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带前缘冲击复杂叶片内冷通道换热特性实验
引用本文:吴宏,刘裕盛,徐国强.带前缘冲击复杂叶片内冷通道换热特性实验[J].航空动力学报,2011,26(12):2641-2647.
作者姓名:吴宏  刘裕盛  徐国强
作者单位:北京航空航天大学能源与动力工程学院航空发动机气动热力国家级重点实验室,北京,100191
基金项目:国家自然科学基金(50976008)
摘    要:采用瞬态热色液晶方法对不同雷诺数下静止状态涡轮工作叶片带前缘冲击复杂蛇形通道的换热特性进行了考察,得到了不同位置吸、压力面的表面传热系数分布.实验结果表明:相同雷诺数下,叶片通道内表面带肋区域两肋间的局部换热强于光滑区域,相邻两肋间的传热系数沿流动方向呈单峰分布.随着雷诺数增加,内表面传热系数提高,在弯头下游的光滑区域...

关 键 词:涡轮叶片  蛇形通道  冲击气膜冷却  换热  热色液晶
收稿时间:2010/12/28 0:00:00
修稿时间:2011/4/12 0:00:00

Experimental investigation on heat transfer in complex internal cooling blade channel with leading-edge
WU Hong,LIU Yu-sheng and XU Guo-qiang.Experimental investigation on heat transfer in complex internal cooling blade channel with leading-edge[J].Journal of Aerospace Power,2011,26(12):2641-2647.
Authors:WU Hong  LIU Yu-sheng and XU Guo-qiang
Institution:National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China;National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:Heat transfer characteristics of complex serpentine channels with leading-edge impingement in static turbine blade were investigated using the transient thermochromic liquid crystal technique under different Reynolds numbers.Distributions of local heat transfer coefficient at different positions were obtained on both pressure and suction sides.Experimental results show that:local heat transfer between two ribs is stronger than that in smooth region on inner surface of blade channels.A single heat transfer peak occurs between two adjacent ribs along the flow direction.With increase of Reynolds number,heat transfer is enhanced on all surfaces and centrifugal effect of fluid is strengthened in non-rib area downstream the bend,resulting in uneven distribution of local heat transfer there.However,ribs after the bend can reduce this effect significantly.Besides,mainstream speed changes caused by expansion and contraction of channel cross-section also influence the values and distributions of local heat transfer.
Keywords:turbine blade  serpentine channels  impingement film cooling  heat transfer  thermochromic liquid crystal
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