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Next Generation Thermal Barrier Coatings for the Gas Turbine Industry

机译:燃气轮机行业的下一代热障涂层

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The aim of the study presented in this paper was to develop the next generation of production ready air plasma sprayed thermal barrier coating with a low conductivity and long lifetime. In order to achieve these goals; a number of coating architectures were produced using commercially available plasma spray guns. Modifications were made to powder chemistry including; high purity powders for sintering resistance, Dysprosia stabilised Zirconia powders and powders containing porosity formers. Agglomerated & Sintered (A&S) and Hollow Oven Spherical Powder (HOSP) morphologies were used to attain beneficial microstructures. Finally, dual layer coatings were produced using the different powder morphologies. Evaluation of the thermal conductivity of the coating systems from room temperature to 1200℃ was conducted using laser flash technique. Tests were done on as-sprayed samples and samples heat treated for 100 hours at 1150℃ in order to evaluate the first stage sintering resistance of the coating systems. Thermal conductivity results were correlated to coating microstructure using image analysis of porosity and crack content. The results show the influence of beneficial porosity on reducing the thermal conductivity of the produced coatings.
机译:本文提出的研究目的是开发具有低电导率和长寿命的下一代可生产的空气等离子喷涂热障涂层。为了实现这些目标;使用可商购的等离子喷枪生产了许多涂层结构。对粉末化学进行了修改,包括:耐烧结的高纯度粉末,耐Dy稳定的氧化锆粉末和含有孔隙形成剂的粉末。使用团聚和烧结(A&S)和空心烤箱球形粉末(HOSP)形态来获得有益的微观结构。最后,使用不同的粉末形态生产了双层涂层。利用激光闪光技术对涂料体系从室温到1200℃的导热系数进行了评估。对喷涂后的样品进行了测试,并在1150℃下热处理了100小时,以评估涂层系统的第一阶段耐烧结性。使用孔隙率和裂纹含量的图像分析,将导热系数结果与涂层的微观结构相关联。结果表明有利的孔隙率对降低所产生的涂层的热导率的影响。

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