航天推进技术研究院主办
[1]张维星,刘甲天,陈二锋.双增压单向阀颤振特性分析及防颤策略[J].火箭推进,2022,48(05):46-53.
ZHANG Weixing,LIU Jiatian,CHEN Erfeng.Flutter feature and its prevention strategies of the double pressurization check valves connected in series[J].Journal of Rocket Propulsion,2022,48(05):46-53.
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ZHANG Weixing,LIU Jiatian,CHEN Erfeng.Flutter feature and its prevention strategies of the double pressurization check valves connected in series[J].Journal of Rocket Propulsion,2022,48(05):46-53.
双增压单向阀颤振特性分析及防颤策略
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
48
期数:
2022年05期
页码:
46-53
栏目:
目次
出版日期:
2022-10-25
- Title:
- Flutter feature and its prevention strategies of the double pressurization check valves connected in series
- 文章编号:
- 1672-9374(2022)05-0046-08
- 分类号:
- V434 TH138
- 文献标志码:
- A
- 摘要:
- 针对新一代运载火箭贮箱增压单向阀的泄漏问题,全面分析了单向阀结构组成及工作原理,建立了双增压单向阀串联模式的AMESim模型,并对其阀芯颤振特性进行了研究。结果表明,相比于单个增压单向阀的贮箱增压模式,双单向阀串联后阀芯的颤振现象加剧 而通过增加两单向阀之间的管路容积,可有效缓解单向阀的颤振情况。在此基础上,提出了抑制阀芯颤振的3种策略,并结合数值分析结果和工程实践经验,对3种防颤策略的技术可行性进行了对比研究,所获得的研究成果对于新一代运载火箭贮箱增压系统的可靠性提升具有一定价值。
- Abstract:
- In order to solve the gas leakage problem of the check valves applied in the tank of new generation rockets, structure and working principles of the check valve were analyzed, and the AMESim model of the double pressurization check valves connected in series was created.Based on this numerical model, the flutter feature of the spool was studied, and the results indicate that compared with the single check valve model, the flutter phenomenon will be more severe after two check valves were connected in series.Besides, if the tube capacity between two check valves was increased, the flutter phenomenon will be weakened effectively.At last, three flutter prevention strategies were proposed, and contrastive research on the technical feasibility between different prevention strategies was conducted according to the numerical analysis results and the engineering experience.The study results obtained will be helpful to improve the reliability of the tank pressurization system in new generation rockets.
参考文献/References:
[1] 江海峰,周炎,叶超,等.气动阀门自激振动数值模拟研究概述[J].航天制造技术,2014(2):7-11.
[2] 陶玉静,范才智,田章福,等.两位五通电动气阀动态特性研究[J].推进技术,2006,27(6):542-545.
[3] 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(1):40-48.
DAI J,HUANG M C,YU Y,et al.Simulation on the dynamic response characteristics of solenoid valve[J].Journal of Rocket Propulsion,2007,33(1):40-48.
[4] 王剑中,陈二锋,余武江,等.气动阀门自激振动机理及动态稳定性[J].航空动力学报,2014,29(6):1490-1497.
[5] 余武江,王海洲,陈二锋,等.单向阀三维动态流场稳定性仿真研究[J].火箭推进,2015,41(1):82-89.
YU W J,WANG H Z,CHEN E F,et al.Research on three-dimensional dynamic flow stability of check valve[J].Journal of Rocket Propulsion,2015,41(1):82-89.
[6] 王细波,张连万,刘欣,等.某型气动单向阀颤振特性研究[J].液压气动与密封,2017,37(9):23-25.
[7] 陈二锋,王细波,肖泽宁.某型保险阀非线性稳定性及参数影响特性研究[J].液压气动与密封,2017,37(2):46-49.
[8] HAYASHI S,HAYASE T,KURAHASHI T.Chaos in a hydraulic control valve[J].Journal of Fluids and Structures,1997,11(6):693-716.
[9] MISRA A,BEHDINAN K,CLEGHORN W L.Self-excited vibration of a control valve due to fluid-structure interaction[J].Journal of Fluids and Structures,2002,16(5):649-665.
[10] 叶奇昉,陈江平,陈芝久.制冷系统用两级先导式电磁阀动力学特性的仿真与实验[J].低温工程,2008(4):51-56.
[11] 叶奇昉,严诗杰,陈江平,等.气动先导式电磁阀的自激振动[J].机械工程学报,2010,46(1):115-121.
[12] 叶超,余武江,陈二锋,等.冷氦增压电磁阀动力学稳定性分析[J].液压与气动,2015(6):97-100.
[13] 刘上,刘红军,徐浩海,等.单向阀流路系统自激振荡特性研究[J].火箭推进,2011,37(3):1-5.
LIU S,LIU H J,XU H H,et al.Research of self-oscillation characteristics of check valve flow-path system[J].Journal of Rocket Propulsion,2011,37(3):1-5.
[14] 张生昌,王炤东,邓鸿英,等.气液单向阀弹簧刚度对开启特性的仿真分析[J].液压气动与密封,2014,34(2):19-21.
[15] 陈二锋,丁建春,武园浩,等.气动阀门颤振的局部稳定与全局稳定特性[J].航空动力学报,2018,33(3):663-670.
[16] 陈其法,朱春艳,王文彬,等.基于流固耦合方法的运载火箭安全阀颤振问题研究[J].动力学与控制学报,2019,17(6):528-536.
[17] 史刚,岳兵,尹文辉,等.运载火箭气体单向阀防颤振技术研究[J].航天制造技术,2016(2):30-33.
[18] 李晓雷,俞德孚,孙逢春.机械振动基础[M].2版.北京:北京理工大学出版社,2005.
[19] 付永领,祁晓野.LMS Imagine.Lab AMESim系统建模和仿真参考手册[M].北京:北京航空航天大学出版社,2011.
[20] 休泽尔.液体火箭发动机现代工程设计[M].朱宁昌,译.北京:中国宇航出版社,2004.
备注/Memo
收稿日期:2021-07-15 修回日期:2021-08-31
基金项目:国家联合基金项目(U1937602)
作者简介:张维星(1990—),男,硕士,工程师,研究领域为航天测试发射技术。
更新日期/Last Update:
1900-01-01