Thermal-barrier coatings for more efficient gas-turbine engines
โ Scribed by Clarke, David R. (author);Oechsner, Matthias (author);Padture, Nitin P. (author)
- Book ID
- 117996113
- Publisher
- Cambridge University Press
- Year
- 2012
- Tongue
- English
- Weight
- 843 KB
- Volume
- 37
- Category
- Article
- ISSN
- 0883-7694
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๐ SIMILAR VOLUMES
## Abstract The efficiency and performance of advanced aircraft turbines can be markedly increased if higher gas temperatures are used. Although the highly loaded blades and vanes in the high pressure turbine are heavily cooled, today's substrate materials are unable to provide sufficient strength
Thermal barrier coatings (TBCs) for turbine airfoils in high performance engines represent an advanced materials technology that has both performance and durability benefits.Foremost of the benefits of TBCs is the reduction of heat transferred into aircooled components. Other potential benefits incl