Microstructure geometry for thermal barrier coatings to mitigate CMAS attack
Abstract
Thermal barrier coatings and methods to make such coatings present improved resistance to CMAS infiltration. The method for forming a thermal barrier coating includes applying a layer of the thermal barrier coating to a component having a surface, forming a plurality of first channels in the thermal barrier coating, and forming a plurality of second channels in the thermal barrier coating. The first channels extend through a thickness of the thermal barrier coating from an interface with the surface of the component to a free surface opposite the interface. The second channels are disposed between the free surface and the interface and extending lengthwise generally parallel to the free surface of the thermal barrier coating.
- Inventors:
- Issue Date:
- Research Org.:
- Univ. of Connecticut, Farmington, CT (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1771582
- Patent Number(s):
- 10822968
- Application Number:
- 16/435,484
- Assignee:
- University of Connecticut (Farmington, CT)
- Patent Classifications (CPCs):
-
C - CHEMISTRY C23 - COATING METALLIC MATERIAL C23C - COATING METALLIC MATERIAL
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- DOE Contract Number:
- SC0007544
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 06/08/2019
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Jordan, Eric, and Kumar, Rishi. Microstructure geometry for thermal barrier coatings to mitigate CMAS attack. United States: N. p., 2020.
Web.
Jordan, Eric, & Kumar, Rishi. Microstructure geometry for thermal barrier coatings to mitigate CMAS attack. United States.
Jordan, Eric, and Kumar, Rishi. Tue .
"Microstructure geometry for thermal barrier coatings to mitigate CMAS attack". United States. https://www.osti.gov/servlets/purl/1771582.
@article{osti_1771582,
title = {Microstructure geometry for thermal barrier coatings to mitigate CMAS attack},
author = {Jordan, Eric and Kumar, Rishi},
abstractNote = {Thermal barrier coatings and methods to make such coatings present improved resistance to CMAS infiltration. The method for forming a thermal barrier coating includes applying a layer of the thermal barrier coating to a component having a surface, forming a plurality of first channels in the thermal barrier coating, and forming a plurality of second channels in the thermal barrier coating. The first channels extend through a thickness of the thermal barrier coating from an interface with the surface of the component to a free surface opposite the interface. The second channels are disposed between the free surface and the interface and extending lengthwise generally parallel to the free surface of the thermal barrier coating.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Nov 03 00:00:00 EST 2020},
month = {Tue Nov 03 00:00:00 EST 2020}
}
Works referenced in this record:
Turbine Component and Methods of Assembling the Same
patent-application, January 2015
- Lacy, Benjamin Paul; Brzek, Brian Gene; Kottilingham, Srikanth Chandrudu
- US Patent Application 13/940806; 20150017018
Yttrium Aluminum Garnet Based Thermal Barrier Coatings
patent-application, September 2016
- Jordan, Eric H.; Gell, Maurice; Kumar, Rishi
- US Patent Application 15/040871; 20160257618