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High temperature oxidation of conventional and nanocrystalline HVOF thermal-sprayed NiCrAlY coatings

机译:高温氧化常规和纳米晶体HVOF热喷涂的幼苗涂料

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Thermal barrier coating (TBC) systems protect turbine blades against high-temperature corrosion. They consist of a metal bond coating (MCrAlY, M = Ni, Co) and a ceramic top layer (ZrO_2/Y_2O_3). In this work the oxidation behavior of conventional and nanostructured HVOF NiCrAlY coatings have been compared. Commercially available NiCrAlY powder was mechanically cryomilled and HVOF sprayed on a Nickel alloy foil to form a nanocrystalline coating. Free-standing bodies of conventional and nanostructured HVOF NiCrAlY coatings were oxidized at 1273 k for different periods in order to form the thermally grown oxide layer (TGO). The oxidation experiments show that the oxidation kinetics of the nanostructured coating is lower than the conventional coating. In the present work, this observation is explained by the formation of a continuous α-Al_2O_3 layer on the top of the nanostructured HVOF NiCrAlY coating that protects the coating from further oxidation and avoids the formation of mixed oxide protrusions present in the conventional coating. The as-sprayed coatings as well as the morphology of the oxide scale presents on the oxidized coatings were characterized by XRD and SEM.
机译:热屏障涂层(TBC)系统保护涡轮机叶片抵抗高温腐蚀。它们由金属键涂层(McRaly,M = Ni,Co)和陶瓷顶层(ZrO_2 / Y_2O_3)组成。在这项工作中,已经比较了常规和纳米结构HVOF涂层的氧化行为。可商购的幼亮粉末机械冷冻冷冻并喷涂在镍合金箔上以形成纳米晶体涂层。常规和纳米结构HVOF涂层的独立体在1273k中氧化不同的时期,以形成热生长的氧化物层(TGA)。氧化实验表明,纳米结构涂层的氧化动力学低于常规涂层。在本作工作中,通过在纳米结构的HVOF涂层顶部形成连续α-Al_2O_3层来解释该观察,该涂层在含有进一步的氧化中保护涂层并避免形成常规涂层中存在的混合氧化物突起。通过XRD和SEM表征氧化涂层上的氧化物尺度存在的氧化物刻度的形态。

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