航天推进技术研究院主办
[1]黄其殷,王幸果,刘 上,等.液氧/煤油发动机起动箱仿真与试验研究[J].火箭推进,2015,41(03):21-26.
HUANG Qi-yin,WANG Xing-guo,LIU Shang,et al.Simulation and test study on starting box of LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2015,41(03):21-26.
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HUANG Qi-yin,WANG Xing-guo,LIU Shang,et al.Simulation and test study on starting box of LOX/kerosene rocket engine[J].Journal of Rocket Propulsion,2015,41(03):21-26.
液氧/煤油发动机起动箱仿真与试验研究
《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V]
卷:
41
期数:
2015年03期
页码:
21-26
栏目:
研究与设计
出版日期:
2015-06-30
- Title:
- Simulation and test study on starting box of LOX/kerosene rocket engine
- 分类号:
- V434-34
- 文献标志码:
- A
- 摘要:
- 起动箱是保证液氧/煤油发动机可靠起动的重要组件。针对起动箱结构特点，采用胶囊材料Mooney-Revlin本构关系，建立起动箱三维模型，分析起动箱动作特性。仿真结果再现了起动箱工作过程，获得胶囊翻转压力为58 kPa。抽真空试验和计算表明，胶囊压力为50～60kPa时起动箱胶囊可自动复位，仿真结果与试验结果基本吻合。
- Abstract:
- The starting box is an important component for the stable and reliable starting of LOX/kerosene rocket engine. The operational characteristics of the starting box are analyzed by Mooney-Revlin model of bladder material and 3D model of the starting box. The operational process of the starting box was reoccurred by means of simulation result. The reversing pressure (58 kPa) of the rubber bladder was obtained. The vacuum test and calculation show that the bladder will return to its original position automatically under the pressure of 50~60 kPa. The predicted values are agree with the measured ones.
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备注/Memo
收稿日期：2014-12-03；修回日期：2015-01-22 基金项目：国家863项目（2012AA702302） 作者简介：黄其殷（1983—），男，硕士，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