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Title: 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}
}

Works referenced in this record:

Yttrium aluminum garnet based thermal barrier coatings
patent, November 2019


Multilayer thermal barrier coatings
patent-application, June 2010


Thermal conductivity and erosion durability of composite two-phase air plasma sprayed thermal barrier coatings
journal, October 2015


Overview on advanced thermal barrier coatings
journal, November 2010


Luminescent material compositions and structures incorporating the same
patent, June 2015


Phase relations in the ZrO2–La2O3–Y2O3–Al2O3 system: Experimental studies and phase modelling
journal, January 2013


Terbium as an alternative for luminescence sensing of temperature of thermal barrier coating materials
journal, December 2007


Luminescent Material Compositions and Structures Incorporating the Same
patent-application, August 2009


Thermal Barrier Coatings and Coated Components
patent-application, September 2011


Yttrium Aluminum Garnet Based Thermal Barrier Coatings
patent-application, September 2016


Turbine engine components
patent, May 2013


Thermal cycling behavior and failure mechanism of LaTi2Al9O19/YSZ thermal barrier coatings exposed to gas flame
journal, May 2011


Low-Thermal-Conductivity Rare-Earth Zirconates for Potential Thermal-Barrier-Coating Applications
journal, December 2002


Thermal Spray Deposition, Phase Stability and Mechanical Properties of La2Zr2O7/LaAlO3 Coatings
journal, June 2017


Characteristics of Phenomena in Powders Type RE2Zr2O7-Al2O3 in High Temperature Annealing Conditions
journal, April 2011