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Perspective on thermal barrier coatings for industrial gas turbine applicationsThermal Barrier Coatings (TBC's) have been used in high thrust aircraft engines for many years, and have proved to be very effective in allowing higher turbine inlet temperatures. TBC life requirements for aircraft engines are typically less than those required in industrial gas turbines. The use of TBC's for industrial gas turbines can increase if durability and longer service life can be successfully demonstrated. This paper will describe current and future applications of TBC's in industrial gas turbine engines. Early testing and applications of TBC's will also be reviewed. This paper focuses on the key factors that are expected to influence utilization of TBC's in advanced industrial gas turbine engines. It is anticipated that reliable, durable and high effective coating systems will be produced that will ultimately improve engine efficiency and performance.
Document ID
19950019708
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mutasim, Z. Z.
(Solar Turbines Inc. San Diego, CA, United States)
Hsu, L. L.
(Solar Turbines Inc. San Diego, CA, United States)
Brentnall, W. D.
(Solar Turbines Inc. San Diego, CA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1995
Publication Information
Publication: NASA. Lewis Research Center, Thermal Barrier Coating Workshop
Subject Category
Nonmetallic Materials
Accession Number
95N26128
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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