Thermal barrier coatings
Abstract
High temperature stable thermal barrier coatings useful for substrates that form component parts of engines such as a component from a gas turbine engine exposed to high temperatures are provided. The thermal barrier coatings include a multiphase composite and/or a multilayer coating comprised of two or more phases with at least one phase providing a low thermal conductivity and at least one phase providing mechanical and erosion durability. Such low thermal conductivity phase can include a rare earth zirconate and such mechanical durability phase can include a rare earth a rare earth aluminate. The different phases are thermochemically compatible even at high temperatures above about 1200° C.
- Inventors:
- Issue Date:
- Research Org.:
- Pennsylvania State Univ., University Park, PA (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 2222223
- Patent Number(s):
- 11739410
- Application Number:
- 15/624,396
- Assignee:
- The Penn State Research Foundation (University Park, PA)
- DOE Contract Number:
- SC0004356
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 06/15/2017
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Wolfe, Douglas E., and Schmitt, Michael Philipp. Thermal barrier coatings. United States: N. p., 2023.
Web.
Wolfe, Douglas E., & Schmitt, Michael Philipp. Thermal barrier coatings. United States.
Wolfe, Douglas E., and Schmitt, Michael Philipp. Tue .
"Thermal barrier coatings". United States. https://www.osti.gov/servlets/purl/2222223.
@article{osti_2222223,
title = {Thermal barrier coatings},
author = {Wolfe, Douglas E. and Schmitt, Michael Philipp},
abstractNote = {High temperature stable thermal barrier coatings useful for substrates that form component parts of engines such as a component from a gas turbine engine exposed to high temperatures are provided. The thermal barrier coatings include a multiphase composite and/or a multilayer coating comprised of two or more phases with at least one phase providing a low thermal conductivity and at least one phase providing mechanical and erosion durability. Such low thermal conductivity phase can include a rare earth zirconate and such mechanical durability phase can include a rare earth a rare earth aluminate. The different phases are thermochemically compatible even at high temperatures above about 1200° C.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2023},
month = {8}
}
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