Method for treating a gas turbine blade and gas turbine having said blade
US10215034B2 · kind B2 · utility
1Cited by
17References
23Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | Oct 5, 2012 |
| Grant date | Feb 26, 2019 |
| Priority date | — |
| Expiry date | Nov 13, 2033 |
Classification
- Technology area (CPC Y)Emerging Cross-Sectional Technologies
- CPC primaryY02T50/60
- WIPO fieldSurface technology, coating
- WIPO sectorChemistry
Abstract
The use of different ceramic layers allows different configurations of gas turbines to be produced each of which is optimized for a respective use of base load operation or peak load operation.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.