冯冲,祁海鹰,谢刚,等.干式低NOx燃气轮机燃烧室的燃料/空气预混均匀性问题分析[J].中国电机工程学报,2011,31(17):9-19.Feng Chong,Qi Haiying,Xie Gang,et al. Analysis on the issue of fuel/air premixing uniformity of the dry low NOx gas turbine combustor[J].Proceedings of the CSEE,2011,31(17):9-19(in Chinese).
[2]
汪凤山.低NOx排放微型燃气轮机燃烧室的数值模拟及实验研究[D].北京:中国科学院研究生院,工程热物理研究所,2009.Wang Fengshan.,Numerical and experimental inveatigation on a low NOx emission combustor for micro gas turbine[D].Beijing:Institute of Engineering Thermophysics,Chinese Academy of Sciences,2009(in Chinese).
[3]
陆伟,张士杰,肖云汉.燃气轮机与燃气内燃机在联供系统中的应用比较[J].工程热物理学报,2008,29(6):905-910.Lu Wei,Zhang Shijie,Xiao Yunhan.Comparison of the application in CCHP between gas turbine and gas engine[J].Journal of Engineering Thermophysics,2008,29(6):905-910(in Chinese).
[4]
王振铭.我国天然气分布式能源站的发展与建议[J].热电技术.2011,109(1):65-70.Wang Zhenming.Development and suggestions of the natural gas based distributed energy station in China [J].Cogeneration Power Technology,2011,109(1):65-70(in Chinese).
[5]
国家发展改革委.关于发展天然气分布式能源的指导意见[EB/OL].http://www.mof.gov.cn/zhengwuxinxi/ hengcefabu/201110/t20111018_600273.htm. National development and reform commission[EB/OL].On the development of natural gas distributed energy guidance[EB/OL](in Chinese).
[6]
Martin Kautz,lf Hansen.The externally-fired gas- turbine(EFGT-cycle) for decentralized use of biomass [J].Applied Energy,2007(84):795-805.
[7]
Zhang Xiaosong,Han Wei,Hong Hui,et al.A chemical inter cooling gas turbine cycle with chemical-looping combustion[J].Energy,2009(34):2131-2136.
[8]
张昊,朱民,张志军.分级预混燃烧的稳定性[J].动力工程,2006,26(2):221-228.Zhang Hao,Zhu Min,Zhang Zhi-jun.Stability of staged premixed combustion[J].Journal of Power Engineering,2006,26(2):221-228(in Chinese).
[9]
刘富强,穆勇,房爱兵,等.双级旋流环形燃烧室流场的数值分析与试验研究[J].中国电机工程学报,2012,32(15):28-36.Liu Fuqiang,Mu Yong,Fang Aibing,et al. Numerical analysis and experiment research on flow field of an annular combustor with a dual-stage swirler [J].Proceedings of the CSEE,2012,32(15):28-36(in Chinese).
崔玉峰,吕煊,徐纲,等.无焰燃烧模型燃烧室动态特性分析[J].中国科学,2010,40(9):1044-1051.Cui Yu Feng,Lü Xuan,Xu Gang,et al.Dynamic analysis of a flameless combustion model combustor[J]. Science China Technological Sciences,2010,40(9):1044-1051.
[12]
Paubel X,Cessou A,Honore D,et al.A flame stability diagram for piloted non-premixed oxycombustion of low calorific residual gases[J].Proceedings of the Mbustion Nstitute,2007(31):3385-3392.
[13]
Gimenez-Lopez J,Aranda V,Millera A,et al.An experimental parametric study of gas reburning under conditions of interest for oxy-fuel combustion[J].Fuel Processing Technology,2011(92):582-589.
[14]
Li Hailong,Mario Ditaran.David Berstad. Technologies for increasing CO2 concentration in exhaust gas from natural gas-fired power production with post-combustion,amine-based CO2 capture[J].Energy,2011(36) 1124-1133.
[15]
世界燃气轮机手册编委会.世界燃气轮机手册[M].北京:航空工业出版社,2011:7.The Gas Turbine Handbook Editorial Board.Gas turbine handbook[M].Beijing:Aviation Industry Press,2011:7 (in Chinese).
钟芳源.燃气轮机设计基础[M].北京:机械工业出版社,1985:6.Zhong Fangyuan.Design basis of gas turbine [M].Beijing:China Machine Press,1985:6(in Chinese).
[18]
金如山.航空燃气轮机燃烧室[M].北京:宇航出版社,1988:2.Jin Rushan.Aviation gas turbine combustor[M].Beijing:China Astronautic Publishing House,1988:2(in Chinese).
[19]
崔玉峰,徐纲,田学清,等.燃气轮机燃烧室进气孔流量系数的数值模拟[J].航空动力学报,2005,20(2): 192-196.Cui Yufeng,Xu Gang,Tian Xueqing,et al.Numerical simulation studies on the discharge coefficient of gas turbine combustor liner air holes[J].Journal of Aerospace Power,2005,20(2):192-196(in Chinese).
[20]
Bahr D W,Scabla P F,Vinson J W.Small industrial gas turbine combustor performance with low BTU gas fuels[C]//International Conference on Gas Turbine Symposium and Exposition,Beijing,1985.
[21]
崔玉峰,徐纲,聂超群,等.数值模拟在合成气燃气轮机燃烧室设计中的应用[J].中国电机工程学报,2006,26(16):109-116.Cui Yufeng,Xu Gang,Nie Chaoqun,et al. Application of numerical simulation in the design of gas turbine combustor for burning syngas[J].Proceedings of the CSEE,2006,26(16):109-116(in Chinese).
[22]
Boudier G,Gicquel L Y M,Poinsot T,et al.Comparison of LES,RANS and experiments in an aeronautical gasturbine combustion chamber[J]. Proceedings of the Combustion Institute,2007(31):3075-3082.
[23]
王飞,雷勇,杨华.航空发动机燃烧室喷油环三维流场数值模拟[J].航空动力学报,2007(22).1439-1443.Wang Fei,Lei Yong,Yang Hua.Numerical simulation of 3-D flow field in an aeroengine combustor nozzle-loop [J].Journal of Aerospace Power,2007(22):1439-1443(in Chinese).
[24]
胡好生,蔡文祥,赵坚行,等.回流燃烧室燃烧过程的三维数值模拟[J].航空动力学报,2008(23):454-459.Hu Haosheng,Cai Wenxiang,Zhao Jianxing,et al.Numerical simulation of three-dimensional combustion flows in annular reversed combustor[J].Journal of Aerospace Power,2008(23):454-459(in Chinese).
[25]
赵晓燕,李祥晟,丰镇平.燃气轮机低热值合成气燃烧室内三维湍流流动的数值模拟研究[J].动力工程,2009(29):330-335.Zhao Xiaoyan,Li Xiangsheng,Feng Zhenping.Numerical simulation research on three dimensional turbulence flow in a gas turbine combustor burning low heat value syngas [J].Journal of Power Engineering,2009(29):330-335(in Chinese).
[26]
韩昭沧.燃料及燃烧 [M].2版.北京:冶金工业出版社,2007:10.Hang Zhaocang.Fuel and combustion [M]. 2nd Edition.Beijing:Metallurgical Industry Press,2007:10(in Chinese).