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The pollution reduction technology program for can-annular combustor engines - Description and resultsPollutant reduction and performance characteristics were determined for three successively more advanced combustor concepts. Program Element I consisted of minor modifications to the current production JT8D combustor and fuel system to evaluate means of improved fuel preparation and changes to the basic airflow distribution. Element II addressed versions of the two-staged Vorbix (vortex burning and mixing) combustor and represented a moderate increase in hardware complexity and difficulty of development. The concept selected for Element III employed vaporized fuel as a means of achieving minimum emission levels and represented the greatest difficulty of development and adaptation to the JT8D engine. Test results indicate that the Element I single-stage combustors were capable of dramatic improvement in idle pollutants. The multistage combustors evaluated in Program Elements II and III simultaneously reduced CO, THC and NOx emissions, but were unable to satisfy the current 1979 EPA standards.
Document ID
19760055286
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Roberts, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Fiorentino, A. J.
(United Technologies Corp. Pratt and Whitney Aircraft Div., East Hartford, Conn., United States)
Diehl, L.
(NASA Lewis Research Center Combustor Technology and Research Section, Cleveland, Ohio, United States)
Date Acquired
August 8, 2013
Publication Date
July 1, 1976
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 76-761
Meeting Information
Meeting: Propulsion Conference
Location: Palo Alto, CA
Start Date: July 26, 1976
End Date: July 29, 1976
Sponsors: American Institute of Aeronautics and Astronautics and Society of Automotive Engineers
Accession Number
76A38252
Funding Number(s)
CONTRACT_GRANT: NAS3-18548
Distribution Limits
Public
Copyright
Other

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