| Citation: | Influence of fuel stage under idle condition on combustion efficiency for high-temperature rise combustor[J]. Journal of Aerospace Power, 2017, 32(3): 577-583. doi: 10.13224/j.cnki.jasp.2017.03.008
|
| [1] |
Mongia H C.TAPS：a fourth generation propulsion combustor technology for low emissions［R］.AIAA-2003-2657,2003.
|
| [2] |
Stouffer S D,Ballal D R.Development and combustion performance of a high-pressure WSR and TAPS combustor［R］.AIAA-2005-1416,2005.
|
| [3] |
Lazik W,Doerr T,Bake S,et al.Development of lean-burn low-NOx combustion technology at Rolls-Royce Deutschland［R］.ASME Paper 2008-GT-51115,2008.
|
| [4] |
Yamamoto T,Shimodaira K,Krosawa Y,et al.Investigations of a staged fuel atomizer for aeroengines by multi-sector combustor test［R］.ASME Paper 2010-GT-23206,2010.
|
| [5] |
尉曙明.先进燃气轮机燃烧室设计研发［M］.上海:上海交通大学出版社,2014:63-89.
|
| [6] |
程明,尚守堂,刘殿春,等.燃油分级比例对TAPS燃烧室性能的影响［J］.航空发动机,2012,38(4):6-10.CHENG Ming,SHANG Shoutang,LIU Dianchun,et al.Influence of fuel-staging ratio on TAPS combustor performance［J］.Aeroengine,2012,38(4):6-10.(in Chinese)
|
| [7] |
付镇柏,林宇震,张驰,等.中心分级燃烧室进场工况燃油分级方式试验研究［J］.推进技术,2014,35(1):77-86.FU Zhenbo,LIN Yuzhen,ZHANG Chi,et al.Experimental investigation on fuel-staging mode of internally-staged combustor under approach condition［J］.Journal of Propulsion Technology,2014,35(1):77-86.(in Chinese)
|
| [8] |
刘富强,穆勇,刘存喜,等.燃油分级对中心分级燃烧室NOx排放的影响［J］.燃烧科学与技术,2013,19(3):254-260.LIU Fuqiang,MU Yong,LIU Cunxi,et al.Influence of fuel stage proportion on NOx emission from central stage combustor［J］.Journal of Combustion Science and Technology,2013,19(3):254-260.(in Chinese)
|
| [9] |
邓远灏,颜应文,朱嘉伟,等.LPP低污染燃烧室两相喷雾燃烧数值研究［J］.推进技术,2013,34(3):353-361.DENG Yuanhao,YAN Yingwen,ZHU Jiawei,et al.Numerical study of two-phase spray combustion for lean premixed prevaporized low-emission combustor［J］.Journal of Propulsion Technology,2013,34(3):353-361.(in Chinese)
|
| [10] |
徐榕,赵坚行,刘勇,等.TAPS/MLDI 低污染燃烧室油雾特性［J］.航空动力学报,2012,27(11):2421-2428.XU Rong,ZHAO Jianxing,LIU Yong,et al.Fuel spray characteristic of TAPS/MLDI low emission combustor［J］.Journal of Aerospace Power,2012,27(11):2421-2428.(in Chinese)
|
| [11] |
李继保,胡正义.高温升高热容燃烧室设计技术分析［J］.燃气涡轮试验与研究,2000,13(4):5-8.LI Jibao,HU Zhengyi.Design technology for high-temperature rise and high-heat capacity combustor［J］.Gas Turbine Experiment and Research,2000,13(4):5-8.(in Chinese)
|
| [12] |
Lefebvre A H.Fuel effects on gas turbine combustion:ignition,stability,and combustion efficiency［J］.Journal of Engineering for Gas Turbine and Power,1984,107(1):23-37.
|
| [13] |
《航空发动机设计手册》总编委会.航空发动机设计手册:第9册 主燃烧室设计［M］.北京:航空工业出版社,2000:189-190.
|
| [14] |
房人麟,邱伟,徐兵,等.一种富油直混分区燃烧室:中国,CN201320809412.0［P］.2014-08-06.
|
| [15] |
钟华贵,吉洪湖,李继保.燃气分析测量高温燃气温度的方法［J］.航空动力学报,2005,20(3):460-466.ZHONG Huagui,JI Honghu,LI Jibao.Methods for gas temperature measurement by gas analysis［J］.Journal of Aerospace Power,2005,20(3):460-466.(in Chinese)
|
| [16] |
《航空发动机设计手册》总编委会.航空发动机设计手册:第1册 通用基础［M］.北京:航空工业出版社,2000:621-622.
|
| [17] |
林启勋.热工与气动参数测量［M］.西安:西北工业大学出版社,1995:6-7.
|
| [18] |
International Civil Aviation Organization.International standards and recommended practices:environmental protection,annex 16-to the convention on international civil aviation:Volume Ⅱ aviation engine emissions［M］.3rd ed.Montreal:International Civil Aviation Organization,2008.
|
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