引用本文:
【打印本页】   【HTML】 【下载PDF全文】   查看/发表评论  【EndNote】   【RefMan】   【BibTex】
←前一篇|后一篇→ 过刊浏览    高级检索
本文已被:浏览 1497次   下载 826 本文二维码信息
码上扫一扫!
分享到: 微信 更多
高致密多孔层板结构选型研究
赵乃芬1,谭晓茗1,李业芳1,房人麟2,徐华胜2
(1. 江苏省航空动力系统重点实验室,南京航空航天大学 能源与动力学院,江苏 南京 210016;2. 中国燃气涡轮研究院,四川 成都 610500)
摘要:
针对6种高致密多孔层板结构,利用CFD软件进行流动与换热的数值模拟,分析了冲击孔、扰流柱以及气膜孔的排列方式对层板流动特性和冷却效率的影响。计算结果表明:6种不同的排列方式,总压力损失均为4.5%左右,其中气流流经冲击壁与气膜壁的压力损失为2.2%左右;不同结构的双层板当量流量系数在0.86左右;层板的排列方式对综合冷却效果影响较大,在其他结构参数不变的情况下,不同的排列方式之间的综合冷却效率最大差值达到10%,在流体流动方向上,各排列的气膜壁面的温度梯度由最初的21K/mm减小到15K/mm;综合考虑各项因素的影响,气膜孔呈梭形排布最优的排列方式,其综合冷却效率最好。
关键词:  层板结构  压力损失  流量系数  冷却效率  数值模拟
DOI:
分类号:V233.1
基金项目:
Research on Structures of High-Density Laminate Porous Plates
ZHAO Nai-fen1,TAN Xiao-ming1,LI Ye-fang1,FANG Ren-lin2,XU Hua-sheng2
(1.Jiangsu Province Key Laboratory of Aerospace Power Systems,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;2. China Gas Turbine Establishment,Chengdu 610500,China)
Abstract:
Numerical simulation is carried out by CFD software to study six kinds of high-density porous lamilloy configurations. Arrays of impinging holes,pin-fins and film holes were studied to obtain cooling coefficient,lamilloy flow characteristic and pressure loss coefficient. The results show that the total pressure loss is about 4.5% for different arrangements with a 2.2% pressure-loss through impinging and film wall. Lamilloy equivalent flow coefficients of different configurations are always about 0.86. Maximum difference of cooling efficiency of lamilloy different configurations is up to 10%. Along flow direction,the film wall temperature rate decreases from 21K/mm to 15K/mm. By comprehensive comparision,‘shuttle’ shape is better than others with the highest cooling efficiency.
Key words:  Lamilloy configurations  Pressure loss  Flow coefficient  Cooling efficiency  Numerical simulation