航天推进技术研究院主办
ZHU Wei,WANG Xin.Measuring process control of liquid rocket engine liquid flow testing system[J].Journal of Rocket Propulsion,2011,37(04):71-75.
液体火箭发动机液流试验系统测量过程控制研究
- Title:
- Measuring process control of liquid rocket engine liquid flow testing system
- 文章编号:
- 1672-9374(2011)04-0071-05
- Keywords:
- liquid flow; testing system; measurement; process control
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 介绍了液流试验系统测量过程控制。从日常液流试验系统测量过程验证及控制方法入手,详细介绍了各种测量验证及控制方法的应用场合及其优缺点。最后给出了目前开展测量控制工作所存在的问题及今后的发展方向。
- Abstract:
- The measuring process control of the liquid rocket engine liquid flow testing system is introduced. Proceeding from daily testing and measuring process control method, the advantages and disadvantages of each measuring verification and control method are elaborated. The problems existing in current measuring process control and development trend of the liquid flow testing system for liquid rocket are pointed out.
参考文献/References:
[1]董双财. 测量系统分析-理论、方法和应用[M]. 北京: 中国计量出版社, 2006.
[2]上海市计量测试技术研究院. 常用测量不确定度评定方法及应用实例[M]. 北京: 中国计量出版社, 2000.
[3]李为柱. 2000版ISO9000族标准统计技术应用教程[M].北京: 企业管理出版社, 2001.
[4]李宗扬. 计量技术基础[M]. 北京: 原子能出版社, 2002.
[5]孙淮清. 流量测量节流装置设计手册[M]. 北京: 化学工业出版社, 2005.
[6]倪育才. 实用测量不确定度评定[M]. 北京: 中国计量出版社, 2010.
[7]蔡武昌. 流量测量方法和仪表的选用[M]. 北京: 化学工业出版社, 2001.
[8]于善奇. 应用统计技术[M]. 北京: 中国标准出版社, 1999.
[9]耿文忠. 新型液体火箭发动机试车台起动试验系统方案设计[J]. 火箭推进, 2008, 34(3): 53-57.
[10]黄强, 吴建军, 刘洪刚, 等. 液体火箭发动机基于神经网络的实时故障检测算法实现[J].国防科学技术大学, 2007, (5): 14-17.
相似文献/References:
[1]赵耀中,郑 然,彭龙涛,等.运载火箭氧自生增压不锈钢管道的安全性研究[J].火箭推进,2015,41(06):105.
ZHAO Yaozhong,ZHENG Ran,PENG Longtao,et al.Study on reliability of stainless steel tube for
self-pressurization oxygen tank of launch vehicle[J].Journal of Rocket Propulsion,2015,41(04):105.
[2]王 珺,胡 鹏,颜 勇.液体火箭发动机泵的POGO气蚀动特性试验研究[J].火箭推进,2012,38(04):26.
WANG Jun,HU Peng,YAN Yong.Experimental investigation of POGO cavitation dynamic characteristic for liquid rocket engine pump[J].Journal of Rocket Propulsion,2012,38(04):26.
[3]朱伟.气动装夹在试验工装中的利用[J].火箭推进,2005,31(04):54.
Zhu Wei.Application of pneumatic equipment in test clamping apparatus[J].Journal of Rocket Propulsion,2005,31(04):54.
[4]侯健,贺宏,陈聪,等.发动机高模试验技术研究[J].火箭推进,2016,42(06):81.
HOU Jian,HE Hong,CHEN Cong,et al.Study on high altitude simulation test technology of engine[J].Journal of Rocket Propulsion,2016,42(04):81.
[5]刘成胜,王晓锋,赵艳丽,等.试验系统夹气对离心泵性能测量的影响分析[J].火箭推进,2018,44(06):75.
LIU Chengsheng,WANG Xiaofeng,ZHAO Yanli,et al.Analysis on influence of gas entrapment of test system on
centrifugal pump performance measuring[J].Journal of Rocket Propulsion,2018,44(04):75.
备注/Memo
收稿日期:2011-04-15;修回日期:2011-04-28
作者简介:朱伟(1978—),男,工程师,研究领域为液体火箭发动机试验技术