航天推进技术研究院主办
[1]马 键,童 飞,陈祖奎.贮箱容积偏差及测量精度分析[J].火箭推进,2013,39(01):41-45.
MA Jian,TONG Fei,CHEN Zu-kui.Analysis on deviation and measuring precision of tank volume[J].Journal of Rocket Propulsion,2013,39(01):41-45.
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MA Jian,TONG Fei,CHEN Zu-kui.Analysis on deviation and measuring precision of tank volume[J].Journal of Rocket Propulsion,2013,39(01):41-45.
贮箱容积偏差及测量精度分析
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
39
期数:
2013年01期
页码:
41-45
栏目:
研究与设计
出版日期:
2013-02-28
- Title:
- Analysis on deviation and measuring precision of tank volume
- Keywords:
- tank; volume measurement; deviation analysis
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 贮箱一般采用称重法进行容积测量，但测量值与理论设计值偏差较大。分析了贮箱在生产制造、液压试验、介质加注、称重、容积计算和变形等环节出现偏差的原因。通过贮箱计算实例分析了各环节偏差大小，提出了减小偏差的对策，并对贮箱容积测量提出了改进方案。
- Abstract:
- The weighting method is usually adopted to measure the volume of tanks, but its measured value has a great deviation from the theoretical value. The reasons that the deviation occurs in the process of manufacture, hydraulics test, medium filling, weighting, volume calculation and distortion are analyzed. The deviation value of each link is also analyzed by means of an example of tank volume calculation. Some solutions for decreasing the deviation and a modification scheme regarding with tank volume measurement are proposed in this paper.
参考文献/References:
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[2]机械设计手册编委会. 机械设计手册[M]. 3版. 北京: 机械工业出版社, 2007.
[3]周广文. 推进剂贮箱优化设计思考[J]. 导弹与航天运载技术, 2011 (1): 26-28.
[4]朱平萍, 刘宪力. 大型贮箱结构及工艺性研究[J]. 航天制造技术, 2011 (3): :42-45.
[5]陈朝, 黄敏超, 陈志坚. 空间表面张力贮箱结构分析与优化设计[J]. 航天制造技术, 2007 (5): 9-12.
[6]石晓强. 卫星用推进剂贮箱和高压气瓶封头制造技术[J]. 真空与低温, 2008 (3): 184-186.
[7]MICHAEL JDEBRECENI, WILLIAM D LAY. Propellant tank for an advanced communications satellite，AIAA-2001-3826[R]. USA: AIAA, 2001.
[8]WALTER H TAM，JIM R TAYLOR. Design and manu- facture of a propellant tank assembly，AIAA-97-2813[R]. USA：AIAA，1997.
相似文献/References:
[1]王定军,袁洪滨,董苑.贮箱充填过程仿真和分析[J].火箭推进,2008,34(01):23.
Wang Dingjun,Yuan Hongbin,Dong Yuan.Simulation and analysis of the tank filling process[J].Journal of Rocket Propulsion,2008,34(01):23.
备注/Memo
收稿日期：2012-06-１5；修回日期：2012-09-25 作者简介：马键（1972—），男，高级工程师，研究领域为液体火箭发动机总体设计
更新日期/Last Update:
1900-01-01