叶片前缘两相流冲击冷却的耦合数值模拟

推进技术 ›› 2015, Vol. 36 ›› Issue (3): 443-449.

叶片前缘两相流冲击冷却的耦合数值模拟

姜玉廷¹,郑　群¹,罗铭聪²,岳国强¹,董　平¹,高　杰¹

哈尔滨工程大学动力与能源工程学院，黑龙江哈尔滨 150001,哈尔滨工程大学动力与能源工程学院，黑龙江哈尔滨 150001,中国船舶重工集团公司第七〇三研究所/燃气轮机事业部，黑龙江哈尔滨 150036,哈尔滨工程大学动力与能源工程学院，黑龙江哈尔滨 150001,哈尔滨工程大学动力与能源工程学院，黑龙江哈尔滨 150001,哈尔滨工程大学动力与能源工程学院，黑龙江哈尔滨 150001

发布日期:2021-08-15
作者简介:姜玉廷(1987—)，男，博士生，研究领域为燃气轮机涡轮传热与冷却技术。
基金资助:
中央高校基本科研业务专项基金(HEUCF130304)。

Conjugate Simulation of Two Phase Flow Impingement Cooling

College of Power and Energy Engineering，Harbin Engineering University，Harbin 150001，China,College of Power and Energy Engineering，Harbin Engineering University，Harbin 150001，China,The 703 Research Institute of CSIC，Turbine Research Institute，Harbin 150036，China,College of Power and Energy Engineering，Harbin Engineering University，Harbin 150001，China,College of Power and Energy Engineering，Harbin Engineering University，Harbin 150001，China and College of Power and Energy Engineering，Harbin Engineering University，Harbin 150001，China

Published:2021-08-15

摘要/Abstract

摘要： 为了更好地强化叶片前缘的换热，对叶片前缘进行两相流强化冲击冷却的耦合数值模拟研究。利用水滴/蒸汽冲击曲面冷却系统进行数值模拟程序的校核。在此基础上，利用欧拉-拉格朗日颗粒追踪方法对叶片前缘的两相流冲击冷却进行耦合数值研究。研究了水滴加湿量、水滴直径和水滴与壁面的作用边界条件对换热性能的影响。结果表明当加湿量从3%增加到8%时，最大的平均传热增强系数从1.671增加到4.913；水滴直径从5μm增加到20μm时，最大的平均传热增强系数从2.128降低到1.164；反弹和反弹+破碎边界条件预测的传热效果好于粘附和粘附+破碎边界条件。

关键词: 叶片前缘；两相流；冲击冷却；耦合数值模拟

Abstract: Conjugate simulations for the blade leading edge of two phase impingent cooling were carried out to enhance the heat transfer. The mist/steam cooling with jet impingement onto a concave surface was used to verify the accuracy of numerical simulation program. The Eulerian-Lagrangian particle tracking method was adopted to investigate the two-phase impingement cooling for blade leading edge. The effects of various parameters，such as mist ratio，mist diameter and mist-wall boundary conditions on the improvement of cooling performance were investigated. The results show that the largest average heat transfer enhancement coefficient increases from 1.67 to 4.94 with increasing mist ratio from 3% to 8%，and it decreases from 2.128 to 1.164 with increasing mist diameter from 5μm to 20μm. The rebound and rebound with break up boundary conditions show the better cooling performance than the trap and trap with break up boundary conditions.

Key words: Blade leading edge；Two phase flow；Impingement cooling；Conjugate simulation

姜玉廷,郑　群,罗铭聪,岳国强,董　平,高　杰. 叶片前缘两相流冲击冷却的耦合数值模拟[J]. 推进技术, 2015, 36(3): 443-449.

JIANG Yu-ting¹,ZHENG Qun¹,LUO Ming-cong²,YUE Guo-qiang¹,DONG Ping¹,GAO Jie¹. Conjugate Simulation of Two Phase Flow Impingement Cooling[J]. Journal of Propulsion Technology, 2015, 36(3): 443-449.

参考文献

[1] 刘高文, 薛彪, 彭力, 等. 叶片前缘旋流和常规冲击对比数值研究[J]. 推进技术, 2011, 32(4):576-580. (LIU Gao-wen, XUE Biao, PENG Li, et al. Numerical Investigation on Difference Between Blade Leading Edge Vortex and Normal Impingement Cooling[J]. Journal of Propulsion Technology, 2011, 32(4):576-580.)
[2] 曾志. 高效的喷雾冷却技术的实验与数值研究[D].哈尔滨:哈尔滨工业大学, 2010.
[3] 姜澎, 黄洪雁, 冯国泰, 等. 水雾/蒸汽相变冲击冷却的数值模拟[J].哈尔滨工程大学学报, 2009, 30(10): 1097-1101.
[4] 谭晓茗, 李业芳, 张靖周. 含湿气流单缝冲击冷却数值模拟[J].航空动力学报, 2013, 28(1): 129-135.
[5] 谭晓茗, 刘波, 朱兴丹, 等. 自由空间水/气垂直冲击冷却实验研究[J]. 工程热物理学报, 2013, 34(12): 2328-2331.
[6] Tan X M, Zhang J Z, Liu B, et al. Experimental Investigation on Heat Transfer Enhancement of Mist/Air Impingement Jet[J]. Science China Technological Science, 2013, 56(10): 2456-2464.
[7] Li X C, Gaddis J L, Wang T. Modeling of Heat Transfer in a Mist/Steam Impinging Jet[J]. Journal of Heat Transfer, 2001, 123(6): 1086-1092.
[8] Li X C, Gaddis J L, Wang T. Mist/Steam Heat Transfer with Jet Impingement onto a Concave Surface[J]. Journal of Heat Transfer, 2003, 125(3): 438-446.
[9] Li X C, Wang T. Mist/Steam Cooling by a Row of Impinging Jets[J]. International Journal of Heat and Mass Transfer, 2003, 46(12): 2279-2290.
[10] Wang T, Dhanasekaran T S. Calibration of CFD Model for Mist/Steam Impinging Jets Cooling[R].ASME 2008-GT-50737.
[11] 董平, 郭兆元, 王强, 等. 进口温度不均匀对气冷涡轮叶片传热的影响[J]. 工程热物理学报, 2010, 31(7): 1109-1112.
[12] Poling B E, Prausnitz J M, O’Connell J P, et al. The Properties of Gases and Liquids[M]. New York: McGraw-Hill, 2001.
[13] 姜玉廷, 郑群, 高杰, 等. 跨声速高压涡轮静叶水滴喷雾/空气冷却性能研究[J].机械工程学报, 2013, 49(16): 131-137.
[14] 姜澎. 考虑冷却工质相变的涡轮叶片高效冷却机理研究[D].哈尔滨:哈尔滨工业大学, 2010.
[15] Bai C X, Gosman A D. Development of Methodology for Spray Impingement Simulation[R]. SAE Technical Paper 950283, 1995.(编辑:张荣莉)　　　　　　　　　　　　　　收稿日期:2014-03-11；修订日期:2014-04-22。基金项目:中央高校基本科研业务专项基金(HEUCF130304)。作者简介:姜玉廷(1987—),男,博士生,研究领域为燃气轮机涡轮传热与冷却技术。E-mail:jiangyuting07314@126.com