NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Advanced technology for reducing aircraft engine pollutionCombustor research programs are described whose purpose is to demonstrate significantly lower exhaust emission levels. The proposed EPA regulations covering the allowable levels of emissions will require a major technological effort if these levels are to be met by 1979. Pollution reduction technology is being pursued by NASA through a combination of in-house research, contracted progams, and university grants. In-house research with the swirl-can modular combustor and the double-annular combustor has demonstrated significant reduction in the level of NO(x) emissions. The work is continuing in an attempt to further reduce these levels by improvements in module design and in air-fuel scheduling. Research on the reduction of idle emissions has included the conversion of conventional duplex fuel nozzles to air-assisted nozzles and exploration of the potential improvements possible with fuel staging and variable combustor geometry.
Document ID
19730018070
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Jones, R. E.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-68256
E-7537
Report Number: NASA-TM-X-68256
Report Number: E-7537
Meeting Information
Meeting: Winter Ann. Meeting of the ASME
Location: Detroit, MI
Country: United States
Start Date: November 11, 1973
End Date: November 15, 1973
Accession Number
73N26797
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available