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Journal of Thermal Spray and Engineering最新文献

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Analytical and Experimental Study of Residual Stresses in Thermal Barrier Coatings Deposited on Gas Turbine Blades in Laboratory Dimensions by APS and HVOF Methods to Calculate the Optimal Thickness 利用APS和HVOF方法对燃气轮机叶片热障涂层在实验室尺寸下的残余应力进行了分析和实验研究
Pub Date : 1900-01-01 DOI: 10.52687/2582-1474/311
E. Poursaeidi, Farzam Montakhabi, J. Rahimi
The constant need to use gas turbines has led to the need to increase turbines' inlet temperature. When the temperature reaches a level higher than the material's tolerance, phenomena such as creep, changes in mechanical properties, oxidation, and corrosion occur at high speeds, which affects the life of the metal material. Nowadays, operation at high temperatures is made possible by proceedings such as cooling and thermal insulation by thermal barrier coatings (TBCs). The method of applying thermal barrier coatings on the turbine blade creates residual stresses. In this study, residual stresses in thermal barrier coatings applied by APS and HVOF methods are compared by Tsui–Clyne analytical model and XRD test. The analytical model results are in good agreement with the experimental results (between 2 and 8% error), and the HVOF spray method creates less residual stress than APS. In the end, an optimal thickness for the coating is calculated to minimize residual stress at the interface between the bond coat and top coat layers.
不断需要使用燃气轮机导致需要提高涡轮的入口温度。当温度超过材料的承受能力时,就会高速发生蠕变、机械性能变化、氧化、腐蚀等现象,影响金属材料的使用寿命。如今,通过热障涂层(tbc)的冷却和隔热等措施,高温下的操作成为可能。在涡轮叶片上应用热障涂层的方法会产生残余应力。本文采用Tsui-Clyne分析模型和XRD测试对比了APS和HVOF两种热障涂层的残余应力。分析模型结果与实验结果吻合较好(误差在2% ~ 8%之间),HVOF喷射法产生的残余应力小于APS法。最后,计算出涂层的最佳厚度,以最小化粘结层和面层之间界面处的残余应力。
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Journal of Thermal Spray and Engineering
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