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首页> 外文期刊>Surface & Coatings Technology >The effects of spray parameters on the microstructure and thermal stability of thermal barrier coatings formed by solution precursor flame spray (spfs)
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The effects of spray parameters on the microstructure and thermal stability of thermal barrier coatings formed by solution precursor flame spray (spfs)

机译:喷涂参数对溶液前驱体火焰喷涂(spfs)形成的热障涂层的微观结构和热稳定性的影响

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摘要

Solution precursor spraying is a new method of applying thermal barrier coatings (TBCs) on metallic substrates. In this work, the injection of a solution precursor has been made axially into an oxy-acetylene flame to deposit 7wt.% yttria stabilized zirconia (7wt.% YSZ) coatings. For this purpose a home-made atomizer has been inserted into the nozzle of a flame spray torch. The precursor used was an aqueous solution containing zirconium and yttrium salts to make a solid solution of 93wt.% ZrO2 and 7wt.% Y2O3 (7YSZ) in the coating. A martensitic stainless steel plate has been used as substrate on which a bond coat of NiCrAlY alloy was applied by atmospheric plasma spray process. The effects of spray distance and atomizing gas (oxygen and hydrogen) on the microstructure, phase composition, thermal shock and thermal exposure resistance of the coatings have been examined. The results show that the use of H_2 as the precursor atomizing gas instead of oxygen increases the enthalpy of the flame the result of which is coatings with the least non decomposed precursor and highest crystalline YSZ. This effect causes the severe cracking at thermal shock and thermal exposure tests in coatings made by oxygen atomizing due to higher amount of non-decomposed precursor. By contrast, coatings made by hydrogen atomizing showed very little cracking because of increased enthalpy of the flame and a small quantity of non-decomposed precursor.
机译:溶液前驱物喷涂是一种在金属基材上施加热障涂层(TBC)的新方法。在这项工作中,已将溶液前体的注入轴向注入氧-乙炔火焰中,以沉积7wt。%的氧化钇稳定的氧化锆(7wt。%的YSZ)涂层。为此目的,将自制的雾化器插入火焰喷灯的喷嘴中。所用的前体是含有锆和钇盐的水溶液,以在涂层中制成93重量%的ZrO 2和7重量%的Y 2 O 3(7YSZ)的固溶体。马氏体不锈钢板已经用作基底,通过大气等离子体喷涂法在其上施加了NiCrAlY合金的粘结层。考察了喷涂距离和雾化气体(氧气和氢气)对涂层的微观结构,相组成,热冲击和耐热暴露性的影响。结果表明,使用H_2作为前体雾化气体而不是氧气会增加火焰的焓,其结果是涂层中未分解的前体最少,结晶YSZ最高。由于大量未分解的前体,这种作用会导致在通过氧气雾化制成的涂层的热冲击和热暴露测试中出现严重的开裂。相反,由于火焰的焓增加和少量未分解的前体,所以通过氢雾化制得的涂层几乎没有破裂。

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