Experimental study of air/ethanol mono-injector gas generator

ZHAO Fang; REN Zebin; LI Xianfeng; GUO Longde; TAO Yu; SHI Yu; LUO Zhifeng

doi:10.11729/syltlx20180186

Volume 34 Issue 1

Feb. 2020

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Journal of Experiments in Fluid Mechanics > 2020 > 34(1): 72-78. > DOI: 10.11729/syltlx20180186

ZHAO Fang, REN Zebin, LI Xianfeng, GUO Longde, TAO Yu, SHI Yu, LUO Zhifeng. Experimental study of air/ethanol mono-injector gas generator[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(1): 72-78. DOI: 10.11729/syltlx20180186

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Experimental study of air/ethanol mono-injector gas generator

1.
Facility Design and Instrumentation Institute of China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China
2.
State Key Laboratory of Aerodynamics, China Aerody-namics Research and Development Center, Mianyang Sichuan 621000, China
3.
AECC Sichuan Gas Turbine Research Establishment, Mianyang Sichuan 621000, China

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Received Date: November 25, 2018
Revised Date: September 09, 2019

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Abstract

Abstract

With regard to the safety, economy and miniaturization of the ejector system, a mono-injector air/ethanol gas generator based on the aero-engine combustor structure was designed. A series of ignition tests were carried out. The results show that:the technical design scheme of the gas generator is feasible, and reliable ignition of the gas generator can be realized by direct ignition of the high energy spark plug. The pressure curve indicates a rapid ignition of the generator, and the main working parameters basically meet the design index. The low limit of the excess air coefficient of the gas generator for reliable ignition is 3.9, showing a wide mass flow-rate range. The combustion efficiency is high, decreasing obviously with the increase of the excess air coefficient.
- ejector system,
- aero-engine combustor,
- gas generator,
- mono-injector,
- excess air coefficient

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References

[1]	FABRI J, PAULON J. Theory and experiments on super-sonic air-to-air ejectors[R]. NACA-TM-1410, 1958.
[2]	徐万武, 邹建军, 王振国, 等.超声速环型引射器启动特性试验研究[J].火箭推进, 2005, 31(6): 7-11. DOI: 10.3969/j.issn.1672-9374.2005.06.002 XU W W, ZOU J J, WANG Z G, et al. Experimental investigation of the start performances of the supersonic annular ejector[J]. Journal of Rocket Propulsion, 2005, 31(6): 7-11. DOI: 10.3969/j.issn.1672-9374.2005.06.002
[3]	陈健, 王振国, 吴继平, 等.等截面超-超引射器流场结构及引射性能[J].强激光与粒子束, 2012, 24(6): 1301-1305. http://d.old.wanfangdata.com.cn/Periodical/qjgylzs201206009 CHEN J, WANG Z G, WU J P, et al. Flow structure and performance of constant-area, supersonic-supersonic ejector[J]. High Power Laser and Particle Beams, 2012, 24(6): 1301-1305. http://d.old.wanfangdata.com.cn/Periodical/qjgylzs201206009
[4]	CONNAUGHTON J C. Application of a hydrazine gas generator to vacuum ejector pumping of a chemical laser[R]. AIAA-77-0892.
[5]	曹再勇, 蔡体敏, 谭永华.富氧燃气发生器三维燃烧流场的数值模拟[J].西北工业大学学报, 2005, 23(5): 557-561. DOI: 10.3969/j.issn.1000-2758.2005.05.003 CAO Z Y, CAI T M, TAN Y H. Furnishing some theoretical basis for design of oxygen-rich gas generator[J]. Journal of Northwestern Polytechnical University, 2005, 23(5): 557-561. DOI: 10.3969/j.issn.1000-2758.2005.05.003
[6]	马冬英, 卢钢, 张小平, 等.液氧/甲烷燃气发生器试验研究[J].火箭推进, 2013, 39(3): 21-26. DOI: 10.3969/j.issn.1672-9374.2013.03.004 MA D Y, LU G, ZHANG X P, et al. Research on hot tests of LOX/methane gas generator[J]. Journal of Rocket Propulsion, 2013, 39(3): 21-26. DOI: 10.3969/j.issn.1672-9374.2013.03.004
[7]	冯军红, 沈赤兵, 赵芳.液氧与气氧对空气加热器燃烧流场的影响分析[J].国防科技大学学报, 2012, 34(4): 43-48. DOI: 10.3969/j.issn.1001-2486.2012.04.009 FENG J H, SHEN C B, ZHAO F. Analysis of liquid and gaseous oxygen influence on the combustion flow field of air heater[J]. Journal of National University of Defense Technology, 2012, 34(4): 43-48. DOI: 10.3969/j.issn.1001-2486.2012.04.009
[8]	李茂, 高玉闪, 陈泽, 等.气氢/气氧富燃预燃室设计与试验[J].航空动力学报, 2011, 26(6): 1426-1430. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hkdlxb201106032 LI M, GAO Y S, CHEN Z, et al. Design and experiment for a GH₂/ GO₂ fuel rich preburner[J]. Journal of Aerospace Power, 2011, 26(6): 1426-1430. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=hkdlxb201106032
[9]	俞南嘉, 蔡国飙, 张国舟, 等.富氧预燃室初步试验研究[J].宇航学报, 2006, 27(5): 834-838. DOI: 10.3321/j.issn:1000-1328.2006.05.003 YU N J, CAI G B, ZHANG G Z, et al. Initial experiment research of oxidizer rich preburner[J]. Journal of Astronautics, 2006, 27(5): 834-838. DOI: 10.3321/j.issn:1000-1328.2006.05.003
[10]	金平, 俞南嘉, 邬志岐, 等.氢氧全流量补燃循环发动机燃预燃室试验[J].推进技术, 2008, 29(3): 273-277. DOI: 10.3321/j.issn:1001-4055.2008.03.004 JIN P, YU N J, WU Z Q, et al. Experimental investigation of fuel rich preburner of hydrogen/oxygen FFSC cycle engine[J]. Journal of Propulsion Technology, 2008, 29(3): 273-277. DOI: 10.3321/j.issn:1001-4055.2008.03.004
[11]	李清廉, 李庆, 王振国.氧气/醇类燃气发生器启动过程试验研究[J].火箭推进, 2010, 36(1): 13-18. DOI: 10.3969/j.issn.1672-9374.2010.01.003 LI Q L, LI Q, WANG Z G. Experimental research of the start-up process of gaseous oxygen/ethanol gas generator[J]. Journal of Rocket Propulsion, 2010, 36(1): 13-18. DOI: 10.3969/j.issn.1672-9374.2010.01.003
[12]	张新桥, 李清廉, 康忠涛.空气/煤油/水燃气发生器点火特性试验[J].国防科技大学学报, 2013, 35(4): 35-40. DOI: 10.3969/j.issn.1001-2486.2013.04.007 ZHANG X Q, LI Q L, KANG Z T. Experimental researches on ignition characteristic of air /kerosene /water gas generator[J]. Journal of National University of Defense Technology, 2013, 35(4): 35-40. DOI: 10.3969/j.issn.1001-2486.2013.04.007
[13]	金盛宇, 许宏博, 吉林.空气/煤油燃气发生器技术研究[J].火箭推进, 2014, 40(3): 29-32. DOI: 10.3969/j.issn.1672-9374.2014.03.005 JIN S Y, XU H B, JI L. Technology research on air/jet fuel gas generator[J]. Journal of Rocket Propulsion, 2014, 40(3): 29-32. DOI: 10.3969/j.issn.1672-9374.2014.03.005
[14]	陈志强, 廖达雄, 刘宗政, 等.过氧化氢加酒精补燃气体发生器实验研究[J].强激光与粒子束, 2007, 19(9): 1409-1412. http://d.old.wanfangdata.com.cn/Periodical/qjgylzs200709001 CHEN Z Q, LIAO D X, LIU Z Z, et al. Experimental studies of gas generator based on hydrogen peroxide and hypergolic ethanol[J]. High Power Laser and Particle Beams, 2007, 19(9): 1409-1412. http://d.old.wanfangdata.com.cn/Periodical/qjgylzs200709001
[15]	刘景华, 谭建国, 杨涛, 等.过氧化氢发动机中的低频振荡[J].国防科技大学学报, 2007, 29(5): 23-26. DOI: 10.3969/j.issn.1001-2486.2007.05.006 LIU J H, TAN J G, YANG T, et al. Research on low-frequency oscillation in hydrogen peroxide engine[J]. Journal of National University of Defense Technology, 2007, 29(5): 23-26. DOI: 10.3969/j.issn.1001-2486.2007.05.006
[16]	刘盛田, 胡兴伟, 柳琪, 等.一氧化二氮/乙醇燃气发生器试验研究[J].舰船科学与技术, 2008, 30(6): 223-226. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=jckxjs2008z2012 LIU S T, HU X W, LIU Q, et al. The experimental studies of gas generator based on nitrous oxide and ethanol[J]. Ship Science and Tech-nology, 2008, 30(6): 223-226. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=jckxjs2008z2012
[17]	廖达雄, 任泽斌, 余永生, 等.等压混合引射器设计与实验研究[J].强激光与粒子束, 2006, 18(5): 728-732. http://d.old.wanfangdata.com.cn/Periodical/qjgylzs200605007 LIAO D X, REN Z B, YU Y S, et al. Design and experiment of constant pressure mixing ejector[J]. High Power Laser and Particle Beams, 2006, 18(5): 728-732. http://d.old.wanfangdata.com.cn/Periodical/qjgylzs200605007
[18]	廖达雄.气体引射器原理及设计[M].北京: 国防工业出版社, 2018. LIAO D X. Principle and design of gas ejector[M]. Beijing: National Defense Industry Press, 2018.
[19]	LEFEBVRE A H. Gas turbine combustion[M]. Washington: Hemisphere Publishing Corp, 1983.
[20]	MELLOR A M. Design of modern turbine combustors[M]. New York: Academic Press Inc, 1990.

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