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)。
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).
作者
陈学
卢国鹏
孙创
夏新林
王秦阳
康宏琳
CHEN Xue;LU Guopeng;SUN Chuang;XIA Xinlin;WANG Qinyang;KANG Honglin(School of Energy Science and Engineering,Harbin Institute of Technology,Harbin 150001,China;Beijing Aerospace Technology Institute,The Third Academy,China Aerospace Science and Industry Corporation Limited,Beijing 100074,China)
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2023年第4期777-786,共10页
Journal of Aerospace Power
基金
国家自然科学基金(51806046)
中国博士后科学基金(2020T130145)。
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
thermal conductivity of coating
transient plane source(TPS)
two-dimensional unsteady heat transfer model
particle swarm optimization algorithm
inversion identification