航天推进技术研究院主办
SHI Qiu-ming,XIE Rong-hua.Design sensitivity analysis and reliability research on sliding pairs of solenoid valve[J].Journal of Rocket Propulsion,2013,39(03):87-92.
电磁阀滑动副的设计参数灵敏度分析与可靠性研究
- Title:
- Design sensitivity analysis and reliability research on sliding pairs of solenoid valve
- 文章编号:
- 1672-9374(2013)03-0072-07
- Keywords:
- solenoid valve; sliding pair; design parameter sensitivity; reliabili
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 分析了电磁阀的组成和功能,给出了电磁阀的4个典型任务剖面,并由此分析对阀门可靠性产生重要影响的功能结构。用设计参数灵敏度分析法研究了导致阀芯-壳体滑动副卡死的直接原因,认为问题的核心在于多余物导致摩擦力大幅度增加。因此消除滑动副的疲劳磨损和粘着磨损是提高可靠性的关键。用质量功能配置方法找出了与滑动副相关的零件和结构,在灵敏度分析的基础上建立了结构要素的设计思路和原则,研究了螺管式电磁阀的滑动副结构对空间推进系统的适用性,并给出了滑动副结构要素的加工方法和对应的工序质量控制点。
- Abstract:
- Based on the analysis of the function and composition of the solenoid valve, four mission phases of the valve were presented, and the functional structures affecting the reliability significantly were discussed. The method of design sensitivity analysis was presented, and the result shows that the clamping of moving parts was caused by the obvious enhancement of friction with debris. To improve the reliability of sliding pairs, the fatigue and scuffing must be eliminated. On the basis of the design sensitivity analysis, the rules of designing a sliding pairs were established. The applicability of solenoid valve sliding parts' structure for space propulsion system was studied. The manufacturing method and corresponding process quality control point of the sliding parts' structure are offered in this paper.
参考文献/References:
[1]ADELMAN H M, HAFTKA R T. Sensitivity analysis of discrete structural systems[J]. AIAA Journal, 1986, 24(5): 823-832.
[2]SMITH D E, SIDDHI V. Generalized approach for incorporating normalization conditions in design sensitivity analysis of eigenvectors[J]. AIAA Journal, 2006, 44(11): 2552-2561.
[3]宋曦, 赵荣珍. 转子-轴承系统固有频率对设计参数的灵敏度[J]. 甘肃工业大学学报, 1999, 25(2): 37-40.
[4]张义民, 闻邦椿, 刘巧伶. 转子-机匣系统碰摩灵敏度研究[J]. 机械设计, 2002, 19(3): 9-10.
[5]LEE T H. Adjoint method for design sensitivity analysis of multiple eigenvalues and associated eigenvectors[J]. AIAA Journal, 2007, 45(8): 1998-2004.
[6]REN YX. Evaluation of the stability derivatives using the sensitivity equations[J]. AIAA Journal, 2008, 46(11): 912-917.
[7]史秋明. 直流电磁铁的动特性研究[J]. 自动化仪表, 2007, 28(5): 20-23.
[8]秦现生. 并行工程的理论与方法[M]. 西安: 西北工业大学出版社, 2008.
[9]BEEK A Van. 现代机械工程设计--全寿命周期性能与可靠性[M]. 刘传军 译. 北京: 清华大学出版社, 2010.
[10]田明, 冯进良, 白素平, 等. 精密机械设计[M]. 北京: 北京大学出版社, 2010.
[11]潘英朋, 高汉平, 刘刚. 磁性双位自锁电磁阀磁路设计与分析[C]//上海航天动力技术研究院. 2009年中国航天第三专业信息网第30届技术交流会论文集. 上海: 上海航天动力技术研究院, 2009: 604-613.
[12]李松晶, 梁慧敏, 刘茂恺, 等. 采用极化电磁机构的节能电磁换向阀[J]. 机床与液压, 1997 (5): 5-6.
[13]瓦伦丁 L 波波夫. 接触力学与摩擦学的原理及应用[M]. 李强, 雒建斌 译. 北京: 清华大学出版社, 2011.
相似文献/References:
[1]郝贵欣,周 吉,张 华.一种电磁阀智能测试系统[J].火箭推进,2013,39(05):82.
HAO Gui-xin,ZHOU Ji,ZHANG Hua.Intelligent testing system for solenoid valve[J].Journal of Rocket Propulsion,2013,39(03):82.
[2]许 闯,尤 罡.电磁阀磁路结构对动作寿命的影响[J].火箭推进,2013,39(05):98.
ZHU Min,ZHANG Hui,LEI Zhen.Application of distributed measurement and control system in liquid rocket engine test[J].Journal of Rocket Propulsion,2013,39(03):98.
[3]王晓罡,陈 健,朱 娟,等.电磁阀薄壁隔磁效果分析与试验研究[J].火箭推进,2012,38(06):24.
WANG Xiao-gang,CHEN Jian,ZHU Juan,et al.Analysis and test for thin-walled magnetism isolating effect of solenoid valve[J].Journal of Rocket Propulsion,2012,38(03):24.
[4]封锡凯,李 伟,李 辉.电磁阀启闭特性非接触测量方法研究[J].火箭推进,2011,37(03):65.
FENG Xi-kai,LI Wei,LI Hui.Study on non-contact measurement techniques of solenoid valve response characteristics[J].Journal of Rocket Propulsion,2011,37(03):65.
[5]袁洪滨,张民庆,孙彦堂.基于AMESim的直动式电磁阀动态仿真研究[J].火箭推进,2011,37(05):30.
YUAN Hong-bin,ZHANG Min-qing,SUN Yan-tang.AMESim-based simulation analysis of dynamic characteristics of direct-acting solenoid valve[J].Journal of Rocket Propulsion,2011,37(03):30.
[6]戴佳,黄敏超,余勇,等.电磁阀动态响应特性仿真研究[J].火箭推进,2007,33(01):40.
Dai Jia,Huang Minchao,Yu Yong,et al.Simulation on the dynamic response characteristics of solenoid valve[J].Journal of Rocket Propulsion,2007,33(03):40.
[7]黄红耀,何斌.电磁阀释放电流出现双波峰的机理分析[J].火箭推进,2007,33(05):50.
Huang Hongyao,He Bin.Mechanism analysis of double-peak release current curve of solenoid valve[J].Journal of Rocket Propulsion,2007,33(03):50.
[8]杨亦婷[],李进贤[],张博斌[].轨姿控推进系统用电磁阀性能仿真研究[J].火箭推进,2016,42(02):19.
YANG Yiting[],LI Jinxian[],ZHANG Bobin[].Simulation research on performance of solenoid valve for orbit and attitude control propulsion system[J].Journal of Rocket Propulsion,2016,42(03):19.
[9]高曼,王志永,李小明.电磁阀泄漏故障分析及改进[J].火箭推进,2018,44(05):43.
GAO Man,WANG Zhiyong,LI Xiaoming.Analysis for leakage fault of solenoid valve and its improvement[J].Journal of Rocket Propulsion,2018,44(03):43.
[10]邹 嘉,刘 飞,朱建国,等.基于阻容元件的电磁阀快响应技术[J].火箭推进,2019,45(04):58.
ZOU Jia,LIU Fei,ZHU Jianguo,et al.Fast-response solenoid valve based on resistance and capacitance[J].Journal of Rocket Propulsion,2019,45(03):58.
备注/Memo
收稿日期:2013-01-25;修回日期:2013-02-26
作者简介:史秋明(1975—),男,高级工程师,研究领域为液体火箭发动机推力室和阀门工艺技术