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The Role of Different Atmospheric Plasma Spray Parameters on Microstructure of Abradable AlSi-Polyester Coatings

机译:不同等离子喷涂参数对可磨耗AlSi-聚酯涂层微观结构的影响

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One of the approaches to increase the thermic efficiency of aerospace engines is the application of abradable coatings enabling minimization and control of the clearance between the stator and the rotating blades tips. The main purpose of this contribution is to define the role of different technological parameters utilized for atmospheric plasma spraying of AlSi-polyester coating on its resulting microstructure. Deposition of abradable coatings on the real engine parts is mostly dependent on spraying stand-off distance and on spraying angle. These two parameters influence not only the coating microstructure but also the deposition efficiency itself, which is directly connected with economical aspects of the coating production. The set of experimental samples with atmospheric plasma sprayed Ni-based bond coat and two in chemical composition same initial powders delivered from different powder manufacturers were used to spray thick AlSi-polymer top coats with different spraying stand-off distances and angles. Subsequently some of the samples were also heat treated to burn-out the polymer phase from the coating microstructure. The Rockwell HR15Y hardness was measured on all samples and the microstructure and coating thickness were evaluated by means of light microscopy and image analysis methods.
机译:提高航空发动机热效率的一种方法是使用耐磨涂层,以使定子和旋转叶片尖端之间的间隙最小化并进行控制。这种贡献的主要目的是确定用于大气等离子喷涂AlSi-聚酯涂层在其最终微观结构上使用的不同技术参数的作用。实际发动机零件上的耐磨涂层的沉积主要取决于喷涂的支撑距离和喷涂角度。这两个参数不仅影响涂层的微观结构,而且影响沉积效率本身,这直接关系到涂层生产的经济性。这组具有大气等离子喷涂镍基粘结涂层的实验样品和从不同粉末制造商处交付的两种化学成分相同的初始粉末被用于喷涂具有不同喷涂间隔距离和角度的厚AlSi-聚合物外涂层。随后,还对一些样品进行热处理,以从涂层微结构中烧尽聚合物相。测量所有样品的洛氏HR15Y硬度,并通过光学显微镜和图像分析方法评估其微观结构和涂层厚度。

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