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Energy efficient engineThe feasibility of meeting or closely approaching the emissions goals established for the Energy Efficient Engine (E3) Project with an advanced design, single annular combustor was determined. A total of nine sector combustor configurations and one full-annular-combustor configuration were evaluated. Acceptable levels of carbon monoxide and hydrocarbon emissions were obtained with several of the sector combustor configurations tested, and several of the configurations tested demonstrated reduced levels of nitrogen oxides compared to conventional, single annular designs. None of the configurations tested demonstrated nitrogen oxide emission levels that meet the goal of the E3 Project.
Document ID
19800024900
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Burrus, D.
(General Electric Co. Cincinnati, OH, United States)
Sabla, P. E.
(General Electric Co. Cincinnati, OH, United States)
Bahr, D. W.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 4, 2013
Publication Date
June 1, 1980
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-159685
R79AEG562
Report Number: NASA-CR-159685
Report Number: R79AEG562
Accession Number
80N33408
Funding Number(s)
PROJECT: RTOP 535-01-12
CONTRACT_GRANT: NAS3-20643
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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