Journal of Propulsion Technology ›› 2014, Vol. 35 ›› Issue (11): 1517-1522.

• Combustion , Heat and Mass Transfer • Previous Articles     Next Articles

Research on Structures of High-Density Laminate Porous Plates

  

  1. Jiangsu Province Key Laboratory of Aerospace Power Systems,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;Jiangsu Province Key Laboratory of Aerospace Power Systems,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;Jiangsu Province Key Laboratory of Aerospace Power Systems,College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China;China Gas Turbine Establishment,Chengdu 610500,China;China Gas Turbine Establishment,Chengdu 610500,China
  • Published:2021-08-15

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;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;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;中国燃气涡轮研究院,四川 成都 610500;中国燃气涡轮研究院,四川 成都 610500
  • 作者简介:赵乃芬(1990—),女,硕士生,研究领域为航空发动机热端部件冷却。

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

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