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带有曲率的双层壁冷却结构内部换热特性

于松琦 由儒全 刘润洲 李海旺 鹿泽伦

于松琦, 由儒全, 刘润洲, 等. 带有曲率的双层壁冷却结构内部换热特性[J]. 航空动力学报, 2026, 41(X):20250450 doi: 10.13224/j.cnki.jasp.20250450
引用本文: 于松琦, 由儒全, 刘润洲, 等. 带有曲率的双层壁冷却结构内部换热特性[J]. 航空动力学报, 2026, 41(X):20250450 doi: 10.13224/j.cnki.jasp.20250450
Yu Songqi, You Ruquan, Liu Runzhou, et al. Internal heat transfer characteristics in curved double-wall laminate cooling structures[J]. Journal of Aerospace Power, 2026, 41(X):20250450 doi: 10.13224/j.cnki.jasp.20250450
Citation: Yu Songqi, You Ruquan, Liu Runzhou, et al. Internal heat transfer characteristics in curved double-wall laminate cooling structures[J]. Journal of Aerospace Power, 2026, 41(X):20250450 doi: 10.13224/j.cnki.jasp.20250450

带有曲率的双层壁冷却结构内部换热特性

doi: 10.13224/j.cnki.jasp.20250450
基金项目: 国家自然科学基金面上项目(52376042); 国家自然科学基金(52225602); 四川省科技计划(2026NSFSC1210); 中国博士后科学基金(2025M780853)
详细信息
    作者简介:

    于松琦(2002-),男,博士生,主要从事涡轮叶片冷却研究。E-mail:yusongqi_buaa@163.com

    通讯作者:

    刘润洲(1997-),男,博士后,主要从事涡轮叶片冷却研究。E-mail:liurunzhou_buaa@163.com

  • 中图分类号: V231.1

Internal heat transfer characteristics in curved double-wall laminate cooling structures

  • 摘要:

    采用瞬态液晶测量技术,通过实验定量分析了带冲击孔、扰流柱和狭缝的复杂双层壁结构靶面的换热情况与曲率(9°凹面、30°凸面和75°凸面)和冲击雷诺数(1000040000)的关系。研究发现,随着曲率增大,双层壁结构内部换热得到增强,在相同冲击雷诺数下,75°凸面的平均表面传热系数比9°凹面高出约20 W/(m2·K)。冲击雷诺数每升高10000,3种曲率结构的平均表面传热系数升高约30 W/(m2·K),仅当冲击雷诺数从30000升高到40000时,平均表面传热系数的增长变小。表面传热系数在展向上呈多峰分布,当雷诺数达到40000时,次峰数值超过主峰。表面传热系数沿流向整体呈下降趋势,在流向的不同位置处呈现不同的分布规律。

     

  • 图 1  双层壁结构示意图

    Figure 1.  Geometrical configuration of double-wall structure

    图 2  基于涡轮叶片曲率的弯曲双层壁

    Figure 2.  Curved double-wall structures based on turbine blade curvature

    图 3  实验装置

    Figure 3.  Experimental setup

    图 4  实验系统

    Figure 4.  Experimental system

    图 5  瞬态液晶标定曲线

    Figure 5.  Transient liquid crystal calibration result

    图 6  弯曲双层壁结构靶面表面传热系数分布

    Figure 6.  Contours of h at target surface of curved double-wall structure

    图 7  面平均表面传热系数

    Figure 7.  Area-averaged heat transfer coefficient

    图 8  平均表面传热系数计算区域

    Figure 8.  Calculation region of averaged heat transfer coefficient

    图 9  展向平均表面传热系数

    Figure 9.  Spanwise-averaged heat transfer coefficient

    图 10  流向平均表面传热系数

    Figure 10.  Flow direction averaged heat transfer coefficient

    表  1  结构参数设计

    Table  1.   Configuration of double-wall structure mm

    参数 数值 参数 数值
    L1 36.34 P 14
    L2 11 R1 5
    L3 11 R2 3
    L4 3 R3 9.68
    L5 26 R4 2
    L6 5 R5 3
    L7 6 R6 5
    L8 11 R7 4.5
    L9 103.9 R8 2
    L10 112 D 13
    L11 10 α1/(°) 35
    L12 17.46 α2/(°) 95
    L13 10.74 S* 5
    L14 19.79
    下载: 导出CSV

    表  2  各参数不确定度表

    Table  2.   Uncertainty of various parameters

    参数 数值 不确定度
    T0/K 293.15 ±0.2
    Th/K 333.15 ±0.2
    Tlc/K 302.46 ±0.2
    $ \lambda /\sqrt{\alpha } (\text{W}\sqrt{\text{s}}/ ({\text{m}}^{2}\cdot\text{K}) ) $ 554.96 ±22.3
    低换热 t/s 20 ±0.1
    h/(W/(m2·K)) 30 8.15%
    高换热 t /s 2 ±0.1
    h/(W/(m2·K)) 240 12.42%
    下载: 导出CSV
  • [1] 刘润洲, 李海旺, 由儒全, 等. 基于双层壁冷却结构的综合冷效数值解耦研究[J]. 航空动力学报, 2024, 39(5): 20220372. Liu Runzhou, Li Haiwang, You Ruquan, et al. Numerical decoupling of overall cooling effectiveness based on double-wall cooling structure[J]. Journal of Aerospace Power, 2024, 39(5): 20220372. (in Chinese

    Liu Runzhou, Li Haiwang, You Ruquan, et al. Numerical decoupling of overall cooling effectiveness based on double-wall cooling structure[J]. Journal of Aerospace Power, 2024, 39(5): 20220372. (in Chinese)
    [2] Unnikrishnan U, Yang V. A review of cooling technologies for high temperature rotating components in gas turbine[J]. Propulsion and Power Research, 2022, 11(3): 293-310. doi: 10.1016/j.jppr.2022.07.001
    [3] Nealy D A, Reider S B. Evaluation of laminated porous wall materials for combustor liner cooling[J]. Journal of Engineering for Power, 1980, 102(2): 268-276. doi: 10.1115/1.3230247
    [4] You Ruquan, Liu Runzhou, Li Haiwang. Experimental study of the couple effects of internal and external cooling on double-wall laminate structure with novel slot and pin-fins[J]. Applied Thermal Engineering, 2025, 260: 124989. doi: 10.1016/j.applthermaleng.2024.124989
    [5] Tian Xiaojing, Ye Weiqi, Xu Liang, et al. Optimization research on laminated cooling structure for gas turbines: a review[J]. AIMS Energy, 2025, 13(2): 354-401. doi: 10.3934/energy.2025014
    [6] Xu Liang, Sun Zineng, Ruan Qicheng, et al. Development trend of cooling technology for turbine blades at super-high temperature of above 2000 K[J]. Energies, 2023, 16(2): 668. doi: 10.3390/en16020668
    [7] Xu Liang, Jin Shenglong, Ye Weiqi, et al. A review of machine learning methods in turbine cooling optimization[J]. Energies, 2024, 17(13): 3177. doi: 10.3390/en17133177
    [8] Liu Runzhou, Li Haiwang, You Ruquan, et al. Numerical decoupling of the effect of internal cooling and external film cooling on overall cooling effectiveness[J]. Applied Thermal Engineering, 2023, 222: 119905. doi: 10.1016/j.applthermaleng.2022.119905
    [9] Ruan Qicheng, Xu Liang, Xi Lei, et al. Cooling performance of droplet-shaped Kagome truss structure combined with jet array impingement composite cooling structure[J]. Case Studies in Thermal Engineering, 2023, 51: 103558. doi: 10.1016/j.csite.2023.103558
    [10] 孙启超. 层板结构内部流动与换热特性研究[D]. 南京: 南京航空航天大学, 2012. Sun Qichao. Investigation on flow and heat transfer of the internal characteristics with lamilloy board[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012. (in Chinese

    Sun Qichao. Investigation on flow and heat transfer of the internal characteristics with lamilloy board[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012. (in Chinese)
    [11] Liang G. Gas turbine vane with integral cooling system: US 7255534 B2 [P]. 2007-08-14.
    [12] 全栋梁, 刘松龄, 李江海. 层板冷却结构强化换热机理[J]. 航空动力学报, 2004, 19(6): 860-865. Quan Dongliang, Liu Songling, Li Jianghai. Numerical investigation on mechanism of heat transfer augmentation in lamilloy[J]. Journal of Aerospace Power, 2004, 19(6): 860-865. (in Chinese

    Quan Dongliang, Liu Songling, Li Jianghai. Numerical investigation on mechanism of heat transfer augmentation in lamilloy[J]. Journal of Aerospace Power, 2004, 19(6): 860-865. (in Chinese)
    [13] 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 Technology, 2004, 25(2): 134-138. (in Chinese

    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 Technology, 2004, 25(2): 134-138. (in Chinese)
    [14] 全栋梁, 郁新华, 刘松龄, 等. 层板冷却结构流阻特性的实验与数值模拟[J]. 推进技术, 2003, 24(5): 425-428. Quan Dongliang, Yu Xinhua, Liu Songling, et al. Experimental and numerical investigation of internal-flow resistance characteristics in laminate porous plates[J]. Journal of Propulsion Technology, 2003, 24(5): 425-428. (in Chinese

    Quan Dongliang, Yu Xinhua, Liu Songling, et al. Experimental and numerical investigation of internal-flow resistance characteristics in laminate porous plates[J]. Journal of Propulsion Technology, 2003, 24(5): 425-428. (in Chinese)
    [15] You Ruquan, Liu Runzhou, Li Haiwang. Experiments on heat transfer and film cooling characteristics of double-wall cooling structure with novel slot holes and pin-fins[J]. Applied Thermal Engineering, 2024, 249: 123415. doi: 10.1016/j.applthermaleng.2024.123415
    [16] Terzis A, Von Wolfersdorf J, Weigand B, et al. Thermocouple thermal inertia effects on impingement heat transfer experiments using the transient liquid crystal technique[J]. Measurement Science and Technology, 2012, 23(11): 115303. doi: 10.1088/0957-0233/23/11/115303
    [17] Jang J H, Chiu H C, Yan W M. Impinging cooling of film hole surface using transient liquid crystal thermograph[J]. International Communications in Heat and Mass Transfer, 2013, 44: 23-30. doi: 10.1016/j.icheatmasstransfer.2013.03.009
    [18] Lee J, Ren Zhong, Ligrani P, et al. Crossflows from jet array impingement cooling: Hole spacing, target plate distance, Reynolds number effects[J]. International Journal of Thermal Sciences, 2015, 88: 7-18. doi: 10.1016/j.ijthermalsci.2014.09.003
    [19] Xing Yunfei, Spring S, Weigand B. Experimental and numerical investigation of impingement heat transfer on a flat and micro-rib roughened plate with different crossflow schemes[J]. International Journal of Thermal Sciences, 2011, 50(7): 1293-1307. doi: 10.1016/j.ijthermalsci.2010.11.008
    [20] Lo Y H, Liu Y H. Heat transfer of impinging jet arrays onto half-smooth, half-rough target surfaces[J]. Applied Thermal Engineering, 2018, 128: 79-91. doi: 10.1016/j.applthermaleng.2017.08.165
    [21] Rao Yu, Liu Yuyang, Wan Chaoyi. Multiple-jet impingement heat transfer in double-wall cooling structures with pin fins and effusion holes[J]. International Journal of Thermal Sciences, 2018, 133: 106-119. doi: 10.1016/j.ijthermalsci.2018.07.021
    [22] Liu Yuyang, Rao Yu, Yang Li. Numerical simulations of a double-wall cooling with internal jet impingement and external hexagonal arrangement of film cooling holes[J]. International Journal of Thermal Sciences, 2020, 153: 106337. doi: 10.1016/j.ijthermalsci.2020.106337
    [23] 饶宇, 刘宇阳, 万超一. 具有气膜出流孔和针肋的双层壁冷却结构内的冲击传热性能[J]. 航空学报, 2018, 39(1): 94-102. Rao Yu, Liu Yuyang, Wan Chaoyi. Jet impingement heat transfer performance in a double-wall cooling structure with film effusion holes and pin fins[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1): 94-102. (in Chinese

    Rao Yu, Liu Yuyang, Wan Chaoyi. Jet impingement heat transfer performance in a double-wall cooling structure with film effusion holes and pin fins[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(1): 94-102. (in Chinese)
    [24] Funazaki K, Tarukawa Y, Kudo T, et al. Heat transfer characteristics of an integrated cooling configuration for ultra-high temperature turbine blades: experimental and numerical investigations[C]//Volume 3: Heat Transfer; Electric Power; Industrial and Cogeneration. American Society of Mechanical Engineers, 2001: V003T01A031.
    [25] Funazaki K I, Bin Salleh H. Extensive studies on internal and external heat transfer characteristics of integrated impingement cooling structures for HP turbines[C]//Volume 4: Heat Transfer, Parts A and B. ASMEDC, 2008: 167-176.
    [26] Bu Shi, Yang Lianfeng, Qiu Hanghai, et al. Effect of sidewall slots and pin fins on the performance of latticework cooling channel for turbine blades[J]. Applied Thermal Engineering, 2017, 117: 275-288. doi: 10.1016/j.applthermaleng.2017.01.110
    [27] Axtmann M, Poser R, Von Wolfersdorf J, et al. Endwall heat transfer and pressure loss measurements in staggered arrays of adiabatic pin fins[J]. Applied Thermal Engineering, 2016, 103: 1048-1056. doi: 10.1016/j.applthermaleng.2016.04.066
    [28] Schultz D L, Jones T V. Heat-transfer measurements in short-duration hypersonic facilities[J]. agardograph, 1973.
    [29] Chen Lingling, Brakmann R G, Weigand B, et al. An experimental heat transfer investigation of an impingement jet array with turbulators on both target plate and impingement plate[J]. Applied Thermal Engineering, 2020, 166: 114661. doi: 10.1016/j.applthermaleng.2019.114661
    [30] Han J C, Wright L M. Analytical heat transfer[M]. 2nd Ed. Boca Raton: CRC Press, 2022.
    [31] Whitaker S. Forced convection heat transfer correlations for flow in pipes, past flat plates, single cylinders, single spheres, and for flow in packed beds and tube bundles[J]. AIChE Journal, 1972, 18(2): 361-371. doi: 10.1002/aic.690180219
    [32] Yan Youyou, Owen J M. Uncertainties in transient heat transfer measurements with liquid crystal[J]. International Journal of Heat and Fluid Flow, 2002, 23(1): 29-35. doi: 10.1016/S0142-727X(01)00125-4
    [33] Owen J M, Newton P J, Lock G D. Transient heat transfer measurements using thermochromic liquid crystal. Part 2: Experimental uncertainties[J]. International Journal of Heat and Fluid Flow, 2003, 24(1): 23-28. doi: 10.1016/S0142-727X(02)00207-2
    [34] Schlunder E U, Gnielinski V. Heat and mass transfer between a Surface and an impinging jet[J]. Chemie Ingenieur Technik, 1967, 39(9/10): 578-584.
    [35] Martin H. Heat and mass transfer between impinging gas jets and solid surfaces[M]//Advances in Heat Transfer Volume 13. Amsterdam: Elsevier, 1977: 1-60.
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  • 收稿日期:  2025-09-30
  • 网络出版日期:  2026-05-16

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