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Title: In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components

Abstract

A turbine component (10), such as a turbine blade, is provided which is made of a metal alloy (22) and a base, planar-grained thermal barrier layer (28) applied by air plasma spraying on the alloy surface, where a heat resistant ceramic oxide overlay material (32') covers the bottom thermal barrier coating (28), and the overlay material is the reaction product of the precursor ceramic oxide overlay material (32) and the base thermal barrier coating material (28).

Inventors:
 [1]
  1. Oviedo, FL
Issue Date:
Research Org.:
Westinghouse Electric Corp., Pittsburgh, PA (United States)
OSTI Identifier:
874014
Patent Number(s):
6294260
Assignee:
Siemens Westinghouse Power Corporation (Orlando, FL)
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
Y - NEW / CROSS SECTIONAL TECHNOLOGIES Y10 - TECHNICAL SUBJECTS COVERED BY FORMER USPC Y10S - TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
DOE Contract Number:  
AC05-95OR22242
Resource Type:
Patent
Country of Publication:
United States
Language:
English
Subject:
in-situ; formation; multiphase; air; plasma; sprayed; barrier; coatings; turbine; components; component; 10; blade; provided; metal; alloy; 22; base; planar-grained; thermal; layer; 28; applied; spraying; surface; heat; resistant; ceramic; oxide; overlay; material; 32; covers; bottom; coating; reaction; product; precursor; heat resistant; coating material; plasma spray; turbine blade; thermal barrier; metal alloy; reaction product; plasma spraying; barrier coating; barrier layer; ceramic oxide; turbine components; resistant ceramic; alloy surface; plasma sprayed; turbine component; situ formation; in-situ formation; barrier coatings; /428/416/

Citation Formats

Subramanian, Ramesh. In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components. United States: N. p., 2001. Web.
Subramanian, Ramesh. In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components. United States.
Subramanian, Ramesh. Mon . "In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components". United States. https://www.osti.gov/servlets/purl/874014.
@article{osti_874014,
title = {In-situ formation of multiphase air plasma sprayed barrier coatings for turbine components},
author = {Subramanian, Ramesh},
abstractNote = {A turbine component (10), such as a turbine blade, is provided which is made of a metal alloy (22) and a base, planar-grained thermal barrier layer (28) applied by air plasma spraying on the alloy surface, where a heat resistant ceramic oxide overlay material (32') covers the bottom thermal barrier coating (28), and the overlay material is the reaction product of the precursor ceramic oxide overlay material (32) and the base thermal barrier coating material (28).},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2001},
month = {1}
}