论文:2023,Vol:41,Issue(4):750-756
引用本文:
李皓璠, 云雪. 涡轮叶片带肋通道换热性能数值和试验研究[J]. 西北工业大学学报
LI Haofan, YUN Xue. Numerical simulation and experimental investigation of heat transfer performance of turbine blade with ribbed channel[J]. Journal of Northwestern Polytechnical University

涡轮叶片带肋通道换热性能数值和试验研究
李皓璠, 云雪
沈阳飞机设计研究所, 辽宁 沈阳 110035
摘要:
采用数值模拟与试验测试相结合的方法,利用涡旋核心可视化技术对于带肋通道内部流动与换热机理进行研究。对于宽高比为1的45°斜置带肋直通道的原型结构(无切除结构)和另外6种优化结构,全部肋片在流动方向下游切除2个肋高(3.8 mm)的改良结构在综合换热性能上表现最优,相对于原型结构的带肋面平均Nu数、平均Nu数比和平均换热因子分别增长25.1%,24.8%,22.7%;经试验验证,带肋通道外壁面温度的试验值与数值模拟值误差在10%左右。
关键词:    带肋通道    冷却性能    叶片冷却   
Numerical simulation and experimental investigation of heat transfer performance of turbine blade with ribbed channel
LI Haofan, YUN Xue
Shenyang Aircraft Design & Research Institute, Shenyang 110035, China
Abstract:
A combination of numerical simulation and experimental test is carried out, and the vortex core visualization technology is adopted to visualize vortex in the flow field and study the heat transfer mechanism. The heat transfer characteristics of air flow in 45° ribbed straight channel with aspect ratio of 1 and the other 6 new ribbed channels are studied. The results show that the average heat transfer performance of the new ribbed channel with all the fins 3.8 mm cut at the far end of fins along the flow direction is the best by comparing with the original ribbed straight channel under the same conditions. The average Nu, the average Nu/Nu0 and the average heat transfer enhancement factor FT of the ribbed wall is increased respectively by 25.1%, 24.8%, 22.7% on the average by comparing with the original ribbed channel. The experimental results show that the error between the experimental value and the simulated is about 10% for the outer wall temperature of ribbed channel.
Key words:    ribbed channel    cooling performance    blade cooling   
收稿日期: 2022-07-22     修回日期:
DOI: 10.1051/jnwpu/20234140750
通讯作者:     Email:
作者简介: 李皓璠(1992—),沈阳飞机设计研究所工程师,主要从事飞机推进系统设计研究。e-mail:geniuslhf@163.com
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