航天推进技术研究院主办
[1]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(03):1-5.
LIU Shang,LIU Hong-jun,XU Hao-hai,et al.Research of self-oscillation characteristics of check valve flow-path system[J].Journal of Rocket Propulsion,2011,37(03):1-5.
点击复制
LIU Shang,LIU Hong-jun,XU Hao-hai,et al.Research of self-oscillation characteristics of check valve flow-path system[J].Journal of Rocket Propulsion,2011,37(03):1-5.
单向阀流路系统自激振荡特性研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
37
期数:
2011年03期
页码:
1-5
栏目:
研究与设计
出版日期:
2011-06-15
- Title:
- Research of self-oscillation characteristics of check valve flow-path system
- 文章编号:
- 1672-9374(2011)03-0001-06
- 分类号:
- V433-34
- 文献标志码:
- A
- 摘要:
- 针对液流试验中出现的单向阀系统自激振荡现象,建立了描述该系统动态过程的非线性动力学模型。通过数值计算证实了系统在一定条件下出现极限环,系统是局部稳定,大范围不稳定,计算结果与试验相吻合。分析了此系统产生自激振荡的原因、影响因素及抑制措施。
- Abstract:
- In order to investigate the self-oscillation phenomenon of the check valve system happening in the hydraulic experiments, a nonlinear dynamics model was established to describe the dynamic process of the system. The limit cycle oscillation was emerged under specified conditions through the simulation tests. It is found by the numerical calculation that the system is local stable but unstable in large scale. The simulation results agree well with the experimental ones. The reasons why the sytem produces self-oscillation, the infuencing fctors of self-oscillation and the measures restraining the self-oscillation are analyzed.
相似文献/References:
[1]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(01):82.
YU Wu-jiang WANG Hai-zhou CHEN Er-feng YE Chao ZENG Bin.Research on three-dimensional dynamic flow stability of check valve[J].Journal of Rocket Propulsion,2015,41(03):82.
[2]雷 恒,贾景卫,谢 宁.液氧煤油发动机蒸发器路单向阀结构优化[J].火箭推进,2012,38(01):27.
LEI Heng,JIA Jing-wei,XIE Ning.Structure optimization of check valve in evaporator pipeline of LOX/kerosene engine[J].Journal of Rocket Propulsion,2012,38(03):27.
备注/Memo
收稿日期:2011-02-26;修回日期:2011-04-11
基金项目:国家航天技术支撑项目
作者简介:刘上(1984—),男,博士研究生,研究领域为液体火箭发动机系统
更新日期/Last Update:
1900-01-01