uniform,and the balance of radial force of spool can be improved.Based on this,the valve structure was improved and verified through experiments.The experimental results show that after the oil inlet diameter of the double slide valve is changed to 8 mm,the number of valve sleeve holes is changed to 6,the diameter of valve sleeve holes to 4 mm,and canceling the contact form between the spool and the spring seat point,the spool is switched at least 600 times under two working conditions,and there is no scratch on the surface of the valve core.The improved dual slide valve fully meets the design requirements.

double slide valve auxiliary valvesticking of valve corefluid-structure couplinghydraulic systemfault analysis

王艳召、李博海、王洋、邱龙祥

展开 >

中国航发贵州红林航空动力控制科技有限公司,贵阳 550009

双滑阀副活门 阀芯卡滞 流固耦合 液压系统 故障分析

2024

燃气涡轮试验与研究
中国燃气涡轮研究院

燃气涡轮试验与研究

影响因子:0.146
ISSN:1672-2620
年,卷(期):2024.37(6)