| Citation: | MAO Yan-hui, YANG Jin-hu, LIU Cun-xi, MU Yong, LIU Fu-qiang, XU Gang. Performance comparison and analysis of high temperature rise combustor engine and two-combustor engine[J]. Journal of Aerospace Power, 2013, 28(3): 673-680.
|
| [1] |
Bahr D W.Technology for the design of high temperature rise combustor[R].AIAA 85-1292,1985.
|
| [2] |
林宇震,许全宏,刘高恩.燃气轮机燃烧室[M].北京:国防工业出版社,2006.
|
| [3] |
许全宏,林宇震,刘高恩,等.航空发动机高温升燃烧室贫油熄火及冒烟性能研究[J].航空动力学报,2005,20(4):636-640. XU Quanhong,LIN Yuzhen,LIU Gaoen,et al.Research on the high temperature rise combustor lean blow-out and smoke emission characteristics[J].Journal of Aerospace Power,2005,20(4):636-640.(in Chinese)
|
| [4] |
黎明,吴二平,唐明.高温升蒸发型双腔燃烧室的设计[J].推进技术,2010,31(4):418-422. LI Ming,WU Erping,TANG Ming.Design of vaporing combustor with double chambers and high temperature rise[J].Journal of Propulsion Technology,2010,31(4):418-422.(in Chinese)
|
| [5] |
彭云晖,刘旦,林宇震.高温升燃烧室主燃区流场和燃烧性能[J].燃烧科学与技术,2010,16(5):456-461. PENG Yunhui,LIU Dan,LIN Yuzhen.Primary zone flow field and combustion performance of high temperature rise combustor[J].Journal of Combustion Science and Technology,2010,16(5):456-461.(in Chinese)
|
| [6] |
Zhang R C,Fan W J.The design and performance of a high temperature rise combustor for wind tunnel[J].Journal of Thermal Science,2011,20(6):556-562.
|
| [7] |
Sirignano W A,Delplanque J P,Liu F.Selected challenges in jet and rocket engine combustion research[R].AIAA 97-2701,1997.
|
| [8] |
Lee A S,Singh R,Probert S D.Performances of a two-combustor turbofan engine under design and off-design conditions[R].AIAA-2008-4901,2008.
|
| [9] |
Liu F,Sirignano W A.Turbojet and turbofan engine performance increase through turbine burners[R].AIAA-2000-0741,2000.
|
| [10] |
Liew K H,Urip E,Yang S L.A parametric cycle analysis of a separate-flow turbofan with inter-stage turbine burner[R].NASA/CR-2005-213657,2005.
|
| [11] |
孙泽晖,蔡元虎.带混排涡轮级间燃烧的涡扇发动机循环参数[J].推进技术,2010,31(2):139-142. SUN Zehui,CAI Yuanhu.Parametric cycle analysis of mixed exhaust turbofan with inter stage turbine burner[J].Journal of Propulsion Technology,2010,31(2):139-142.(in Chinese)
|
| [12] |
Zelina J,Ehret J,Hancock R D.Ultra-compact combustor combustion technology using high swirl for enhanced burning rate[R].AIAA-2002-3725,2002.
|
| [13] |
Thornburg H,Sekar B,Zelina J.Geometrical parametric studies of inter-turbine burner for improved performance[R].AIAA-2007-5099,2007.
|
| [14] |
金如山,索建秦.先进加力燃烧室技术发展[R].北京:中国航空学会第七届动力年会,2010.
|
| [15] |
张宝诚.航空发动机试验和测试技术[M].北京:北京航空航天大学出版社,2005.
|
| [16] |
Chen G,Hoffman M A,Davis R L.Gas turbine performance improvement through the use of multiple turbine inter-stage burners[J].Journal of Propulsion and Power,2004,20(5):828-834.
|
| [17] |
廉筱纯,吴虎.航空发动机原理[M].西安:西北工业大学出版社,2005.
|
| [18] |
毛艳辉,刘存喜,刘富强,等.级间燃烧室在航空发动机上应用分析[J].航空动力学报,2012,27(3):578-587. MAO Yanhui,LIU Cunxi,LIU Fuqiang,et al.Application analysis of inter stage turbine burner of aero engine[J].Journal of Aerospace Power,2012,27(3):578-587.(in Chinese)
|
| [19] |
彭泽琰,刘刚,桂幸民,等.航空燃气轮机原理[M].北京:国防工业出版社,2008.
|
DownLoad: