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AZO改性Y2O3-ZnO-Al2O3热控涂层性能分析
引用本文:李涛,张鹏,卢松涛,吴晓宏.AZO改性Y2O3-ZnO-Al2O3热控涂层性能分析[J].航天器环境工程,2021,38(5):548-554.
作者姓名:李涛  张鹏  卢松涛  吴晓宏
作者单位:哈尔滨工业大学 化工与化学学院,哈尔滨 150001
基金项目:国家自然科学基金项目(编号:51671074)
摘    要:为解决铝合金表面液相等离子体电解氧化(PEO)涂层(Y2O3-ZnO-Al2O3)导电性差而导致的静电效应,对其进行表面改性处理。采用原子层沉积(ALD)技术在铝合金表面PEO涂层原位沉积铝掺杂氧化锌(AZO)导电薄膜以提高PEO涂层的导电性。对AZO改性PEO涂层的相组成和表面微观结构进行分析;对不同沉积温度下所得复合涂层的电阻率、载流子浓度和迁移率,以及沉积前后的热控性能、耐腐蚀性进行测量分析。结果表明:AZO导电薄膜均质连续致密地沉积在PEO涂层表面;当沉积温度为150 ℃时,AZO@Y2O3-ZnO-Al2O3复合涂层的电阻率为1.15×10-4 Ω·cm,载流子浓度为1.8×1020 cm-3,太阳吸收比为0.409,发射率为0.892,且抗电化学腐蚀性能良好,能够满足航天器热控涂层在空间环境应用的技术要求。

关 键 词:原子层沉积    铝掺杂氧化锌    PEO涂层    热控性能
收稿时间:2021-07-30

The performance of AZO conductive film modified Y2O3-ZnO-Al2O3 coatings as a thermal control material
Institution:School of Chemical Engineering and Chemistry, Harbin Institute of Technology, Harbin 150001, China
Abstract:In order to eliminate an electrostatic effect due to the poor conductivity of the Y2O3-ZnO-Al2O3 coatings prepared by liquid-phase plasma electrolytic oxidation (PEO) on the surfaces of the aluminum alloy. A modification is made by the aluminum-doped zinc oxide (AZO) conductive film, deposited through the atomic layer deposition (ALD) technique in situ on the PEO coating to improve the overall conductivity. The phase composition and surface microstructure of the resulting AZO@Y2O3-ZnO-Al2O3 coatings are analyzed. Meanwhile, the conductive property including the resistivity, the carrier concentration, and the mobility, as well as thermal control and anticorrosion performance of the composite coatings obtained at different deposition temperatures are measured. It is shown that the AZO conductive film deposited on the surface of the PEO coating is uniform, continuous and dense. When the deposition temperature is 150 ℃, the AZO@Y2O3-ZnO-Al2O3 composite coating has an excellent charge conductivity with a resistivity of 1.15×10-4 Ω·cm and the carrier concentration of 1.8×1020 cm-3. In addition, the AZO@Y2O3-ZnO-Al2O3 coating has excellent anticorrosion and thermal control properties with a solar absorptivity of 0.409 and an emissivity of 0.892, which can meet technical requirements for spacecraft thermal control coatings in space environments.
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