刘尚明,魏成亮,蒲星星,等.一种计算燃气轮机透平叶片温度分布和冷却空气需求量的修正的解析模型[J].中国电机工程学报,2012,32(14):88-94.Liu Shangming,Wei Chengliang,Pu Xingxing,et al.A modified analytical model to calculate temperature distribution of gas turbine blade and the cooling air required[J].Proceedings of the CSEE,2012,32(14):88-94(in Chinese).
[2]
王晋声,罗磊,崔涛,等.燃气涡轮导叶冷却结构设计及数值模拟[J].中国电机工程学报,2014,34(5):800-807.Wang Jinsheng,Luo Lei,Cui Tao,et al.Cooling structure design and numerical simulation in gas turbine guide vane[J].Proceedings of the CSEE,2014,34(5):800-807(in Chinese).
[3]
虞跨海,杨茜,罗昌金,等.涡轮叶片二维冷却结构参数化设计技术研究[J].燃气涡轮试验与研究,2013,26(1):12-15.Yu Kuahai,Yang Xi,Luo Changjin,et al.Parametric design method of 2D turbine blade cooling structure [J].Gas Turbine Experiment and Research,2013,26(1):12-15(in Chinese).
[4]
韩绪军.涡轮叶片冷却结构参数化及带肋通道优化设计[D].哈尔滨:哈尔滨工业大学,2011.Han Xujun.Parametric expression of cooling structure of turbine blade and the optimization design of channels with ribs[D].Harbin:Harbin Institute of Technology,2011(in Chinese).
[5]
呼艳丽.高效涡轮铸冷工作叶片冷却设计[D].成都:电子科技大学,2010.Hu Yanli.Cooling design for high efficiency cast-cooling turbine blade[D].Chengdu:University of Electronic Science and Technology of China,2010(in Chinese).
[6]
于飞龙.低压涡轮动叶冷却结构的改进研究[D].哈尔滨:哈尔滨工程大学,2013.Yu Feilong.Improvement research of cooling structure in low pressure turbine blade[D].Harbin:Harbin Engineering University,2013(in Chinese).
[7]
孙纪宁,邓晶,邓宏武.涡轮叶片微小通道气膜新型复合冷却结构设计[J].北京航空航天大学学报,2012,38(5):702-706.Sun Jining,Deng Jing,Deng Hongwu.Structure design of a new cooling system combined micro channel and film cooling in the turbine blade[J].Journal of Beijing University of Aeronautics and Astronautics,2012,38(5):702-706(in Chinese).
[8]
李少华,朱励,李延臣,等.多孔气膜冷却纵向耦合涡的数值模拟[J].中国电机工程学报,2009,29(8):55-59.Li Shaohua,Zhu Li,Li Yanchen,et al.Numerical simulation in lengthways coupled-vortex of multiple holes[J].Proceedings of the CSEE,2009,29(8):55-59(in Chinese).
[9]
姚建辉.低压涡轮叶片冷却结构优化设计[D].哈尔滨:哈尔滨工程大学,2013.Yao Jianhui.Optimization design of cooling structure in low pressure turbine blade[D].Harbin:Harbin Engineering University,2013(in Chinese).
[10]
戴萍,林枫.不同孔形气膜冷却效率的数值模拟[J].中国电机工程学报,2010,30(14):102-108.Dai Ping,Lin Feng.Numerical simulation on film cooling effectiveness for different shaped holes[J].Proceedings of the CSEE,2010,30(14):102-108(in Chinese).
[11]
王松涛,迟重然,温风波,等.涡轮动叶冷却结构设计方法I:参数化设计[J].工程热物理学报,2011,32(4):581-584.Wang Songtao,Chi Zhongran,Wen Fengbo,et al.Cooling structure design for turbine blades I:parameterized design[J].Journal of Engineering Thermophysics,2011,32(4):581-584(in Chinese).
[12]
迟重然,温风波,王松涛,等.涡轮动叶冷却结构设计方法II-管网计算[J].工程热物理学报,2011,32(6):933-936.Chi Zhongran,Wen Fengbo,Wang Songtao,et al.Cooling structure design for turbine blades II:pipe-net calculation [J].Journal of Engineering Thermophysics,2011,32(6):933-936(in Chinese).
[13]
迟重然.气冷涡轮叶片的传热设计[D].哈尔滨工业大学,2011.Chi Zhongran.Heat transfering design for air-cooled turbine blades[D].Harbin:Harbin Institute of Technology,2011(in Chinese).
[14]
Jen H F,Sobanik J B.Cooling air flow characteristics in gas turbine components[J].Journal of Engineering for Power,1982,104(2):275-280.
[15]
Timko L P.Energy efficient engine high pressure turbine component test performance report[R].Washington,DC:National Aeronautics and Space Administration,1990.
[16]
Sridhar M,Sunnam S,Goswami S,et al.CFD aerodynamic performance validation of a two-stage high pressure turbine[R].Vancouver,British Columbia,Canada:ASME,2011.
[17]
董平.航空发动机气冷涡轮叶片的气热耦合数值模拟研究[D].哈尔滨:哈尔滨工业大学,2009.Dong Ping.Research on conjugate heat transfer simulation of aero turbine engine air-cooled vane[D].Harbin:Harbin Institute of Technology,2009(in Chinese).
[18]
Boyce M P.Gas turbine engineering handbook[M].2nd Edition.Oxford:Elsevier,2002:351-352.
[19]
孙启超.层板结构内部流动与换热特性研究[D].南京:南京航空航天大学,2012.Sun Qichao.Investigation on flow and heat transfer of the internal characteristics with lamilloy board[D].Nanjing:Nanjing University of Aeronautics and Astronautics,2012(in Chinese).
[20]
Ekkad S V,Han J C.Detailed heat transfer distributions in two-pass square channels with rib turbulators [J].International Journal of Heat and Mass Transfer,1997,40(11):2525-2537.
[21]
Han J C,Dutta S,Srinath V E.Gas turbine heat transfer and cooling technology[M].New York:Taylor & Francis,2000.
[22]
刘湘云,丁水汀,陶智,等.不同肋间距变截面回转通道内的流阻和换热特性[J].航空动力学报,2004,19(5):640-644.Liu Xiangyun,Ding Shuiting,Tao Zhi,et al.Characteristic of flow resistance and heat transfer in a turnover variable cross-section channel with different rib pitches[J].Journal of Aerospace Power,2004,19(5):640-644(in Chinese).
[23]
戚磊,丁水汀,徐国强,等.带肋变截面回转通道内换热特性的实验研究[J].航空动力学报,2003,18(5):629-633.Qi Lei,Ding Shuiting,Xu Guoqiang,et al.An experimental study of flow performance in a 180° turn-over channel with ribs[J].Journal of Aerospace Power,2003,18(5):629-633(in Chinese).
[24]
马世岩,徐国强,邓宏武,等.微小通道在叶片冷却结构中的应用研究[J].航空动力学报,2009,24(9):1989-1993.Ma Shiyan,Xu Guoqiang,Deng Hongwu,et al.Research on application of micro channel in the blade cooling structure[J].Journal of Aerospace Power,2009,24(9):1989-1993(in Chinese).