Microcircuit cooling for gas turbine engine combustor

• 1. 冷却燃气涡轮发动机燃烧室的装置 [P] . 中国专利： CN100353117C . 2007.12.05
• 2. 冷却燃气涡轮发动机燃烧室的方法和装置 [P] . 中国专利： CN1576544A . 2005-02-09
• 3. METHOD FOR COOLING A MICROCIRCUIT OF A BLADE OF A GAS TURBINE ENGINE COMPOSED OF A FAN, A COMPRESSOR, A COMBUSTOR, A TURBINE AND A NOZZLE [P] . 韩国专利： KR20050018594A . 2005-02-23

  机译： 冷却由风扇，压缩机，燃烧器，涡轮和喷嘴组成的燃气轮机叶片的微循环的方法

• 4. Microcircuit cooling for gas turbine engine combustor [P] . 美国专利： US10094563B2 . 2018-10-09

  机译： 燃气涡轮发动机燃烧室的微回路冷却

• 5. Microcircuit cooling for gas turbine engine combustor [P] . 欧洲知识产权局专利： EP2551592A3 . 2017-05-17

  机译： 燃气涡轮发动机燃烧室的微回路冷却

• 1. NUMERICAL CALCULATIONS OF GASEOUS REACTING FLOWS IN A MODEL OF GAS TURBINE COMBUSTORS [J] . 中国航空学报：英文版 . 1991,第001期
• 2. THREE—DIMENSIONAL GAS TURBINE COMBUSTOR PERFORMANCE MODELING [J] . ZhaoJianxing, ZhouFenglun, LeiYubing 南京航空航天大学学报：英文版 . 2002,第001期
• 3. Gas Turbine Engine Durability Impacts of High Fuel-Air Ratio Combustors: Near Wall Reaction Effects on Film-Cooled Backward-Facing Step Heat Transfer [J] . David W. Milanes, Daniel R. Kirk, Krzysztof J. Fidkowski, Journal of Engineering for Gas Turbines and Power . 2006,第2期
• 4. Gas Turbine Engine Durability Impacts of High Fuel-Air Ratio Combustors―Part Ⅱ: Near-Wall Reaction Effects on Film-Cooled Heat Transfer [J] . D. R. Kirk, G. R. Guenette, S. P. Lukachko, Journal of Engineering for Gas Turbines and Power . 2003,第3期
• 5. Flame-cooling air interaction in an effusion-cooled model gas turbine combustor at elevated pressure [J] . Greifenstein M., Hermann J., Boehm B., Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2019,第1期
• 6. Film-Cooling Techniques at the End of Combustor and Inlet of Turbine in a Gas Turbine Engine: A Review [C] . Nor Azwadi Che Sidik, Ehsan Kianpour World Virtual Conference on Advanced Research in Mechanical and Materials Engineering . 2014
• 7. Experimental Investigation of the Effect of Engine Representative Combustor Exit Temperature Profile and Disc Cavity Leakage Flow on the Film Cooling of Contoured Hub Endwall of a High Pressure Gas Turbine Rotor Cascade. [D] . Ayaskanta, Arya. 2013
• 8. Dispersion of Entropy Perturbations Transporting through an Industrial Gas Turbine Combustor [O] . Yu Xia, Ignacio Duran, Aimee S. Morgans, -1
• 9. Experimental Investigation of the Influence of Combustor Cooling on the Characteristics of a FLOX©-Based Micro Gas Turbine Combustor [O] . Zanger, Jan, Monz, Thomas, Aigner, Manfred 2013
• 10. High-Temperature Turbine-Technology Program. Phase II. Technology Test and Support Studies. Design and Development of a Regeneratively Fuel Cooled High Temperature Gas Turbine Combustor for Operation on Low Btu Gas [R] . Dobson, R. L., Kwan, T. C., Straume, T. 1982

• 1. Energy, Exergy and Thermoeconomics Analysis of Water Chiller Cooler for Gas Turbines Intake Air Cooling [J] . Galal Mohammed Zaki ,Rahim Kadhim Jassim ,Majed Moalla Alhazmy . 智能电网与可再生能源（英文） . 2011,第3期
• 2. Surface Temperatures Determination with Influencing Convective and Radiative Thermal Resistance Parameters of Combustor of Gas Turbine [J] . Ebene Ufot ,Ibiba Emmanuel Douglas ,Howel Iberefata Hart . 工程（英文）（1947-3931） . 2014,第9期
• 3. Development of a micro gas turbine combustor with T-type vaporizers [J] . XU Quan-hong LIU Jun XU Jian LIN Yu-zhen LIU Gao-en . 航空动力学报 . 2007,第7期
• 4. 燃气涡轮发动机低污染燃烧室的发展趋势及思考 [C] . 金捷 ,岳明 . 大型飞机关键技术高层论坛暨中国航空学会2007年年会 . 2007
• 5. 燃气涡轮发动机层板冷却结构涡轮叶片冷却设计与内流试验研究 [A] . 韩嵩 . 2011