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Experimental clean combustor program, phase 3A two-stage vortex burning and mixing combustor and associated fuel system components were successfully tested at steady state and transient operating conditions. The combustor exceeded the program goals for all three emissions species, with oxides of nitrogen 10 percent below the goal, carbon monoxide 26 percent below the goal, and total unburned hydrocarbons 75 percent below the goal. Relative to the JT9D-7 combustor, the oxides of nitrogen were reduced by 58 percent, carbon monoxide emissions were reduced by 69 percent, and total unburned hydrocarbons were reduced by 9 percent. The combustor efficiency and exit temperature profiles were comparable to those of production combustor. Acceleration and starting characteristics were deficient relative to the production engine.
Document ID
19770025217
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Roberts, R.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Fiorentino, A.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Greene, W.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1977
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-CR-135253
PWA-5493
Report Number: NASA-CR-135253
Report Number: PWA-5493
Accession Number
77N32161
Funding Number(s)
CONTRACT_GRANT: NAS3-19447
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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