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Multifuel evaluation of rich/quench/lean combustorThe fuel flexible combustor technology was developed for application to the Model 570-K industrial gas turbine engine. The technology, to achieve emission goals, emphasizes dry NOx reduction methods. Due to the high levels of fuel-bound nitrogen (FBN), control of NOx can be effected through a staged combustor with a rich initial combustion zone. A rich/quench/lean variable geometry combustor utilizes the technology presented to achieve low NOx from alternate fuels containing FBN. The results focus on emissions and durability for multifuel operation.
Document ID
19830002289
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Notardonato, J. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Novick, A. S.
(Detroit Diesel Allison)
Troth, D. L.
(Detroit Diesel Allison)
Date Acquired
September 4, 2013
Publication Date
January 1, 1982
Subject Category
Energy Production And Conversion
Report/Patent Number
NASA-TM-82986
E-1418
NAS 1.15:82986
DOE/NASA/13111-10
Report Number: NASA-TM-82986
Report Number: E-1418
Report Number: NAS 1.15:82986
Report Number: DOE/NASA/13111-10
Meeting Information
Meeting: Joint Power Conf.
Location: Denver
Start Date: October 17, 1982
End Date: October 21, 1982
Accession Number
83N10559
Funding Number(s)
CONTRACT_GRANT: DE-AI01-77ET-13111
PROJECT: RTOP 778-14-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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