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Methods for reducing pollutant emissions from jet aircraftPollutant emissions from jet aircraft and combustion research aimed at reducing these emissions are defined. The problem of smoke formation and results achieved in smoke reduction from commercial combustors are discussed. Expermental results of parametric tests performed on both conventional and experimental combustors over a range of combustor-inlet conditions are presented. Combustor design techniques for reducing pollutant emissions are discussed. Improved fuel atomization resulting from the use of air-assist fuel nozzles has brought about significant reductions in hydrocarbon and carbon monoxide emissions at idle. Diffuser tests have shown that the combustor-inlet airflow profile can be controlled through the use of diffuser-wall bleed and that it may thus be possible to reduce emissions by controlling combustor airflow distribution. Emissions of nitric oxide from a shortlength annular swirl-can combustor were significantly lower than those from a conventional combustor operating at similar conditions.
Document ID
19720010359
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Butze, H. F.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-68000
E-6762
Report Number: NASA-TM-X-68000
Report Number: E-6762
Meeting Information
Meeting: Winter Ann. Meeting of ASME
Location: Washington, DC
Country: United States
Start Date: November 28, 1971
End Date: December 2, 1971
Accession Number
72N18009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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