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Experimental clean combustor program, phase 2The alternate fuels investigation objective was to experimentally determine the impacts, if any, on exhaust emissions, performance, and durability characteristics of the hybrid and vorbix low pollution combustor concepts when operated on test fuels which simulate composition and property changes which might result from future broadened aviation turbine fuel specifications or use of synthetically derived crude feedstocks. Results of the program indicate a significant increase in CO and small NOX increase in emissions at idle for both combustor concepts, and an increase in THC for the vorbix concept. Minimal impact was observed on gaseous emissions at high power. The vorbix concept exhibited significant increase in exhaust smoke with increasing fuel aromatic content. Altitude stability was not affected for the vorbix combustor, but was substantially reduced for the hybrid concept. Severe carbon deposition was observed in both combustors following limited endurance testing with No. 2 home heat fuel. Liner temperature levels were insensitive to variations in aromatic content over the range of conditions investigated.
Document ID
19760021341
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Roberts, R.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Peduzzi, A.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Vitti, G. E.
(Pratt and Whitney Aircraft East Hartford, CT, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1976
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-CR-134970
PWA-5370
Report Number: NASA-CR-134970
Report Number: PWA-5370
Accession Number
76N28429
Funding Number(s)
CONTRACT_GRANT: NAS3-18544
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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