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Effect of degree of fuel vaporization on emissions for a premixed-prevaporized combustor systemThe impact of the degree of fuel vaporization upon emission from a flametube combustor was studied using an inlet air pressure of 3 x 10 to the 5th power pascals, inlet air temperatures of 600K and 700K, a reference velocity of 35 meters per second and equivalence ratios of .6 and .72 using Jet A fuel. Incoming air was preheated to temperatures from 600K to 700K by a nonvitiating preheater. Jet A fuel was injected into this airstream through two different fuel injectors manifolded together and mounted in series upstream of a watercooled preforated plate flameholder. The fuel-air mixture burned in a watercooled combustor section. Samples of the fuel-air mixture upstream of the flameholder were obtained for analysis to determine the local degree of fuel vaporization and the fuel-air ratio. Samples of the combustion products were analyzed to determine gaseous emissions. The effects of vaporization on carbon monoxide and nitric on carbon monoxide and nitric oxide emissions are presented.
Document ID
19790016832
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cooper, L. P.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: Premixed Prevaporized Combustor Technol. Forum
Subject Category
Aircraft Propulsion And Power
Accession Number
79N25003
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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