航天推进技术研究院主办
[1]郝贵欣,张 华,董 飞.表面张力贮箱泡破点盲测技术研究[J].火箭推进,2012,38(05):59-64.
HAO Gui-xin,ZHANG Hua,DONG Fei.Blind test technology for bubble break point of surface tension tank[J].Journal of Rocket Propulsion,2012,38(05):59-64.
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HAO Gui-xin,ZHANG Hua,DONG Fei.Blind test technology for bubble break point of surface tension tank[J].Journal of Rocket Propulsion,2012,38(05):59-64.
表面张力贮箱泡破点盲测技术研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
38
期数:
2012年05期
页码:
59-64
栏目:
工艺与材料
出版日期:
2012-10-15
- Title:
- Blind test technology for bubble break point of surface tension tank
- 文章编号:
- 1672-9374(2012)05-0059-06
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 通过对表面张力贮箱结构、泡破点测试难点分析，提出了采用微压闭环控制技术解决测试过程管理装置内腔压力维持准平衡状态难题的技术途径，研制的贮箱泡破点盲测系统具有自动控制、自动判读及测试精度高等特点，经试验验证该技术满足贮箱泡破点盲测要求，已在型号研制中得到应用。
- Abstract:
- A technical method to adopt the mini-pressure closed-loop control technology to maintain quasi-equilibrium state of internal cavity pressure of management device during the test was proposed by the analysis of surface tension tank structure and bubble break point tests difficulties. The developed blind test system for surface tension tank bubble break point has the characteristics of automatic control, automatic interpretation and high precision, which satisfies blind test requirements. The technology passed test verification and has been applied to tank production.
参考文献/References:
[1] JAEKLE D E, Jr. Propellant management device conceptual design and analysis， AIAA-97-2811[R]. USA: AIAA, 1997.
[2] 陈志坚, 孟庆平, 李建. 表面张力贮箱推进剂管理装置流阻的计算[J]. 上海航天, 2001 (5): 23-32.
[3] 李治, 沈赤兵, 周进. 通道式表面张力贮箱通道的计算和确定[J]. 火箭推进, 2003, 24(3): 244-246.
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[6] 盛敬超. 液压流体力学[M]. 北京: 机械工业出版社, 1980.
[7] 李庆扬, 关治, 白峰衫. 数值计算原理[M]. 北京: 清华大学出版社, 2000.
[8] 王顺晃, 舒迪前. 智能控制系统及其应用[M]. 北京: 机械工业出版社, 2005.
[9] 刘君华. 现代检测技术与测试系统设计[M]. 西安: 西安交通大学出版社, 1999.
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备注/Memo
收稿日期：2012-03-08；修回日期：2012-05-28
基金项目：中国航天科技集团公司支撑项目（2008JY03)
作者简介：郝贵欣（1977—），男，工程师，研究领域为非标准设备的开发、设计、研制
更新日期/Last Update:
1900-01-01