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Gas-turbine critical research and advanced technology support projectA technology data base for utility gas turbine systems capable of burning coal derived fuels was developed. The following areas are investigated: combustion; materials; and system studies. A two stage test rig is designed to study the conversion of fuel bound nitrogen to NOx. The feasibility of using heavy fuels in catalytic combustors is evaluated. A statistically designed series of hot corrosion burner rig tests was conducted to measure the corrosion rates of typical gas turbine alloys with several fuel contaminants. Fuel additives and several advanced thermal barrier coatings are tested. Thermal barrier coatings used in conjunction with low critical alloys and those used in a combined cycle system in which the stack temperature was maintained above the acid corrosion temperature are also studied.
Document ID
19820005636
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Clark, J. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Hodge, P. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Lowell, C. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Anderson, D. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Schultz, D. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 4, 2013
Publication Date
March 1, 1981
Subject Category
Energy Production And Conversion
Report/Patent Number
DOE/NASA/2593-24
E-737
NASA-TM-81708
Report Number: DOE/NASA/2593-24
Report Number: E-737
Report Number: NASA-TM-81708
Accession Number
82N13509
Funding Number(s)
CONTRACT_GRANT: DE-AI01-77ET-10350
PROJECT: RTOP 778-11-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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