کد مقاله | کد نشریه | سال انتشار | مقاله انگلیسی | نسخه تمام متن |
---|---|---|---|---|
10668478 | 1008373 | 2011 | 4 صفحه PDF | دانلود رایگان |
عنوان انگلیسی مقاله ISI
Estimation of spallation life of thermal barrier coating of gas turbine blade by thermal fatigue test
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کلمات کلیدی
موضوعات مرتبط
مهندسی و علوم پایه
مهندسی مواد
فناوری نانو (نانو تکنولوژی)
پیش نمایش صفحه اول مقاله
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چکیده انگلیسی
In this study, thermal fatigue tests were performed at 1100 °C and 1151 °C. Then, c-scanning and bond strength tests were performed for TBC specimens that were thermally aged by thermal fatigue tests. From the results, an empirical equation based on the ratio of the delamination area and the thermal cycle number was presented and the spallation life of a TBC specimen could be roughly estimated using the relationship between the delaminated area and the number of cycles.
ناشر
Database: Elsevier - ScienceDirect (ساینس دایرکت)
Journal: Surface and Coatings Technology - Volume 205, Supplement 2, 25 July 2011, Pages S157-S160
Journal: Surface and Coatings Technology - Volume 205, Supplement 2, 25 July 2011, Pages S157-S160
نویسندگان
In-Hwan Shin, Jae-Mean Koo, Chang-Sung Seok, Sung-Ho Yang, Tack-Woon Lee, Bum-Soo Kim,