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Finite element simulation of stress distribution through novel duplex thermal barrier coating used in turbine engine

عنوان مقاله: Finite element simulation of stress distribution through novel duplex thermal barrier coating used in turbine engine
شناسه ملی مقاله: ICC13_096
منتشر شده در سیزدهمین کنگره سرامیک ایران و سومین کنفرانس بین المللی سرامیک ایران در سال 1401
مشخصات نویسندگان مقاله:

N. Nayebpashaee - Department of Metallurgy and Mechanical Engineering, Technology and Engineering Research Center, StandardResearch Institute (SRI), Karaj, Iran

خلاصه مقاله:
Thermal barrier coatings (TBCs) have become an important element in hot section component durability. Anattempt was made to investigate the thermal and residual stress distribution in a novel three layer (۸YSZ/La۲Zr۲O۷/NiCrAlY) during a real-like heating regime which includes heating, service time and final cooling.Finite element approach with considering temperature dependency and also hybrid meshing was Heat fluxand nodal temperature contours indicated that, most of damaging and harmful thermal load and residualstress concentrate on ceramic top coats and this lead less harm and life time reduction in substrate.

کلمات کلیدی:
Thermal barrier coating, Residual stresses, Finite element simulation, Thermal shock

صفحه اختصاصی مقاله و دریافت فایل کامل: https://civilica.com/doc/1557096/