[1] BUNKER R S. Evolution of turbine cooling[C]//Proceedings of ASME Turbo Expo 2017:Turbomachinery Technical Conference and Exposition. Charlotte, USA:ASME, 2017.
[2] OWEN J M. Air-cooled gas-turbine discs:A review of recent research[J]. International Journal of Heat and Fluid Flow, 1988, 9(4):354-365.
[3] HAN J C. Turbine blade cooling studies at Texas A&M University:1980-2004[J]. Journal of Thermophysics and Heat Transfer, 2006, 20(2):161-187.
[4] EKKAD S V, HAN J C, DU H. Detailed film cooling measurements on a cylindrical leading edge model:Effect of free-stream turbulence and coolant density[J]. Journal of Turbomachinery, 1998, 120(4):799-807.
[5] TENG S Y, HAN J C, POINSATTE P E. Effect of film-hole shape on turbine-blade heat-transfer coefficient distribution[J]. Journal of Thermophysics and Heat Transfer, 2001, 15(3):249-256.
[6] HUANG Y Z, EKKAD S V, HAN J C. Detailed heat transfer distributions under an array of orthogonal impinging Jets[J]. Journal of Thermophysics and Heat Transfer, 1998, 12(1):73-79.
[7] LIU Z, FENG Z P. Numerical simulation on the effect of jet nozzle position on impingement cooling of gas turbine blade leading edge[J]. International Journal of Heat and Mass Transfer, 2011, 54(23-24):4949-4959.
[8] 韩昌, 迟重然, 尹洪, 等. 燃气轮机一级透平动静叶交互作用的气膜非定常特性及泛冷却效应:Part 1-静叶栅[J]. 工程热物理学报, 2013, 34(5):845-848. HAN C, CHI Z R, YIN H, et al. Unsteady characteristic of film cooling and phantom cooling on the first stage of a gas turbine:Part 1-vane cascade[J]. Journal of Engineering Thermophysics, 2013, 34(5):845-848. (in Chinese)
[9] 胥蕊娜, 李晓阳, 廖致远, 等. 航天飞行器热防护相变发汗冷却研究进展[J]. 清华大学学报(自然科学版), 2021, 61(12):1341-1352.XU R N, LI X Y, LIAO Z Y, et al. Research progress in transpiration cooling with phase Change[J]. Journal of Tsinghua University (Science and Technology), 2021, 61(12):1341-1352. (in Chinese)
[10] 尹洪, 王文萍, 任静, 等. 燃烧室出口辐射对气膜冷却传热影响研究[J]. 工程热物理学报, 2012, 33(2):214-217. YIN H, WANG W P, REN J, et al. Research on the effect of combustor outlet radiation on the film cooling heat transfer[J]. Journal of Engineering Thermophysics, 2012, 33(2):214-217. (in Chinese)
[11] 吴宏超, 袁浩, 魏佳明, 等. 增材制造在燃气轮机研发及生产中的应用[J]. 航空动力, 2020(2):26-28. WU H C, YUAN H, WEI J M, et al. The application of addictive manufacturing technology in gas turbine research, development and manufacture[J]. Aerospace Power, 2020(2):26-28. (in Chinese)
[12] 徐文涛. 增材制造在燃气轮机中的应用[J]. 燃气轮机技术, 2017, 30(3):61-64. XU W T. Application of additive manufacturing in the manufacture of gas turbine[J]. Gas Turbine Technology, 2017, 30(3):61-64. (in Chinese)
[13] 中国航天. 西门子3D打印涡轮机叶片成功通过1 250℃、13 000 转/分的测试[EB/OL]. (2017-02-07). http://www.njszzn.com/content.php?catid=11&id=458.
[14] 杨力. 基于冲击的燃气轮机透平叶片冷却结构研究[D]. 北京:清华大学, 2015. YANG L. Research on the application of impingement cooling in gas turbineblades[D]. Beijing:Tsinghua University, 2015. (in Chinese)
[15] TALLMAN J A, OSUSKY M, MAGINA N, et al. An assessment of machine learning techniques for predicting turbine airfoil component temperatures, using FEA simulations for training data[C]//Proceedings of ASME Turbo Expo 2019:Turbomachinery Technical Conference and Exposition. Phoenix, USA:ASME, 2019.
[16] MILANI P M, LING J L, EATON J K. Generalization of machine-learned turbulent heat flux models applied to film cooling flows[J]. Journal of Turbomachinery, 2020, 142(1):011007.
[17] MORET M, DELECOURT A, MOUSTAPHA H, et al. Automated thermal and stress preliminary analyses applied to a turbine rotor[C]//Proceedings of ASME Turbo Expo 2016:Turbomachinery Technical Conference and Exposition. Seoul, South Korea:ASME, 2016.
[18] WEAR J D, TROUT A M, SMITH J M, et al. Design and preliminary results of a semitranspiration cooled (Lamilloy) liner for a high-pressure high-temperature combustor[C]//Proceedings of the 14th Joint Propulsion Conference. Las Vegas, USA:AIAA, 1978. DOI:10.2514/6.1978-997.
[19] BUNKER R S. Cooling for double-wall structures:6000908[P]. 1999-12-14.
[20] VANDERVAART P L, RHODES J F, KWON O, et al. Cooled gas turbine engine component:20150016944[P]. 2015-01-15.
[21] 李佳. 燃气轮机透平气膜冷却机理的实验与理论研究[D]. 北京:清华大学, 2011. LI J. Experimental and theoretical research on gas turbine film cooling[D]. Beijing:Tsinghua University, 2011. (in Chinese)
[22] 韩昌. 燃气轮机高温透平气膜冷却的孔型机理及叶栅特性研究[D]. 北京:清华大学, 2014. HAN C. Research on film-hole mechanism and cascade characteristics of gas turbine film cooling[D]. Beijing:Tsinghua University, 2014. (in Chinese)
[23] 李雪英. 气膜冷却各向异性湍流场中流动传热的相互作用机理研究[D]. 北京:清华大学, 2013. LI X Y. Research on the mechanism of flow and heat transfer interaction in anisotropic turbulent film cooling flows[D]. Beijing:Tsinghua University, 2013. (in Chinese)
[24] 秦晏旻. 透平叶栅环境下气膜冷却流动传热机理研究[D]. 北京:清华大学, 2015. QIN Y M. Heat transfer and aerodynamic characteristics of film cooling under turbine flow condition[D]. Beijing:Tsinghua University, 2015. (in Chinese)
[25] 王文萍. 燃气轮机高温部件对流/导热/辐射耦合的流动传热机理研究[D]. 北京:清华大学, 2012. WANG W P. Research on flow and heat transfer mechanics at the interaction of conduction, convection and radiation on gas turbine hot component[D]. Beijing:Tsinghua University, 2012. (in Chinese)
[26] 尹洪. 先进燃气轮机燃烧室与透平交互作用的流动传热机理研究[D]. 北京:清华大学, 2014. YI H. Research on the flow and heat trasnfer of combustor-turbine interactionin advanced gas turbine[D]. Beijing:Tsinghua University, 2014. (in Chinese)
[27] 迟重然. 燃气轮机透平冷却结构作用机制与设计优化方法[D]. 北京:清华大学, 2014. CHI Z R. Mechanism and optimization methods of gas turbine cooling structures[D]. Beijing:Tsinghua University, 2014. (in Chinese)
[28] 秦晏旻, 李雪英, 任静, 等. 基于BP神经网络的多参数气膜冷却效率研究[J]. 工程热物理学报, 2011, 32(7):1127-1130. QIN Y M, LI X Y, REN J, et al. Prediction of the adiabatic film cooling effectiveness influnenced by multi parameters based on BP neural network[J]. Journal of Engineering Thermophysics, 2011, 32(7):1127-1130. (in Chinese)
[29] 谭勤学. p型多重网格间断有限元及其在燃机冷却系统中的应用[D]. 北京:清华大学, 2013. TAN Q X. p-multigrid discontinuous finite element method and application for gas turbine's cooling flow[D]. Beijing:Tsinghua University, 2013. (in Chinese)
[30] 王浪. 燃机透平叶片全覆盖气膜冷却特性与优化方法[D]. 北京:清华大学, 2020.WANG L. Characteristics and optimization of the fully coveraged film coolingvanes of gas turbine[D]. Beijing:Tsinghua University, 2020. (in Chinese)
[31] LI W H, LI X Y, YANG L, et al. Effect of Reynolds number, hole patterns, and hole inclination on cooling performance of an impinging jet array-Part I:Convective heat transfer results and optimization[J]. Journal of Turbomachinery, 2017, 139(4):041002. DOI:10.1115/1.4035045.
[32] LI W H, XU M H, REN J, et al. Experimental investigation of local and average heat transfer coefficients under an inline impinging jet array, including jets with low impingement distance and inclined angle[J]. Journal of Heat Transfer, 2017, 139(1):012201. DOI:10.1115/1.4034165.
[33] 任敏, 陆训丰, 李雪英, 等. 冲击冷却结构流动传热特性研究[J]. 工程热物理学报, 2017, 38(7):1577-1582. REN M, LU X F, LI X Y, et al. The flow and heat transfer characteristics of a impinging cooling structure[J]. Journal of Engineering Thermophysics, 2017, 38(7):1577-1582. (in Chinese)
[34] WANG L, LI X Y, REN J, et al. The interaction between upstream and downstream film cooling rows in flow field and heat transfer[J]. International Journal of Thermal Sciences, 2020, 149:106176. DOI:10.1016/j.ijthermalsci.2019.106176.
[35] LI W H, LU X F, LI X Y, et al. High resolution measurements of film cooling performance of simple and compound angle cylindrical holes with varying hole length-to-diameter ratio-Part I:Adiabatic film effectiveness[J]. International Journal of Thermal Sciences, 2018, 124:146-161. DOI:10.1016/j.ijthermalsci.2017.10.013.
[36] LI W H, LU X F, LI X Y, et al. On improving full-coverage effusion cooling efficiency by varying cooling arrangements and wall thickness in double wall cooling application[J]. Journal of Heat Transfer, 2019, 141(4):042201. DOI:10.1115/1.4042772.
[37] LU X F, LI W H, LI X Y, et al. Flow and heat transfer characteristics of micro pin-fins under jet impingement arrays[J]. International Journal of Heat and Mass Transfer, 2019, 143:118416. DOI:10.1016/j.ijheatmasstransfer.2019.07.066.