Dip process thermal barrier coatings for gas turbines
β Scribed by Allam, Ibrahim M.
- Book ID
- 121810591
- Publisher
- AVS (American Vacuum Society)
- Year
- 1986
- Tongue
- English
- Weight
- 731 KB
- Volume
- 4
- Category
- Article
- ISSN
- 0734-2101
- DOI
- 10.1116/1.573698
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π SIMILAR VOLUMES
where his activities concentrated on weldable Ti alloys and advanced Al alloys. 1982 he joined DLR's Institute of Materials Research in KΓΆln, where he worked as group leader on AlΒ±Li alloys and high temperature titanium alloys. 1988 he became section head ΒͺLight Metals and CoatingsΒΊ. Presently he is
## Abstract Improved thermal barrier coatings can lead to increased engine operating efficiency. A significant problem is that multilayer systems are not thermally stable at elevated temperatures. Phenomena such as interdiffusion, oxidation and sintering take place, limiting coating lifetime. In or