| Citation: | XIE Fa, ZHANG Shan-shan, JIANG Hong-de. Effects of inlet flow parameters oscillation on combustion instability of gas turbine combustor[J]. Journal of Aerospace Power, 2015, 30(7): 1561-1565. doi: 10.13224/j.cnki.jasp.2015.07.004
|
| [1] |
Lefebvre A H.Gas turbine combustion[M].Phiadelphia,US:Taylor and Francis,1999.
|
| [2] |
焦树建.燃气轮机燃烧室[M].北京:机械工业出版社,1988.
|
| [3] |
Mellor A M.Design of modern turbine combustors[M].New York:Academic Press,1990.
|
| [4] |
Imamura A,Yoshida M.Research and development of a LPP combustor with swirling flow for low NOx[R].AIAA-2001-3311,2001.
|
| [5] |
Marek C J,Smith T D.Low emission hydrogen combustors for gas turbines using lean direct injection[R].AIAA-2005-3776,2005.
|
| [6] |
Robert T,Mao C P,Changlie W.Experimental investigation of a multiplex fuel injector module for low emission combustors[R].AIAA-2003-0827,2003.
|
| [7] |
Davis L B,Black S H.Dry low NOx combustion systems for GE heavy-duty gas turbines[R].New York:GE Power Systems GER-3568G,1996.
|
| [8] |
Tanaka K,Nishida K,Akizuki W.Gas turbine combustor technology contributing to environmental conservation[J].Mitsubishi Heavy Industries Technical Review,2009,46(2):6-12.
|
| [9] |
赵巍.燃气轮机干式低污染燃烧室的设计研究[D].上海:上海发电设备成套设计研究所,2003. ZHAO Wei.Investigation of dry low emission gas turbine combustion chamber[D].Shanghai:Shanghai Power Equipment Research Institute,2003.(in Chinese)
|
| [10] |
XIE Fa,HUANG Yong,HU Bin,et al.Improved semiempirical correlation to predict lean blowout limits for gas turbine combustors[J].Journal of Propulsion and Power,2012,28(1):197-203.
|
| [11] |
谢法,黄勇,苗辉,等.气量分配对轴径向旋流器燃烧室贫熄边界的影响[J].航空动力学报,2011,26(8):1756-1760. XIE Fa,HUANG Yong,MIAO Hui,et al.Effects of airflow split and primary holes arrangement on the lean blowout limits of a combustor with axial-radial swirl cup[J].Journal of Aerospace,2011,26(8):1756-1760.(in Chinese)
|
| [12] |
Abdulsada M.Flashback and blowoff characteristics of gas turbine swirl combustor[D].Cardiff,UK:Cardiff University,2011.
|
| [13] |
房爱兵.燃气轮机合成气燃烧室燃烧稳定性的实验研究[D].北京:中国科学院,2007. FANG Aibing.Investigation of combustion instability in syngas combustor of gas turbine[D].Beijing:Chinese Academy of Sciences,2007.(in Chinese)
|
| [14] |
郭志辉,王帅,李磊,等.贫燃预混旋流火焰燃烧不稳定性的实验[J].航空动力学报,2009,24(12):2637-2642. GUO Zhihui,WANG Shuai,LI Lei,et al.Experimental study on combustion instability of lean premixed swirl flame[J].Journal of Aerospace Power,2009,24(12):2637-2642.(in Chinese)
|
| [15] |
Lee H J.Combustion instability mechanisms in a lean premixed gas turbine combustor[D].Phiadelphia,US:Pennsylvania State University,2009.
|
| [16] |
Zukoski E E.Afterburners[M]//Oates G C.Aerothermodynamics of aircraft engine components.New York:AIAA,1985:45-144.
|
| [17] |
云竹士.Chemkin基础培训资料[EB/OL].[2013-01-07]. http://wenku.baidu.com/view/66af971f5f0e7cd1842536c2.html.
|
| [18] |
李卓毅,张会强.甲烷一维层流预混火焰的详细和单步反应机理模拟[J].清华大学学报:自然科学版,2005,45(11):1510-1512,1517. LI Zhuoyi,ZHANG Huiqiang.Numerical simulations of one-dimensional laminar premixed CH4/air flames using the detailed and one-step reaction mechanisms[J].Journal of Tsinghua University:Science and Technology,2005,45(11):1510-1512,1517.(in Chinese)
|
| [19] |
Lieuwen T C,Neumeier Y,Zinn B T.The role of unmixedness and chemical kinetics in driving combustion instabilities in lean premixed combustors[J].Combustion Science and Technology,1998,135(1):193-211.
|
| [20] |
Lieuwen T C.Investigation of combustion instability mechanisms in premixed gas turbine combustors[D].Atlanta:Georgia Institute of Technology,1999.
|
DownLoad: