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Status of the DOE/NASA critical gas turbine research and technology projectActivities performed in order to provide an R&T data base for utility gas turbine systems burning coal-derived fuels are described. Experiments were run to determine the corrosivity effects of trace metal contaminants (and potential fuel additives) on gas turbine materials and these results were correlated in a corrosion-life prediction model. Actual fuels were burned in a burner rig hot corrosion test to verify the model. A deposition prediction model was assembled and compared with results of actual coal-derived fuel deposition tests. Thermal barrier coatings were tested to determine their potential for protecting gas turbine hardware from the corrosive contaminants. Several coatings were identified with significantly improved spallation-resistance (and, hence, corrosion resistance).
Document ID
19800006235
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Clark, J. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
January 1, 1980
Subject Category
Energy Production And Conversion
Report/Patent Number
E-263
DOE/NASA/2593-79/11
NASA-TM-79307
Report Number: E-263
Report Number: DOE/NASA/2593-79/11
Report Number: NASA-TM-79307
Meeting Information
Meeting: Annual Gas Turbine Conf.,
Location: New Orleans
Start Date: March 9, 1980
End Date: March 13, 1980
Sponsors: Am. Soc. of Mech. Engineers
Accession Number
80N14493
Funding Number(s)
CONTRACT_GRANT: EF-77-A-01-2593
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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