| Citation: | ZHANG Shuai, ZENG Jun, FANG Hongyi, et al. Aerodynamic and heat transfer performance measurements for double wall cooled turbine vanes in a hot cascade[J]. Journal of Aerospace Power, 2026, 41（3）：20240308 doi: 10.13224/j.cnki.jasp.20240308
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A hot cascade facility equipped with an annular cascade sector of double wall impinge-ment film cooled vanes of energy effective engine (E3) high pressure turbine was used to determine the local gas side temperature and static pressure simultaneously for inlet gas temperature of
| [1] |
郭文, 吉洪湖, 蔡毅, 等. 复合式气冷涡轮导叶冷却设计与试验[J]. 航空动力学报, 2005, 20(3): 456-459. GUO Wen, JI Honghu, CAI Yi, et al. Design and experimental research of compound air-cooled turbine guide vane[J]. Journal of Aerospace Power, 2005, 20(3): 456-459. (in Chinese
GUO Wen, JI Honghu, CAI Yi, et al. Design and experimental research of compound air-cooled turbine guide vane[J]. Journal of Aerospace Power, 2005, 20(3): 456-459. (in Chinese)
|
| [2] |
吴向宇, 丁新星, 谢建文, 等. 前缘气膜孔布局对涡轮转子叶片流动传热的影响[J]. 航空发动机, 2017, 43(3): 5-9. WU Xiangyu, DING Xinxing, XIE Jianwen, et al. Influence of leading edge film holes layout on turbine rotor blade flow and heat transfer characteristics[J]. Aeroengine, 2017, 43(3): 5-9. (in Chinese
WU Xiangyu, DING Xinxing, XIE Jianwen, et al. Influence of leading edge film holes layout on turbine rotor blade flow and heat transfer characteristics[J]. Aeroengine, 2017, 43(3): 5-9. (in Chinese)
|
| [3] |
JAMES W G. Effects of film injection angle on turbine vane cooling: NASA TP-1095 [R]. Cleveland, US: National Aeronautics and Space Administration, 1977.
|
| [4] |
唐国庆, 黄康才, 薛伟鹏, 超跨声涡轮扇形叶栅试验流场周期性设计 [J]. 燃气涡轮试验与研究, 2018, 31(3): 27-31. TANG Guoqing, HUANG Kangcai, XUE Weipeng. Periodic design of sector cascade test flow field for supersonic and transonic turbine [J]. Gas Turbine Experiment and Research, 2018, 31(3): 27-31. (in Chinese
TANG Guoqing, HUANG Kangcai, XUE Weipeng. Periodic design of sector cascade test flow field for supersonic and transonic turbine [J]. Gas Turbine Experiment and Research, 2018, 31(3): 27-31. (in Chinese)
|
| [5] |
张维涛, 吴佳玉, 曾军, 等. 大尺寸低压涡轮导向叶片冷效试验件设计及验证[J]. 燃气涡轮试验与研究, 2021, 34(4): 18-25. ZHANG Weitao, WU Jiayu, ZENG Jun, et al. Optimization and verification of cooling efficiency test for large-size low pressure turbine vane[J]. Gas Turbine Experiment and Research, 2021, 34(4): 18-25. (in Chinese
ZHANG Weitao, WU Jiayu, ZENG Jun, et al. Optimization and verification of cooling efficiency test for large-size low pressure turbine vane[J]. Gas Turbine Experiment and Research, 2021, 34(4): 18-25. (in Chinese)
|
| [6] |
CHARLES H. Advanced methods for cascade testing: AGARD-AG-328 [R]. Neuilly sur Seine, France: Advisory Group for Aerospace Research and Development, 1993.
|
| [7] |
ZHANG L J, GLEZER B. Turbine airfoil external heat transfer measurement in a hot-cascade [C]// ASME International Gas Turbine & Aeroengine Congress and Exhibition. Orlando, Florida: American Society of Mechanical Engineers, 1997.
|
| [8] |
VENKATASUBRAMANYA S, VASUDEV S A, CHANDEL S. Experimental evaluation of cooling effectiveness of high pressure turbine nozzle guide vane[C]// Proceedings of the ASME 2012 Gas Turbine India Conference. Mumbai, Maharashtra, India: American Society of Mechanical Engineers, 2012.
|
| [9] |
HYLTON L D, MIHELC M S, TURNER E R. Analytical and experimental evaluation of the heat transfer distribution over the surfaces of turbine vanes: NASA-CR-168015 [R]. Cleveland, US: National Aeronautics and Space Administration, 1983.
|
| [10] |
POST J W, ACHARYA S. Temperature and pressure measurements in a hot cascade with film cooled endwalls and airfoils[C]// Proceedings of ASME Turbo Expo 2008: Power for Land, Sea and Air. Berlin, Germany: American Society of Mechanical Engineers, 2008.
|
| [11] |
GLADDEN H J, YEH F C, FRONEK D L. Heat transfer results and operational characteristics of the NASA lewis research center hot section cascade test facility[R]. Houston: American Society of Mechanical Engineers, 1985.
|
| [12] |
VASUDEV S, PRAKASH B, KAUSHAL M. High pressure high temperature static test facility for turbine blade cooling research[J]. AIAA Journal, 2000, 20(3): 456-459.
|
| [13] |
李广超, 莫唯书, 张魏, 等. 涡轮导向叶片综合冷却特性实验研究[J]. 推进技术, 2018, 39(12): 2772-2778. LI Guangchao, MO Weishu, ZHANG Wei, et al. Experimental investigation on integrated cooling performance of nozzle guide vane[J]. Journal of Propulsion Technology, 2018, 39(12): 2772-2778. (in Chinese doi: 10.13675/j.cnki.tjjs.2018.12.016
LI Guangchao, MO Weishu, ZHANG Wei, et al. Experimental investigation on integrated cooling performance of nozzle guide vane[J]. Journal of Propulsion Technology, 2018, 39(12): 2772-2778. (in Chinese) doi: 10.13675/j.cnki.tjjs.2018.12.016
|
| [14] |
姚春意, 朱惠人, 刘存良, 等. 涡轮导叶压力面气膜孔排位置对气膜冷却特性的影响[J]. 推进技术, 2020, 41(7): 1560-1570. YAO Chunyi, ZHU Huiren, LIU Cunliang, et al. Effects of film hole row location on film cooling characteristic for pressure side of a turbine vane[J]. Journal of Propulsion Technology, 2020, 41(7): 1560-1570. (in Chinese
YAO Chunyi, ZHU Huiren, LIU Cunliang, et al. Effects of film hole row location on film cooling characteristic for pressure side of a turbine vane[J]. Journal of Propulsion Technology, 2020, 41(7): 1560-1570. (in Chinese)
|
| [15] |
宣文韬, 钟博, 魏景涛, 等. 涡轮动叶表面换热特性的试验研究[J]. 推进技术, 2022, 43(7): 200843. XUAN Wentao, ZHONG Bo, WEI Jingtao, et al. Experimental research on heat transfer characteristics of turbine blade surface[J]. Journal of Propulsion Technology, 2022, 43(7): 200843. (in Chinese
XUAN Wentao, ZHONG Bo, WEI Jingtao, et al. Experimental research on heat transfer characteristics of turbine blade surface[J]. Journal of Propulsion Technology, 2022, 43(7): 200843. (in Chinese)
|
| [16] |
杨其国, 王祥锋, 石玉文, 等. 高负荷涡轮叶栅气动性能试验[J]. 航空动力学报, 2011, 26(12): 2722-2730. YANG Qiguo, WANG Xiangfeng, SHI Yuwen, et al. Experiment on aerodynamic performance of turbine static cascade with high aerodynamic loading[J]. Journal of Aerospace Power, 2011, 26(12): 2722-2730. (in Chinese
YANG Qiguo, WANG Xiangfeng, SHI Yuwen, et al. Experiment on aerodynamic performance of turbine static cascade with high aerodynamic loading[J]. Journal of Aerospace Power, 2011, 26(12): 2722-2730. (in Chinese)
|
| [17] |
马超, 臧述升, 黄名海. 变几何涡轮动叶栅流场的PIV实验研究[J]. 动力工程学报, 2014, 34(6): 458-462, 481. MA Chao, ZANG Shusheng, HUANG Minghai. PIV flow field measurement for rotor blade cascade of a variable geometry turbine[J]. Journal of Chinese Society of Power Engineering, 2014, 34(6): 458-462, 481. (in Chinese
MA Chao, ZANG Shusheng, HUANG Minghai. PIV flow field measurement for rotor blade cascade of a variable geometry turbine[J]. Journal of Chinese Society of Power Engineering, 2014, 34(6): 458-462, 481. (in Chinese)
|
| [18] |
巩昊, 徐惊雷, 陈宇. 开槽尾流板对跨声速涡轮平面叶栅流场影响的实验[J]. 航空动力学报, 2018, 33(12): 3048-3056. GONG Hao, XU Jinglei, CHEN Yu. Experiment on effects of slotted tailboard on flow field of transonic turbine linear cascade[J]. Journal of Aerospace Power, 2018, 33(12): 3048-3056. (in Chinese
GONG Hao, XU Jinglei, CHEN Yu. Experiment on effects of slotted tailboard on flow field of transonic turbine linear cascade[J]. Journal of Aerospace Power, 2018, 33(12): 3048-3056. (in Chinese)
|
| [19] |
TIMKO L P. Energy efficient engine high pressure turbine component test performance report: NASA CR-168289 [R]. Cleveland, US: National Aeronautics and Space Administration, 1990.
|
| [20] |
周鸿儒, 王振峰, 颜培刚, 等. 具有转捩流动特性的高压燃气气冷涡轮叶栅的气热耦合计算[J]. 航空动力学报, 2010, 25(6): 1221-1226. ZHOU Hongru, WANG Zhenfeng, YAN Peigang, et al. Conjugate heat transfer simulation of a high pressure air-cooled gas turbine with transition flow characteristics[J]. Journal of Aerospace Power, 2010, 25(6): 1221-1226. (in Chinese
ZHOU Hongru, WANG Zhenfeng, YAN Peigang, et al. Conjugate heat transfer simulation of a high pressure air-cooled gas turbine with transition flow characteristics[J]. Journal of Aerospace Power, 2010, 25(6): 1221-1226. (in Chinese)
|
| [21] |
曾军, 张维涛, 王鹏飞, 等. 空心气冷低压涡轮动叶气热耦合数值模拟[J]. 推进技术, 2020, 41(6): 1268-1275. ZENG Jun, ZHANG Weitao, WANG Pengfei, et al. Conjugate heat transfer analysis for cooled low pressure turbine rotor blade[J]. Journal of Propulsion Technology, 2020, 41(6): 1268-1275. (in Chinese doi: 10.13675/j.cnki.tjjs.190395
ZENG Jun, ZHANG Weitao, WANG Pengfei, et al. Conjugate heat transfer analysis for cooled low pressure turbine rotor blade[J]. Journal of Propulsion Technology, 2020, 41(6): 1268-1275. (in Chinese) doi: 10.13675/j.cnki.tjjs.190395
|
| [22] |
曾文演, 乔渭阳, 李文澜. 冷气掺混对涡轮叶栅气动损失影响的试验研究[J]. 机械设计与制造, 2006(10): 91-92. ZENG Wenyan, QIAO Weiyang, LI Wenlan. Experimental study influence of cooling-air injection on the aerodynamic performance of rectangular turbine blade[J]. Machinery Design & Manufacture, 2006(10): 91-92. (in Chinese
ZENG Wenyan, QIAO Weiyang, LI Wenlan. Experimental study influence of cooling-air injection on the aerodynamic performance of rectangular turbine blade[J]. Machinery Design & Manufacture, 2006(10): 91-92. (in Chinese)
|
| [23] |
张村元, 刘冬华, 潘尚能, 等. 冷气掺混对高压涡轮气动性能影响的数值研究[J]. 航空动力学报, 2017, 32(4): 990-1000. ZHANG Cunyuan, LIU Donghua, PAN Shangneng, et al. Numerical study on influence of coolant injection on the aerodynamic performance of high pressure turbine[J]. Journal of Aerospace Power, 2017, 32(4): 990-1000. (in Chinese
ZHANG Cunyuan, LIU Donghua, PAN Shangneng, et al. Numerical study on influence of coolant injection on the aerodynamic performance of high pressure turbine[J]. Journal of Aerospace Power, 2017, 32(4): 990-1000. (in Chinese)
|
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