Modeling of Residual Stresses in TBC Coated Gas Turbine Blades

Volume: 2 Number: 2 July 23, 2016
  • Yaşar Kahraman
  • Sedat İriç
  • İmdat Taymaz
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Modeling of Residual Stresses in TBC Coated Gas Turbine Blades

Abstract

Ceramic thermal barrier coatings have been developed for advanced gas turbine and diesel engine applications to improve engine reliability and fuel efficiency. Blades and vanes of the high-pressure turbine stages of aero-engines are the most highly stressed parts in engineering components. The blade geometry was objected to airflow at the temperatures about 800°C. These high gas turbine temperatures can only be maintained through advanced cooling techniques like electro-beam physical vapor deposition (EB-PVD) and thermal barrier coatings (TBCs). Such TBCs consist of thin ceramic layers of low thermal conductivity, yttrium stabilized zirconia (YSZ) which are applied on the blade surface. The coating imparts good adhesion of the ceramic to the substrate

References

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Details

Primary Language

English

Subjects

-

Journal Section

-

Authors

Yaşar Kahraman This is me
Sakarya University, Engineering Faculty, Serdivan, Sakarya, Turkey

Sedat İriç This is me
Sakarya University, Engineering Faculty, Serdivan, Sakarya, Turkey

İmdat Taymaz This is me
Sakarya University, Engineering Faculty, Serdivan, Sakarya, Turkey

Publication Date

July 23, 2016

Submission Date

July 23, 2016

Acceptance Date

-

Published in Issue

Year 2012 Volume: 2 Number: 2

IZ

https://izlik.org/JA22JH32CZ

Cite

RIS / Bibtex
APA
Kahraman, Y., İriç, S., & Taymaz, İ. (2016). Modeling of Residual Stresses in TBC Coated Gas Turbine Blades. TOJSAT, 2(2), 51-56. https://izlik.org/JA22JH32CZ
AMA
1.Kahraman Y, İriç S, Taymaz İ. Modeling of Residual Stresses in TBC Coated Gas Turbine Blades. TOJSAT. 2016;2(2):51-56. https://izlik.org/JA22JH32CZ
Chicago
Kahraman, Yaşar, Sedat İriç, and İmdat Taymaz. 2016. “Modeling of Residual Stresses in TBC Coated Gas Turbine Blades”. TOJSAT 2 (2): 51-56. https://izlik.org/JA22JH32CZ.
EndNote
Kahraman Y, İriç S, Taymaz İ (July 1, 2016) Modeling of Residual Stresses in TBC Coated Gas Turbine Blades. TOJSAT 2 2 51–56.
IEEE
[1]Y. Kahraman, S. İriç, and İ. Taymaz, “Modeling of Residual Stresses in TBC Coated Gas Turbine Blades”, TOJSAT, vol. 2, no. 2, pp. 51–56, July 2016, [Online]. Available: https://izlik.org/JA22JH32CZ
ISNAD
Kahraman, Yaşar - İriç, Sedat - Taymaz, İmdat. “Modeling of Residual Stresses in TBC Coated Gas Turbine Blades”. TOJSAT 2/2 (July 1, 2016): 51-56. https://izlik.org/JA22JH32CZ.
JAMA
1.Kahraman Y, İriç S, Taymaz İ. Modeling of Residual Stresses in TBC Coated Gas Turbine Blades. TOJSAT. 2016;2:51–56.
MLA
Kahraman, Yaşar, et al. “Modeling of Residual Stresses in TBC Coated Gas Turbine Blades”. TOJSAT, vol. 2, no. 2, July 2016, pp. 51-56, https://izlik.org/JA22JH32CZ.
Vancouver
1.Yaşar Kahraman, Sedat İriç, İmdat Taymaz. Modeling of Residual Stresses in TBC Coated Gas Turbine Blades. TOJSAT [Internet]. 2016 Jul. 1;2(2):51-6. Available from: https://izlik.org/JA22JH32CZ