基于AMESim的隔舱式贮箱推进剂管理仿真研究

苏立超; 刘建勇; 章成亮; 石竟成

doi:10.13224/j.cnki.jasp.2015.09.030

基于AMESim的隔舱式贮箱推进剂管理仿真研究

doi: 10.13224/j.cnki.jasp.2015.09.030

中国航天科技集团公司中国运载火箭技术研究院空间物理重点实验室, 北京 100076

详细信息

作者简介:
苏立超(1985-),男,河北衡水人,工程师,硕士,主要研究方向为发动机总体设计、增压输送系统总体设计.

中图分类号: V434.1
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出版历程
- 收稿日期: 2014-08-03
- 刊出日期: 2015-09-28

Simulation research on compartmental tank propellant management based on AMESim

Science and Technology on Space Physics Laboratory, China Academy of Launch Vehicle Technology, China Aerospace Science and Technology Corporation, Beijing 100076, China

摘要

摘要: 通过多学科动力学建模方法研究,利用AMESim建立了隔舱式贮箱推进剂输送系统机械、液流与控制动力学模型,并对不同工况下推进剂输送系统动态特性进行数值仿真,获得了隔舱式贮箱推进剂动态变化、各个隔舱的推进剂消耗率及质心位移等结果.仿真结果显示隔舱总体布局与初始容积分配、隔舱连通结构、飞行轨迹等均对隔舱式贮箱推进剂动态变化产生影响,所建立的模型可应用于隔舱式贮箱总体及结构设计.
- 动态仿真 /
- 隔舱式贮箱 /
- AMESim模型 /
- 推进剂管理 /
- 质心计算
Abstract: According to the research on the method of multi-subjects dynamic modeling, an AMESim mechanical, hydraulic and control dynamic complicated model of propellant feed system based on the compartmental tank was established, and then numerical simulation was made on the dynamic characteristics of the propellant feed system under different working conditions. The results of dynamic change of the propellant, the comsumption rate and the centroid displacement of the propellant were obtained. The simulation results show that the dynamic change of the compartmental tank propellant is influenced by the compartments general layout, initial compartments volume, structure design, flight trajectory and etc, so the simulation model can provide guidance to improve compartmental tank overall and structure design.
- dynamic simulation /
- compartmental tank /
- AMESim model /
- propellant management /
- centroid calculation

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参考文献(20)

[1]	廖少英.液体火箭推进增压输送系统[M].北京:国防工业出版社,2007.
[2]	廖少英,赵金才.航空-航天飞行器推进增压输送系统设计[M].北京:中国宇航出版社,2012.
[3]	Wiswell R.X-15 propulsion system[R].AIAA 97-2682,1997.
[4]	Brown T M,Knight K C,Champion R H.X-34 main propulsion system design and operation[R].AIAA 98-4032,1998.
[5]	陈嵩禄.飞机设计手册:动力装置系统设计[M].北京:航空工业出版社,2006.
[6]	廖少英.大气层内高超声速机动飞行器液体推进剂管理[J].上海航天,2005,22(2):34-38. LIAO Shaoying.Liquid propellant management for the hypersoar mobile vehicle in the atmospheric layer[J].Aerospace Shanghai,2005,22(2):34-38.(in Chinese)
[7]	郭斌.X-34主推进系统输送管路的流动分析[J].火箭推进,2001,27(3):59-62. GUO Bin.Flow analysis of X-34 main propulsion system feed-line[J].Journal of Rocket Propulsion,2001,27(3):59-62.(in Chinese)
[8]	廖少英.跨大气层和空间区域飞行器的液体推进剂管理[J].上海航天,2006,23(5):38-41. LIAO Shaoying.Research on liquid propellant management for cross atmospheric layer and space vehicle[J].Aerospace Shanghai,2006,23(5):38-41.(in Chinese)
[9]	BrownT M,McDonald J P,Hedayat A,et al.Propellant management and conditioning within the X-34 main propulsion system[R].AIAA 98-3518,1998.
[10]	Chanipion R H,Jr,Darrow R J,Jr.X-34 main propulsion system design and operation[R].AIAA 98-4032,1998.
[11]	McDonald J P,Minor R B,Knight K C,et al.Propellant feed subsystem for X-34 main propulsion system[R].AIAA 98-3517,1998.
[12]	Patrick K S.X-34 propulsion system design[R].Seattle,W A:3rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit,1997.
[13]	潘辉,张黎辉.AMESim软件在液体火箭发动机系统动态仿真上的应用[J].火箭推进,2011,37(3):6-11. PAN Hui,ZHANG Lihui.Application of AMESim in dynamic characteristic simulation of liquid rocket engine system[J].Journal of Rocket Propulsion,2011,37(3):6-11.(in Chinese)
[14]	刘靖东,隋国发,娄东亮,等.液体火箭增压输送系统多学科动力学研究[J].中国科学:E辑技术科学,2009,39(3):474-481. LIU Jingdong,SUI Guofa,LOU Dongliang,et al.Study on the multidisciplinary dynamics of the liquid rocket pressurization feed system[J].Science in China:Series E Technological Sciences,2009,39(3):474-481.(in Chinese)
[15]	付永领,齐海涛.AMESim系统建模和仿真[M].北京:北京航空航天大学出版社,2011.
[16]	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(2):23-25. WANG Dingjun,YUAN Hongbin,DONG Yuan.Simulation and analysis of the tank filling process[J].Journal of Rocket Propulsion,2008,34(2):23-25.(in Chinese)
[17]	尤裕荣,赵双龙,吴宝元,等.基于AMESim的冲压发动机燃油调节器动态特性仿真[J].火箭推进,2010,36(4):12-15. YOU Yurong,ZHAO Shuanglong,WU Baoyuan,et al.A simulation on dynamic characteristics of ramjet fuel regulator based on AMESim[J].Journal of Rocket Propulsion,2010,36(4):12-15.(in Chinese)
[18]	董春方,朱玉杰,冯国红.基于AMESim的长管道液压系统动态仿真[J].煤矿机械,2010,31(1):73-75. DONG Chunfang,ZHU Yujie,FENG Guohong.Study on dynamical simulation of long pipeline hydraulic system based on AMESim[J].Coal Mine Machinery,2010,31(1):73-75.(in Chinese)
[19]	司景萍.液类货物运输中质心位置的计算分析[J].内蒙古工业大学学报,2002,21(3):222-226. SI Jingping.Calculating analysis on the barycenter location in transporting of liquid goods[J].Journal of Inner Mongolia University of Technology,2002,21(3):222-226.(in Chinese)
[20]	岳宝增,刘延柱,王照林.求解液体大幅晃动问题的数值方法评述[J].上海交通大学学报,1996,33(6):760-763. YUE Baozeng,LIU Yanzhu,WANG Zhaolin.Review of the numerical methods for simulating large-scale amplitude sloshing of liquid[J].Journal of Shanghai Jiaotong University,1996,33(6):760-763.(in Chinese)