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Deposition of Silicon-Enriched Nickel Aluminide Coatings on Internally Cooled Airfoils

机译:在内部冷却的机翼上沉积富硅铝化镍涂层

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摘要

We have shown that formation ofrnnickel aluminide coatings enriched with silicon is possible when using HC1 gas activation. The aluminum and silicon donating materials are provided as solids, which do not melt during the high-temperature diffusion process. By adjusting the Al:Si donator ratio, it is possible to deposit Ni-Al-Si coatings in a single-step process. A two-step process involving first aluminizing and then siliconizing leads to a depletion of aluminum and replacement by nickel silicides. Internal coating of complex structures (e.g., cooling channels of airfoils) is possible in principle. However, coating thickness and silicon content are significantly lower compared to external surfaces. Silicon-enriched layers normally lead to superior surface protection against hot corrosion when compared to simple nickel aluminide diffusion coatings. Further investiga-rntions will focus on optimization of internal coating by varying pressure parameters and donator mixtures.
机译:我们已经表明,当使用HCl气体活化时,可能会形成富含硅的铝化铝镍涂层。供铝和供硅的材料以固体形式提供,在高温扩散过程中不会熔化。通过调整Al:Si供体比率,可以在一个步骤中沉积Ni-Al-Si涂层。包括先渗铝然后渗硅的两步过程导致铝的消耗和硅化镍的替代。原则上可以对复杂结构(例如机翼的冷却通道)进行内部涂层。但是,与外表面相比,涂层厚度和硅含量要低得多。与简单的铝化镍扩散涂层相比,富含硅的层通常可提供出色的表面保护以防热腐蚀。进一步的研究将集中于通过改变压力参数和施主混合物来优化内部涂层。

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