|Table of Contents|

Flutter feature and its prevention strategies of the double pressurization check valves connected in series(PDF)

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]

Issue:
2022年05期
Page:
46-53
Research Field:
目次
Publishing date:

Info

Title:
Flutter feature and its prevention strategies of the double pressurization check valves connected in series
Author(s):
ZHANG Weixing1 LIU Jiatian1 CHEN Erfeng2
(1.Wenchang Aerospace Launch Site, Xichang Sattelite Launch Center,Wenchang 571300, China 2.Beijing Institute of Astronautical Systems Engineering,China Aerospace Science and Technology Corporation, Beijing 100076, China)
Keywords:
double check valves tank pressurization flutter feature AMESim tube capacity flutter prevention strategies
PACS:
V434 TH138
DOI:
-
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.

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.

Memo

Memo:
-
Last Update: 1900-01-01