Zhang Tong, Song Xuyao, Qi Gongjin, An Baolin, Dong Wei, Zhao Yan, Wang Zhiyong, Yi Xiaosu, Yuan Zundong, Zhao Yunlong, Sun Luge, Mao Hongyu
Department of Materials Science and Engineering, Beihang University, Beijing 100191, China.
Beijing Institute of Aeronautical Materials, Beijing 100195, China.
Materials (Basel). 2021 Dec 29;15(1):235. doi: 10.3390/ma15010235.
Zirconium oxide (ZrO) is widely used as the thermal barrier coating in turbines and engines. Accurate emissivity measurement of ZrO coating at high temperatures, especially above 1000 °C, plays a vital role in thermal modelling and radiation thermometry. However, it is an extremely challenging enterprise, and very few high temperature emissivity results with rigorously estimated uncertainties have been published to date. The key issue for accurately measuring the high temperature emissivity is maintaining a hot surface without reflection from the hot environment, and avoiding passive or active oxidation of material, which will modify the emissivity. In this paper, a novel modified integrated blackbody method is reported to measure the high temperature normal spectral emissivity of ZrO coating in the temperature range 1000 °C to 1200 °C and spectral range 8 μm to 14 μm. The results and the associated uncertainty of the measurement were estimated and a relative standard uncertainty better than 7% ( = 2) is achieved.
氧化锆(ZrO)被广泛用作涡轮机和发动机中的热障涂层。准确测量ZrO涂层在高温下,特别是在1000℃以上的发射率,在热建模和辐射测温中起着至关重要的作用。然而,这是一项极具挑战性的工作,迄今为止,很少有已发表的高温发射率结果带有经过严格估计的不确定度。准确测量高温发射率的关键问题在于保持热表面不受热环境的反射影响,并避免材料发生被动或主动氧化,因为这会改变发射率。本文报道了一种新颖的改进型集成黑体法,用于测量ZrO涂层在1000℃至1200℃温度范围以及8μm至14μm光谱范围内的高温法向光谱发射率。对测量结果及相关不确定度进行了估计,实现了优于7%(k = 2)的相对标准不确定度。