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Emissions Reduction Technology ProgramCombustor concepts having the potential for significantly lower emissions levels were investigated. The combustor emissions reduction was measured in an engine test. Emission characteristics common to all engine classes are shown. Multiple-burning zone combustors, specifically the double-annular and swirl-can combustors were studied. Airblast and air-assist fuel injection techniques were evaluated for emissions control potential. The combustor sceening and refining phases are summarized.
Document ID
19780003122
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, R. E.
(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
78N11065
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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