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Emissions control for ground power gas turbinesThe similarities and differences of emissions reduction technology for aircraft and ground power gas turbines is described. The capability of this technology to reduce ground power emissions to meet existing and proposed emissions standards is presented and discussed. Those areas where the developing aircraft gas turbine technology may have direct application to ground power and those areas where the needed technology may be unique to the ground power mission are pointed out. Emissions reduction technology varying from simple combustor modifications to the use of advanced combustor concepts, such as catalysis, is described and discussed.
Document ID
19780003129
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rudney, R. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Priem, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Juhasz, A. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Anderson, D. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Mroz, T. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Mularz, E. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1977
Publication Information
Publication: Aircraft Eng. Emissions
Subject Category
Aircraft Propulsion And Power
Accession Number
78N11072
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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