Investigation of creep behavior of a gas turbine blade with a Visco plasticFEM model to estimate the blade life

سال انتشار: 1403
نوع سند: مقاله کنفرانسی
زبان: انگلیسی
مشاهده: 177

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شناسه ملی سند علمی:

ICCONF09_003

تاریخ نمایه سازی: 17 تیر 1403

چکیده مقاله:

Creep is one of the most important factors in failure of turbine blades.Usually the life of a turbine blade is estimated based on approximateapproaches such as Larson Miller Parameter method. These methods are notaccurate enough and have several restrictions. Therefore, in this paper, finiteelement (FE) models based on time-dependent plastic behaviors areinvestigated for simulation of creep phenomenon in turbine blades. Threedifferent time-dependent plastic models are employed to estimate thelifetime for a turbine blade. The material of the blade is considered to becast Ni-base super alloy known as Inconel ۷۳۸LC. The results are comparedwith the available experimental data and also the results obtained by theLarson Miller Parameter method. It is shown that, the proposed modelsgives more realistic results and the predicted lifetime is almost ۵۰% longerthan that obtained using elastic stress analysis and Larson Miller Parametersmethod.

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نویسندگان

Mohammadamin Forghani

Lecturer, School of engineering, Zand Institute of Higher education, Shiraz, Iran

Kavous Ariafar

Assistant Professor, School of engineering, Zand Institute of Higher education, Shiraz,Iran.