Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
8025723 | Surface and Coatings Technology | 2016 | 23 Pages |
Abstract
In turbine applications, these alloys will be part of a multilayer system that generates thermal stresses due to the CTE mismatch between the components. To investigate this phenomenon, the CTE data was incorporated into a thermo-mechanical model to calculate the energy release rate (ERR) for the delamination of coatings from these alloys. The ERR of a thermally grown oxide (TGO) formed on the bare and bond coated Co-based alloys was determined as a function of superalloy and bond coat CTE. The ERR of a thermal barrier coating (TBC) was evaluated as a function of temperature, superalloy CTE, and coating thickness. The ERR was found to be about 1.5 à greater in Co-based superalloys compared to Ni-based superalloys cooled from T = 1100 °C to ambient. Strategies for reducing the driving force for delamination are discussed.
Related Topics
Physical Sciences and Engineering
Materials Science
Nanotechnology
Authors
R. Wesley Jackson, Michael S. Titus, Matthew R. Begley, Tresa M. Pollock,