航空燃气涡轮发动机氢燃料研究历史和低污染燃烧技术发展

李迎春; 郑光华

航空燃气涡轮发动机氢燃料研究历史和低污染燃烧技术发展

李迎春¹,
郑光华²

1.
中国航空工业集团公司中国航空动力机械研究所第三研究部, 湖南株洲 412002
2.
西北工业大学动力与能源学院, 西安 710072

计量
- 文章访问数: 2225
- HTML浏览量: 203
- PDF量: 615
- 被引次数: 0
出版历程
- 收稿日期: 2011-04-21
- 修回日期: 2011-08-29
- 刊出日期: 2012-03-28

Review of study history and low emission combustion technology development on aero gas turbines fuelling hydrogen

LI Ying-chun¹,
ZHENG Guang-hua²

1.
The Third Department, China Aviation Powerplant Research Institute, Aviation Industry Corporation of China, Zhuzhou Hunan 412002
2.
School of Power and Energy, Northwestern Polytechnical University, Xi’an 710072, China

摘要

摘要: 氢燃料的应用对航空燃气涡轮发动机技术的发展具有重要的意义.根据国外对氢燃料在航空燃气涡轮发动机领域的应用研究,对相关研究历程进行了回顾,并对氢燃料低污染燃烧技术进行了分析.结果表明氢燃料在航空燃气涡轮发动机领域研究的重点已从早期的以军用为主转为以民用为主;氢燃料低污染燃烧技术的关键在于控制主燃区的贫油燃烧;而微混非预混扩散燃烧技术具有很大的应用潜力.
- 航空燃气涡轮发动机 /
- 氢燃料 /
- 低污染 /
- 贫油燃烧 /
- 微混非预混扩散燃烧
Abstract: The application of hydrogen is substantial to the development of aero gas turbine technology. According to the hydrogen application studies in aero gas turbine field, the history of the studies was reviewed and low emission combustion technologies were analyzed. The result indicates that the focus of hydrogen application study in aero gas turbine field has been shifted from early military purpose oriented to civil purpose oriented; the lean burning of primary zone is the key of hydrogen low emission combustion technology; the micro-mix non-premixed diffusive combustion has a great potential to be applied in hydrogen low emission combustion.
- aero gas turbines /
- hydrogen /
- low emission /
- lean burning /
- micro-mix non-premixed diffusive combustion

HTML

参考文献(25)

[1]	刘敬华,刘兴洲,胡欲立.超音速气流中氧燃料强化混合的燃烧实验研究[J].推进技术,1996,17(1):1-7. LIU Jinghua,LIU Xingzhou,HU Yuli.An experimental study on combustion in supersonic flow with enhanced mixing of hydrogen fuel[J].Journal of Propulsion Technology,1996,17(1):1-7.(in Chinese)
[2]	徐旭,蔡国飙.氢/碳氢燃料超声速燃烧的数值模拟[J].推进技术,2002,23(5):398-401. XU Xu, CAI Guobiao.Numerical simulation on combustion of hydrogen/hydrocarbon in supersonic airstream[J].Journal of Propulsion Technology,2002,25(5):398-401.(in Chinese)
[3]	崔玉峰,徐纲,黄伟光.后台阶喷氢加喷空气超音速燃烧数值模拟[J].航空学报,2004,25(2):113-116. CUI Yufeng,XU Gang,HUANG Weiguang.Numerical simulation on combustion over a reward facing step with transverse hydrogen and air injection[J].Acta Aeronautica et Astronautica Sinica,2004,25(2):113-116.(in Chinese)
[4]	周建兴,朴英,岂兴明.两种超声速燃烧室内氢气燃烧的三维数值研究[J].航空动力学报,2008,23(3):470-475. ZHOU Jianxing,PIAO Ying,QI Xingming.3-D numerical investigation on supersonic combustion of hydrogen in two different type of scramjet combustor[J].Journal of Aerospace Power,2008,23(3):470-475.(in Chinese)
[5]	刘娟,潘余,刘卫东,等.超燃冲压发动机燃烧室中双凹腔对引导氢分布的影响[J].国防科技大学学报,2009,31(2):5-9. LIU Juan,PAN Yu,LIU Weidong,et al.The influence of dual-cavity on pilot hydrogen distribution in scramjet combustor[J].Journal of National University of Defense Technology,2009,31(2):5-9.(in Chinese)
[6]	Cyrus B M, Erik P. Pioneering turbojet developments of Dr. Hans Von Ohain-from the HeS 1 to the HeS 011[J].Journal of Engineering for Gas Turbines and Power, 2000, 122(2):191-201.
[7]	Conrad E W.Turbine engine altitude chamber and flight testing with liquid hydrogen.NASA-TM-79196,1979.
[8]	Sosounov V,Orlov V.Experimental turbofan using liquid hydrogen and liquid natural gas as fuel.AIAA 90-2421,1990.
[9]	Brewer G D.The prospects for liquid hydrogen fuelled aircraft[J].International Journal of Hydrogen Energy,1981,7(1):21-41.
[10]	Drolet B,Gretz J,Kluyskens D,et al.The euro-québec hydro-hydrogen pilot project (EQHHPP):demonstration phase[J].International Journal of Hydrogen Energy,1996,21(4):305-316.
[11]	Susanne M,Robert S,Michael P,et al.Estimate of the climate impact of cryoplanes[J].Aerospace Science Technology,2001,5(1):73-84.
[12]	Ponater M,Marquart S,Strm L.On the potential of the cryoplane technology to reduce aircraft climate impact //Proceedings of the AAC-Conference.Friedrichshafen,Germany:Institute of Electrical and Electronics Engineers Inc.,2003:316-321.
[13]	Charles W F.Future hydrogen markets for large-scale hydrogen production systems[J].International Journal of Hydrogen Energy,2007,32(4):431-439.
[14]	Michael,Susanne P,Robert S,et al.Potential of the cryoplane technology to reduce aircraft climate impact:a state-of-the-art assessment[J].Atmospheric Environment,2006,40(36):6928-6944.
[15]	Andreas W.Hydrogen fuelled aircraft.AIAA-2003-2880,2003.
[16]	Klug H G,Faass R.Cryoplane:hydrogen fuelled aircraft-status and challenges[J].Air & space Europe,2001,3(3-4):252-254.
[17]	Boggia S,Jackson A.Some unconventional aero gas turbines using hydrogen fuel.GT-2002-30412,2002.
[18]	Corchero G,Montanes J L.An approach to the use of hydrogen in actual commercial aircraft engines[J].Journal of Aerospace Engineering,2005,219(1):35-44.
[19]	Haglind F,Singh R.Design of aero gas turbines using hydrogen[J].Journal of Engineering for Gas Turbines and Power,2005,128(4):754-764.
[20]	Haglind F,Hasselrot A,Singh R.Potential of reducing the environmental impact of aviation by using hydrogen Part Ⅰ:background,prospects and challenges[J].The Aeronautical Journal,2006,110:533-540.
[21]	Haglind F,Hasselrot A,Singh R.Potential of reducing the environmental impact of aviation by using hydrogen Part Ⅱ:aero gas turbine design[J].The Aeronautical Journal,2006,110:541-552.
[22]	Lefebvre A H.Gas turbine combustion[M].New York:Taylor & Francis Ltd.,1999.
[23]	Ziemann J,Shum F,Moore M.Low-NO_x combustors for hydrogen fuelled aero engine[J].International Journal of Hydrogen Energy,1998,23(4):281-288.
[24]	Dahl G,Suttrop F.Combustion chamber and emissions,the micromix hydrogen combustor technology.Task Technical Report 4.4-5A,CRYOPLANE Project,2001.
[25]	John M C,Timothy D S,Krishna K.Low emission hydrogen combustors for gas turbines using lean direct injection.AIAA-2005-3776,2005.