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Thermal barrier coatings for gas turbine and diesel enginesThe present state of development of thin thermal barrier coatings for aircraft gas turbine engines and thick thermal barrier coatings for truck diesel engines is assessed. Although current thermal barrier coatings are flying in certain gas turbine engines, additional advances will be needed for future engines. Thick thermal barrier coatings for truck diesel engines have advanced to the point where they are being seriously considered for the next generation of engine. Since coatings for truck engines is a young field of inquiry, continued research and development efforts will be required to help bring this technology to commercialization.
Document ID
19900004320
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miller, Robert A. (NASA Lewis Research Center Cleveland, OH, United States)
Brindley, William J. (NASA Lewis Research Center Cleveland, OH, United States)
Bailey, M. Murray (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1989
Subject Category
Metallic Materials
Report/Patent Number
NASA-TM-102408
E-5160
NAS 1.15:102408
Meeting Information
Meeting: Workshop on Ceramic Coatings for Wear and Thermal Applications
Location: Edmonton, Alberta
Country: Canada
Start Date: October 16, 1989
End Date: October 17, 1989
Sponsors: Canadian Univ.-Industry-Council on Advanced Ceramics
Accession Number
90N13636
Funding Number(s)
PROJECT: RTOP 505-63-1A
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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