The study on delamination life of TBC through burner-rig test

Since gas turbines operate under extremely high temperatures, the hot-section parts of gas turbines should be protected from severe environmental conditions. Thermal Barrier Coating (TBC) is a protection technique that lowers the surface temperature of the hot-section parts. To design reliable gas t...

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Published inInternational journal of precision engineering and manufacturing Vol. 18; no. 4; pp. 555 - 560
Main Authors Yun, Junghan, Kim, Yongseok, Lee, Jeong-Min, Song, Hyunwoo, Wee, Sunguk, Koo, Jae-Mean, Lee, Young-Ze, Seok, Chang-Sung
Format Journal Article
LanguageEnglish
Published Seoul Korean Society for Precision Engineering 01.04.2017
Springer Nature B.V
Subjects
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ISSN2234-7593
2005-4602
DOI10.1007/s12541-017-0066-8

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Abstract Since gas turbines operate under extremely high temperatures, the hot-section parts of gas turbines should be protected from severe environmental conditions. Thermal Barrier Coating (TBC) is a protection technique that lowers the surface temperature of the hot-section parts. To design reliable gas turbines, the delamination life of TBC should be accurately evaluated. This study evaluated the delamination life of TBC by conducting a burner-rig test simulation of thermal fatigue conditions using a hot flame. Two types of TBCs were considered: one with vertical cracks and the other without vertical cracks. To evaluate the effects of pre-isothermal deterioration on thermal fatigue life under flame conditions, burner-rig tests were performed using isothermally deteriorated specimens. The burner-rig tests were conducted until the coating layer was completely delaminated. Using the tests results, predictive equations for delamination life and delaminated TBC area were derived and analyzed.
AbstractList Since gas turbines operate under extremely high temperatures, the hot-section parts of gas turbines should be protected from severe environmental conditions. Thermal Barrier Coating (TBC) is a protection technique that lowers the surface temperature of the hot-section parts. To design reliable gas turbines, the delamination life of TBC should be accurately evaluated. This study evaluated the delamination life of TBC by conducting a burner-rig test simulation of thermal fatigue conditions using a hot flame. Two types of TBCs were considered: one with vertical cracks and the other without vertical cracks. To evaluate the effects of pre-isothermal deterioration on thermal fatigue life under flame conditions, burner-rig tests were performed using isothermally deteriorated specimens. The burner-rig tests were conducted until the coating layer was completely delaminated. Using the tests results, predictive equations for delamination life and delaminated TBC area were derived and analyzed.
Author Lee, Young-Ze
Lee, Jeong-Min
Seok, Chang-Sung
Koo, Jae-Mean
Yun, Junghan
Kim, Yongseok
Song, Hyunwoo
Wee, Sunguk
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Issue 4
Keywords Burner-rig test
Delamination life
Thermally grown oxides
Thermal barrier coating
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Snippet Since gas turbines operate under extremely high temperatures, the hot-section parts of gas turbines should be protected from severe environmental conditions....
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SubjectTerms Delamination
Engineering
Fatigue failure
Fatigue life
Fatigue tests
Gas turbines
High temperature
Industrial and Production Engineering
Materials Science
Regular Paper
Thermal barrier coatings
Thermal fatigue
Thermal simulation
Title The study on delamination life of TBC through burner-rig test
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