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冲击/发散冷却层板隔热屏冷却性能及对比

刘友宏 李英 杨旭

刘友宏, 李英, 杨旭. 冲击/发散冷却层板隔热屏冷却性能及对比[J]. 航空动力学报, 2014, (6): 1272-1278. doi: 10.13224/j.cnki.jasp.2014.06.003
引用本文: 刘友宏, 李英, 杨旭. 冲击/发散冷却层板隔热屏冷却性能及对比[J]. 航空动力学报, 2014, (6): 1272-1278. doi: 10.13224/j.cnki.jasp.2014.06.003
LIU You-hong, LI Ying, YANG Xu. Cooling performance and comparison of impingement/effusion cooling lamilloy used as heat shield[J]. Journal of Aerospace Power, 2014, (6): 1272-1278. doi: 10.13224/j.cnki.jasp.2014.06.003
Citation: LIU You-hong, LI Ying, YANG Xu. Cooling performance and comparison of impingement/effusion cooling lamilloy used as heat shield[J]. Journal of Aerospace Power, 2014, (6): 1272-1278. doi: 10.13224/j.cnki.jasp.2014.06.003

冲击/发散冷却层板隔热屏冷却性能及对比

doi: 10.13224/j.cnki.jasp.2014.06.003
详细信息
    作者简介:

    刘友宏(1963- ),男,江苏东台人,教授、博士生导师,博士,主要从事航空发动机气动热力学领域的研究.

  • 中图分类号: V231.1

Cooling performance and comparison of impingement/effusion cooling lamilloy used as heat shield

  • 摘要: 为了分析对比新型冲击/发散冷却层板隔热屏冷却性能,论证其应用于加力燃烧室的可行性,在3种不同主次流总压比条件下对其进行了三维流固耦合传热数值模拟研究,并与某型波纹板隔热屏和单层平板隔热屏进行了相同工况的对比分析,得到了冷却效果、冷气用量、冷气热负荷和次流总压损失系数等的对比结果和变化规律.结果表明:冲击/发散冷却层板隔热屏具有较好的冷却效果,但其受主次流总压比变化的影响较大.相比某型波纹板,冲击/发散冷却层板隔热屏的冷气消耗量平均减少41.6%,单位面积冷气热负荷平均降低65.9%.

     

  • [1] Champion J L,Deshaies B,Curtelin R,et al.Aerodynamical structure of the wall flow over a wavy surface partially cooled by air injection through multiperforations.AIAA 99-1016,1999.
    [2] 唐婵,常海萍.发散孔纵向波纹隔热屏气膜冷却特性研究[J].燃气轮机技术,2009,22(1):38-41. TANG Chan,CHANG Haiping.Numerical simulation on air film cooling characters of the longitudinal ripple heat shield with effusion holes[J].Gas Turbine Technology,2009,22(1):38-41.(in Chinese)
    [3] 陆永华,常海萍,谈浩元.纵向波纹隔热屏通道的换热特性[J].推进技术,2002,23(3):230-232. LU Yonghua,CHANG Haiping,TAN Haoyuan.Heat transfer of longitudinal ripple heat shield tunnel[J].Journal of Propulsion Techonlogy,2002,23(3):230-232.(in Chinese)
    [4] Jeffery A L,Torence P B,Derk S P.Development needs for advanced afterburner designs.AIAA 2004-4192,2004.
    [5] Jobin T R,Gamble E J,Bachmann J G.Development of a computer program for thermal analysis of aircraft cooling liners.AIAA 2006-986,2006.
    [6] 张宗卫,朱惠人,刘聪,等.全气膜冷却叶片表面换热系数和冷却效率研究[J].西安交通大学学报,2012,46(7):103-107. ZHANG Zongwei,ZHU Huiren,LIU Cong,et al.Heat transfer coefficient and film cooling effectiveness on a full-film cooling vane[J].Journal of Xi'an Jiaotong Unversity,2012,46(7):103-107.(in Chinese)
    [7] 谢浩,张靖周.致密孔阵气膜冷却绝热温比和对流换热系数的数值研究[J].航空动力学报,2009,24(6):1229-1235. XIE Hao,ZHANG Jingzhou.Numerical study on adiabatic wall cooling effectiveness and convective heat transfer coefficient of effusion cooling[J].Journal of Aerospace Power,2009,24(6):1229-1235.(in Chinese)
    [8] 胡超,许全宏,徐剑,等.冲击/发散冷却壁温分布和冷却效率研究[J].航空动力学报,2008,23(10):1080-1084. HU Chao,XU Quanhong,XU Jian,et al.Investigation of the wall temperature distribution and cooling efficiency for impingement/effusion cooling scheme[J].Journal of Aerospace Power,2008,23(10):1080-1084.(in Chinese)
    [9] 张荣春,樊未军,宋双文,等.驻涡燃烧室发散冷却方案试验[J].航空动力学报,2011,26(12):2667-2675. ZHANG Rongchun,FAN Weijun,SONG Shuangwen,et al.Experimental investigation on transpiration cooling of trapped vortex combustor[J].Journal of Aerospace Power,2011,26(12):2667-2675.(in Chinese)
    [10] 王寅会,常海萍,王玉梅.纵向波纹隔热屏气膜孔流量系数的实验[J].航空动力学报,2010,25(8):1758-1762. WANG Yinhui,CHANG Haiping,WANG Yumei.Experimental investigation on discharge of film holes in a longitudinal ripple insulated liner[J].Journal of Aerospace Power,2010,25(8):1758-1762.(in Chinese)
    [11] 常国强.正弦型波纹壁面气膜冷却研究.南京:南京航空航天大学,2011. CHANG Guoqiang.Research on film cooling of sinusoidal corrugated wall.Nanjing:Nanjing University of Aeronautics and Astronautics,2011.(in Chinese)
    [12] Thornton E A.Coupled flow thermal and structural analysis of aerodynamically heat panels[J].Journal of Aircraft,1988,25(11):1052-1059.
    [13] Barozzi G S,Pagliarini G.A method to solve conjugate heat transfer problems:the case of fully developed laminar flow in a pipe[J].Journal of Heat Transfer,1985(107):77-83.
    [14] 王梅娟,宋双文,胡好生,等.冲击+同向对流+气膜冷却的三维壁温计算与分析[J].航空动力学报,2011,26(10):2282-2286. WANG Meijuan,SONG Shuangwen,HU Haosheng,et al.Numerical computation and analysis of three-dimensional wall temperature of impingement+ identical flow convection+ film composite cooling[J].Journal of Aerospace Power,2011,26(10):2282-2286.(in Chinese)
    [15] 全栋梁,刘松龄,李江海,等.层板冷却特性的实验与数值模拟研究[J].推进技术,2004,25(2):134-138. QUAN Dongliang,LIU Songling,LI Jianghai,et al.Experimental and numerical investigation of the cooling characteristics in a laminate porous plate[J].Journal of Propulsion Techonlogy,2004,25(2):134-138.(in Chinese)
    [16] 《高温合金手册》编写组.高温合金手册[M].北京:冶金工业出版社,1972.
    [17] Funazaki K,Hachiya K.Systematic numerical studies on heat transfer and aerodynamic characteristics of impingement cooling devices combined with pins.ASME Paper GT2003-38256,2003.
    [18] Rao G A,Kitron-Belinkov M,Yeshayahou L.Numerical analysis of a multiple jet impingement system.ASME Paper GT2009-59719,2009.
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出版历程
  • 收稿日期:  2013-04-02
  • 刊出日期:  2014-06-28

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