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Correlations of catalytic combustor performance parametersCorrelations for combustion efficiency percentage drop and the minimum required adiabatic reaction temperature necessary to meet emissions goals of 13.6 g CO/kg fuel and 1.64 g HC/kg fuel are presented. Combustion efficiency was found to be a function of the cell density, cell circumference, reactor length, reference velocity, and adiabatic reaction temperature. The percentage pressure drop at an adiabatic reaction temperature of 1450 K was found to be proportional to the reference velocity to the 1.5 power and to the reactor length. It is inversely proportional to the pressure, cell hydraulic diameter, and fractional open area. The minimum required adiabatic reaction temperature was found to increase with reference velocity and decrease with cell circumference, cell density and reactor length. A catalyst factor was introduced into the correlations to account for differences between catalysts. Combustion efficiency, the percentage pressure drop, and the minimum required adiabatic reaction temperature were found to be a function of the catalyst factor. The data was from a 12 cm-diameter test rig with noble metal reactors using propane fuel at an inlet temperature of 800 K.
Document ID
19790003309
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Bulzan, D. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1978
Subject Category
Energy Production And Conversion
Report/Patent Number
E-9803
NASA-TM-79014
DOE/NASA/1040-78/4
Report Number: E-9803
Report Number: NASA-TM-79014
Report Number: DOE/NASA/1040-78/4
Meeting Information
Meeting: Workshop on Catalytic Combust.
Location: Asheville, NC
Country: United States
Start Date: October 3, 1978
End Date: October 4, 1978
Sponsors: EPA
Accession Number
79N11480
Funding Number(s)
CONTRACT_GRANT: EC-77-A-31-1040
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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