采用固体燃料的超燃冲压发动机研究进展

吕仲; 夏智勋; 刘冰; 刘元春

doi:10.13224/j.cnki.jasp.2016.08.024

采用固体燃料的超燃冲压发动机研究进展

doi: 10.13224/j.cnki.jasp.2016.08.024

1. 国防科学技术大学高超声速冲压发动机技术重点实验室, 长沙 410073;
2. 国防科学技术大学航天科学与工程学院, 长沙 410073

详细信息

作者简介:
吕仲(1987-),男,辽宁大连人,博士生,主要研究方向为航空宇航推进技术.

中图分类号: V23
计量
- 文章访问数: 933
- HTML浏览量: 5
- PDF量: 658
- 被引次数: 0
出版历程
- 收稿日期: 2015-04-06
- 刊出日期: 2016-08-28

Review of research on solid fuel scramjet engine

1. Science and Technology on Scramjet Laboratory, National University of Defense Technology, Changsha 410073, China;
2. College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China

摘要

摘要: 对采用固体燃料的超燃冲压发动机构型方案进行了归纳总结，详细的介绍了不同构型方案的发展历程和研究现状.针对固体燃料构型、双燃烧室构型和固体火箭构型3种不同构型的工作特点，分析了各自的优势和存在的问题，并在此基础上对其后续的研究提出了建议.研究认为：固体燃料构型方案虽能实现固体燃料在超声速气流中的点火及稳定燃烧，但燃料燃烧效率较低，且难以长时间稳定工作；固体火箭构型方案有利于燃料的点火和稳定燃烧，可实现发动机的长时间稳定工作，具有更好的研究和应用前景.
- 冲压发动机 /
- 固体燃料 /
- 固体火箭 /
- 双燃烧室 /
- 超声速燃烧
Abstract: The configurations of scramjet using solid fuel as propellant were summarized, and the progress and status of different configurations of scramjet using solid fuel propellant were elaborated, respectively. According to the operating feature of solid-fuel scramjet, solid-fuel dual-combustor scramjet and solid-fuel rocket scramjet, the advantages and existing problems of different configurations were analyzed, and some suggestions for further research were proposed. The research results reveal that though solid fuel can ignite and burn in supersonic combustor of solid-fuel scramjet, the combustion efficiency of propellant is low and the scramjet cannot operate for a long time. The solid-fuel rocket scramjet is beneficial to ignition and stable combustion of solid fuel, and can also operate for a long time. The solid-fuel rocket scramjet has a bright research and application prospect.
- ramjet /
- solid fuel /
- solid rocket /
- dual combustor chamber /
- supersonic combustion

HTML

参考文献(57)

[1]	Richard J W,John S M.An analysis of ramjet engines using supersonic combustion[R].NACA TN4386,1958.
[2]	Billig F S.Tactical missile design concepts[J].Hohes Hopkins APL Technical Digest,1983,4(3):139-154.
[3]	Shelly F,Charles M,Ken R,et al.Hyper-X Mach 7 scramjet design,ground test and flight results[R].AIAA/CIRA 2005-3322,2005.
[4]	Rogers R,Shih A.Scramjet development tests supporting the Mach 10 flight of the X-43[R].AIAA/CIRA 2005-3351,2005.
[5]	Curran E T.Scarmjet engines:the first forty years[J].Journal of Propulsion and Power,2001,17(6):1138-1148.
[6]	Curran E T,Murthy S N B.Scramjet propulsion[M].Reston,VA:Progress in Astronautics and Aeronautics,2000.
[7]	Ronald S F.A century of ramjet propulsion technology evolution[J].Journal of Propulsion and Power,2004,20(1):27-58.
[8]	Shyy W,Rycroft M J.The scramjet engine:processes and characteristics[M].New York:Cambridge University Press,2009.
[9]	蔡国飙,徐大军.高超声速飞行器技术[M].北京:科学出版社,2012.
[10]	赵庆华,刘建全,王莉莉,等.固体燃料的超声速燃烧研究进展[J].飞航导弹,2009,10(10):59-63. ZHAO Qinghua,LIU Jianquan,WANG Lili,et al.Research progress of supersonic combustion[J].Aerodynamic Missile Journal,2009,10(10):59-63.(in Chinese)
[11]	Witt M.Investigation into the feasibility of using solid fuel ramjets for high supersonic/low supersonic tactical missiles[D].Monterey,CA:Naval Postgraduate Schoo1,1989.
[12]	Vaught C,Witt M,Netzer D W,et al.Investigation of solid fuel,dual mode combustion ramjets[J].Journal of Propulsion and Power,1992,8(5):1004-1011.
[13]	吕仲.固体火箭超燃冲压发动机工作特性研究[D].长沙:国防科学技术大学,2012. LV Zhong.Investigation on operating characteristics of solid-fuel rocket scramjet engine[D].Changsha:National University of Defense Technology,2012.(in Chinese)
[14]	Angus W J.An investigation into the performance characteristics of a solid fuel scramjet propulsion device[D].Monterey,CA:Naval Postgraduate Schoo1,1991.
[15]	Angus W J,Witt M,Laredo D,et al.Solid fuel supersonic combustion[J].La Recherche Aerospatiale,1993(6):1-8.
[16]	Ben-Yakar A,Gany A.Experimental study of a solid fuel scramjet[R].AIAA 94-2815,1994.
[17]	Ben-Yakar A,Natan B,Gany A.Investigation of a solid fuel scramjet combustor[J].Journal of Propulsion and Power,1998,14(4):447-455.
[18]	Cohen-Zur A,Natan B.Experimental investigation of a supersonic combustion solid fuel ramjet[J].Journal of Propulsion and Power,1998,14(6):880-889.
[19]	刘巍.固体燃料冲压发动机燃烧组织技术研究[D].长沙:国防科学技术大学,2010. LIU Wei.Research on the combustion technology of solid fuel ramjet[D].Changsha:National University of Defense Technology,2010.(in Chinese)
[20]	夏强.固体燃料冲压发动机工作过程研究[D].南京:南京理工大学,2011. XIA Qiang.Investigation on the working process of solid fuel ramjet[D].Nanjing:Nanjing University of Science and Technology,2011.(in Chinese)
[21]	Helmy A M.Performance of polycubances in solid fuel ramjet[R].AIAA 93-2591,1993.
[22]	Segal C.Iginition characteristics of a new high-energy density fuel in high-speed flows[J].Journal of Propulsion and Power,1997,12(14):762-766.
[23]	Saraf S,Gany A.Testing metallized solid fuel s cramjetcombustion[R].ISABE-2007-1176,2007.
[24]	Char J M,Hsu U K.Observation of solid fuel in a supersonic flowfield[J].Transactions on Modeling and Simulation,2007,46:25-34.
[25]	Hsu U K.Numerical and experimental investigation of a supersonic flow field around solid fuel on an inclined flat plate[J].Modelling and Simulation in Engineering,2009,2009:1-10.
[26]	WANG Lihe,CHI Hongwei,LIU Cangxiu,et al.Numerical and experimental study of solid fuel scramjet combustor with a cavity flame holder[R].AIAA-2014-3453,2014.
[27]	WANG Lihe,WU Zhiwei,Chi Hongwei,et al.Numerical and experimental study on solid-fuel scramjet combustor[J].Journal of Propulsion and Power,2015,31(2):684-693
[28]	杨向明,刘伟凯,陈林泉,等.固体燃料超燃冲压发动机原理性实验研究[J].固体火箭技术,2012,35(3):319-324. YANG Xiangming,LIU Weikai,CHEN Linquan,et al.Experiment study on the principle of solid fuel scramjet[J].Journal of Solid Rocket Technology,2012,35(3):319-324.(in Chinese)
[29]	Marxman G T,Gilbert M.Turbulent boundary layer combustion in the hybrid rocket[R].New York:9th Symposium (International) on Combustion,1963.
[30]	Marxman G T.Combustion in the turbulent boundary layer on a vaporizing surface[J].Symposium (International) on Combustion,1965,10(1):1337-1349.
[31]	Jarymowycz T,Yang V,Kuo K K.A numerical study of solid fuel combustion under supersonic crossflows[R].AIAA 90-2076,1990.
[32]	Snyder T S,Jarymowycz T A,Hsieh W H,et al.Pyrolysis and combustion of solid fuels under subsonic and supersonic conditions[R].Pasodena,US:26th JANNAF Combustion Meeting Report,1989.
[33]	Ben-Arosh R,Natan B,Spiegler E,et al.The reacting flowfield within a supersonic combustion solid fuel ramjet[R].AIAA 97-3119,1997.
[34]	杨明,孙波.固体燃料超燃冲压发动机燃烧室的数值仿真[J].兵工自动化,2012,31(1):37-41. YANG Ming,SUN Bo.Numerical simulation of a solid fuel scramjet combustor[J].Ordnance Industry Automation,2012,31(1):37-41.(in Chinese)
[35]	杨明.固体燃料超燃冲压发动机内流场研究[D].南京:南京理工大学,2012. YANG Ming.Study on the solid fuel scramjet internal flow field[D].Nanjing:Nanjing University of Science and Technology,2012.(in Chinese)
[36]	陶欢,魏志军,武志文,等.固体燃料超燃冲压发动机燃烧室流动与掺混过程研究[J].飞航导弹,2012(8):75-79. TAO Huan,WEI Zhijun,WU Zhiwen,et al.Study on the flow and mixing process of the solid fuel scramjet[J].Aerodynamic Missile Journal,2012(8):75-79.(in Chinese)
[37]	PEI Xinyan,WU Zhijun,WEI Zhijun,et al.Numerical investigation on internal regressing shapes of solid-fuel scramjet combustor[J].Journal of Propulsion and Power,2013,29(5):1041-1051.
[38]	刘伟凯,陈林泉,杨向明.固体燃料超燃冲压发动机燃烧室掺混燃烧数值研究[J].固体火箭技术,2012,35(4):457-462. LIU Weikai,CHEN Linquan,YANG Xiangming.Numerical study of mixing flows in a solid fuel scramjet combustor[J].Journal of Solid Rocket Technology,2012,35(4):457-462.(in Chinese)
[39]	LI Biao,WEI Zhijun,CHI Hongwei.Numerical analysis of solid fuel scramjet operating at Mach 4 to 6[R].AIAA-2013-3695,2013.
[40]	李彪,魏志军,迟鸿伟,等.不同来流条件下固体燃料超燃冲压发动机性能评估[J].固体火箭技术,2014,37(4):469-474. LI Biao,WEI Zhijun,CHI Hongwei,et al.Performance evaluation of solid fuel scramjet under different inflow conditions[J].Journal of Solid Rocket Technology,2014,37(4):469-474.(in Chinese)
[41]	陶欢,魏志军,迟鸿伟,等.等直段直径对固体燃料超燃冲压发动机燃烧室性能的影响[J].推进技术,2015,36(6):884-892. TAO Huan,WEI Zhijun,CHI Hongwei,et al.Effects of diameter of cylindrical section on flowfield characteristics of solid fuel scramjet combustor[J].Journal of Propulsion Technology,2015,36(6):884-892.(in Chinese)
[42]	王利和,武志文,刘昶秀,等.入口气流参数对固体燃料超燃冲压发动机燃烧室性能的影响分析[J].兵工学报,2014,35(5):691-696. WANG Lihe,WU Zhiwen,LIU Changxiu,et al.The effect of entrance airflow parameters on solid fuel scramjet combustor performance[J].Acta Armaentarh,2014,35(5):691-696.(in Chinese)
[43]	PEI Xinyan,WU Zhiwei,WEI Zhijun,et al.Numerical investigation on cavity length for solid fuel scramjet[R].AIAA-2012-3830,2012.
[44]	TAO Huan,WEI Zhijun.Numerical investigation on the effects of Cavity in solid fuel scramjet[R].AIAA-2013-3974,2013.
[45]	陶欢,魏志军,迟鸿伟,等.固体燃料凹腔结构对超声速流动的影响[J].固体火箭技术,2014,37(3):307-314. TIAO Huan,WEI Zhijun,CHI Hongwei,et al.Effects of cavity on solid fuel scramjet combustor characteristics under supersonic cross flow[J].Journal of Solid Rocket Technology,2014,37(4):307-314.(in Chinese)
[46]	PEI Xinyan,HOU Lingyun.Numerical investigation on cavity structure of solid-fuel scramjet combustor[J].Acta Astronautica,2014,105(2):463-475.
[47]	迟鸿伟,魏志军,李彪,等.台阶和凹腔在固体燃料超燃冲压发动机内自点火性能对比[J].固体火箭技术,2014,37(5):628-639. WEI Hongwei,WEI Zhijun,LI Biao,et al.Difference of self-ignition performance in solid fuel scramjet with step or cavity[J].Journal of Solid Rocket Technology,2014,37(5):628-639.(in Chinese)
[48]	迟鸿伟,魏志军,王利和,等.固体燃料超燃冲压发动机燃烧室中PMMA自点火性能数值研究[J].推进技术,2014,35(6):799-808. CHI Hongwei,WEI Zhijun,WANG Lihe,et al.Numerical investigation on self-ignition of PMMA in solid fuel scramjet[J].Journal of Propulsion Technology,2014,35(6):799-808.(in Chinese)
[49]	LIU Changxiu,WEI Zhijun,CHI Hongwei,et al.Numerical investigation on influence on the regression rate of the inlet parameters in solid fuel scramjet combustor[R].AIAA-2014-3452,2014.
[50]	CHI Hongwei,WEI Zhijun,LI Biao,et al.Numerical investigation on self-ignition and flammability characteristics in solid fuel scramjet combustor[R].AIAA-2014-3451,2014.
[51]	迟鸿伟,魏志军,王利和,等.固体燃料超燃冲压发动机燃烧室中火焰稳定数值研究[J].推进技术,2015,36(10):1495-1503. CHI Hongwei,WEI Zhijun,WANG Lihe,et al.Numerical investigation of combustion flammability characteristics in solid fuel scramjet combustor[J].Journal of Propulsion Technology,2015,36(10):1495-1503.(in Chinese)
[52]	王利和,武志文,迟鸿伟,等.固体燃料超燃冲压发动机燃烧室流场准一维计算方法研究[J].固体火箭技术,2013,36(6):742-747. WANG Lihe,WU Zhiwen,CHI Hongwei,et al.A method of quasi-one dimensional numerical analysis for solid fuel scramjet combustor perforamance[J].Journal of Solid Rocket Technology,2013,36(6):742-747.(in Chinese)
[53]	WANG Lihe,LI Shipeng,CHI Hongwei,et al.Quasi-one-dimensional numerical method for solid fuel scramjet combustor analysis and design[J].Journal of Aerospace Engineering,2015,28(3):217-222.
[54]	王利和,武志文,迟鸿伟,等.不同台阶高度下固体燃料超燃冲压发动机燃烧室初始型面变化规律[J].推进技术,2013,34(11):1493-1498. WANG Lihe,WU Zhiwen,CHI Hongwei,et al.Initial profile variation rule of solid fuel scramjet combustor with different step height numerical study of mixing flows in a solid fuel scramjet combustor[J].Journal of Propulsion Technology,2013,34(11):1493-1498.(in Chinese)
[55]	孙海刚,贺永杰.双燃烧室固体燃料超声速燃烧研究[J].弹箭与制导学报,2014,34(4):125-128. SUN Haigang,HE Yongjie.Investigation of supersonic combustion of solid fuel in dual combustor[J].Journal of Project,Rockets,Missiles and Guidance,2014,34(4):125-128.(in Chinese)
[56]	LV Zhong,XIA Zhixun,LIU Bing,et al.Experimental and numerical investigation of a solid-fuel rocket scramjet combustor[J].Journal of Propulsion and Power,2015,32(2):1-6.
[57]	李轩,马利锋,赵永涛,等.固体火箭超燃冲压发动机性能数值模拟研究[J].弹箭与制导学报,2013,34(1):104-161. LI Xuan,MA Lifeng,ZHAO Yongtao,et al.Numerical investigation on combustion performance,solid rocket scramejt[J].Journal of Propulsion,Rocket,Missiles and Guidance,2014,34(1):104-161.(in Chinese)