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Experimental clean combustor program: Diesel no. 2 fuel addendum, phase 3A CF6-50 engine equipped with an advanced, low emission, double annular combustor was operated 4.8 hours with No. 2 diesel fuel. Fourteen steady-state operating conditions ranging from idle to full power were investigated. Engine/combustor performance and exhaust emissions were obtained and compared to JF-5 fueled test results. With one exception, fuel effects were very small and in agreement with previously obtained combustor test rig results. At high power operating condition, the two fuels produced virtually the same peak metal temperatures and exhaust emission levels. At low power operating conditions, where only the pilot stage was fueled, smoke levels tended to be significantly higher with No. 2 diesel fuel. Additional development of this combustor concept is needed in the areas of exit temperature distribution, engine fuel control, and exhaust emission levels before it can be considered for production engine use.
Document ID
19790018050
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Gleason, C. C.
(General Electric Co. Evendale, OH, United States)
Bahr, D. W.
(General Electric Co. Evendale, OH, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1979
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-CR-135413
R79AEG367
Report Number: NASA-CR-135413
Report Number: R79AEG367
Accession Number
79N26221
Funding Number(s)
CONTRACT_GRANT: NAS3-19736
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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