Transient heat transfer experiment and thermal conductivity identification of coating materials
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摘要:
针对涂层‒基体一体化的双层结构,为测试评估其中涂层材料的导热性能,提出基于瞬态平面热源法(transient plane source, TPS)的涂层材料导热系数反演辨识方法。根据Hot-Disk实验测试原理,建立基体‒涂层‒探头整体的二维非稳态传热模型;结合测量过程中的瞬时温升数据信息,采用粒子群优化算法反演辨识获得涂层材料的导热系数;并通过实验和数值模拟论证了上述方法的可靠性。结果表明:该测量方法能够有效获得涂层导热系数,测试反演的数值偏差小于4.0%。最后,实际测量和反演辨识获得了一种涂层材料常温至773 K的导热系数,随温度提高呈现增大趋势,数值范围为0.18~0.29 W/(m·K)。
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关键词:
- 涂层导热系数 /
- 瞬态平面热源法(TPS) /
- 二维非稳态传热模型 /
- 粒子群算法 /
- 反演辨识
Abstract:In order to evaluate the thermal conductivity of the coating material in the coating substrate integrated double-layer structure, an inversion method of thermal conductivity of coating materials based on transient plane source (TPS) was proposed. According to the Hot-Disk experimental measurement process, a two-dimensional unsteady heat transfer model of substrate-coating-probe was established. Combined with the instantaneous temperature rise data in the experimental test, the thermal conductivity of coating materials was obtained by inversion identification using particle swarm optimization algorithm. The reliability of the above method was demonstrated by experiments and numerical simulation. The results showed this technology can effectively acquire the thermal conductivity of coating with a low deviation less than 4.0%. Finally, the thermal conductivity of a coating material from room temperature to 773 K was obtained by actual measurement and inversion identification. A gradual increase was found as the temperature increased and the numerical range was 0.18−0.29 W/(m·K).
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表 1 隔热涂层材料在不同温度下的导热系数
Table 1. Thermal conductivity of the insulation coating at different temperatures
Tamb/K λ/(W/(m·K)) 均值 P1 P2 P3 300 0.184 0.179 0.180 0.181 373 0.210 0.203 0.205 0.206 473 0.219 0.204 0.212 0.217 573 0.241 0.235 0.225 0.225 713 0.248 0.245 0.232 0.242 773 0.292 0.285 0.289 0.292 -
[1] 王志平,费宇杰,刘延宽. 热障涂层失效机理、改进方法及未来发展方向[J]. 表面技术,2021,50(7): 126-137.WANG Zhiping,FEI Yujie,LIU Yankuan. Failure mechanism, improvement method and future development direction of thermal barrier coatings[J]. Surface Technology,2021,50(7): 126-137. (in Chinese) [2] 王利平,张靖周,姚玉. 敷设热障涂层气冷叶片温度分布数值研究[J]. 航空动力学报,2012,27(2): 357-364.WANG Liping,ZHANG Jingzhou,YAO Yu. Numerical investigation on temperature distribution of an air-cooled and thermal barrier coating blade[J]. Journal of Aerospace Power,2012,27(2): 357-364. (in Chinese) [3] 付伟,黄国胜,程旭东,等. NiAl/NiCoCrAlY/8YSZ复合喷涂层的微观结构与性能研究[J]. 表面技术,2019,48(4): 61-67.FU Wei,HUANG Guosheng,CHENG Xudong,et al. Microstructure and properties of NiAl/NiCoCrAlY/8YSZ composite coatings[J]. Surface Technology,2019,48(4): 61-67. (in Chinese) [4] 周雳, 邢志国, 王海斗, 等. 等离子喷涂金属/陶瓷梯度热障涂层研究进展[J]. 表面技术, 2020, 49(1): 122-131.ZHOU Li, XING Zhiguo, WANG Haidou, et al. Research progress of metal/ceramic gradient thermal barrier coatings by plasma spraying[J]. Surface Technology, 2020, 49(1): 122-131. (in Chinese) [5] 王莉莉,王伟,谭世磊,等. 热障涂层制备方法的研究[J]. 热加工工艺,2016,45(18): 15-18.WANG Lili,WANG Wei,TAN Shilei,et al. Research on preparation methods of thermal barrier coatings[J]. Hot Working Technology,2016,45(18): 15-18. (in Chinese) [6] 张建生,杨君友,朱文,等. 薄膜热导率测试方法研究进展[J]. 材料导报,2010,24(7): 103-107.ZHANG Jiansheng,YANG Junyou,ZHU Wen,et al. Research advances in the measurement for the thermal conductivity of thin solid films[J]. Materials Reports,2010,24(7): 103-107. (in Chinese) [7] ZHANG H,LI Y M,TAO W Q. Theoretical accuracy of anisotropic thermal conductivity determined by transient plane source method[J]. International Journal of Heat and Mass Transfer,2017,108: 1634-1644. doi: 10.1016/j.ijheatmasstransfer.2017.01.025 [8] AI Q,HU Z W,WU L L,et al. A single-sided method based on transient plane source technique for thermal conductivity measurement of liquids[J]. International Journal of Heat and Mass Transfer,2017,109: 1181-1190. doi: 10.1016/j.ijheatmasstransfer.2017.03.008 [9] SOLÓRZANO E,REGLERO J A,RODRÍGUEZ-PÉREZ M A,et al. An experimental study on the thermal conductivity of aluminium foams by using the transient plane source method[J]. International Journal of Heat and Mass Transfer,2008,51(25/26): 6259-6267. [10] DAOUAS N,FGUIRI A,RADHOUANI M S. Solution of a coupled inverse heat conduction-radiation problem for the study of radiation effects on the transient hot wire measurements[J]. Experimental Thermal and Fluid Science,2008,32(8): 1766-1778. doi: 10.1016/j.expthermflusci.2008.04.003 [11] GUSTAFSSON S E. Transient plane source techniques for thermal conductivity and thermal diffusivity measurement of solid materials[J]. Review of Scientific Instruments,1991,62(3): 797-804. doi: 10.1063/1.1142087 [12] HE Y. Rapid thermal conductivity measurement with a hot disk sensor: Part 1 theoretical considerations[J]. Thermochimica Acta,2005,436(1/2): 122-129. [13] HE Y. Rapid thermal conductivity measurement with a hot disk sensor: Part 2 characterization of thermal greases[J]. Thermochimica Acta,2005,436(1/2): 130-134. doi: 10.1016/j.tca.2005.07.003 [14] MIHIRETIE B M,CEDERKRANTZ D,ROSÉN A,et al. Finite element modeling of the hot disc method[J]. International Journal of Heat and Mass Transfer,2017,115: 216-223. doi: 10.1016/j.ijheatmasstransfer.2017.08.036 [15] GUSTAVSSON J S,GUSTAVSSON M K,USTAFSSON S E. On the use of the hot disk thermal constants analyser for measuring the thermal conductivity of thin samples of electrically insulating materials[J]. Thermal Conductivity,1997,62(3): 116-122. [16] ZHANG H,LI M J,FANG W Z,et al. A numerical study on the theoretical accuracy of film thermal conductivity using transient plane source method[J]. Applied Thermal Engineering,2014,72(1): 62-69. doi: 10.1016/j.applthermaleng.2014.01.058 [17] KERR L,PAN Y,DINWIDDIE R,et al. Thermal conductivity of coated paper[J]. International Journal of Thermophysics,2009,30(2): 572-579. doi: 10.1007/s10765-009-0565-7 [18] ALIFANOV O M. Inverse heat transfer problems[M]. Berlin: Springer-Verlag, 1994.