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Performance of a catalytic reactor at simulated gas turbine combustor operating conditionsThe performance of a catalytic reactor 12 cm in diameter and 17 cm long was evaluated at simulated gas turbine combustor operating conditions using premixed propane and air. Inlet temperatures of 600 and 800 K, pressures of 3 and 6 atm, and reference velocities of 9 to 30 m/s were tested. Data were taken for equivalence ratios as high as 0.43. The operating range was limited on the low-temperature side by very poor efficiency; the minimum exit temperature for good performance ranged from 1400 to 1600 K depending on inlet conditions. As exit temperatures were raised above this minimum, emissions of unburned hydrocarbons decreased, carbon monoxide emissions became generally less than 1 g CO/kg fuel, and nitrogen oxides were less than about 0.1 g NO2/kg fuel.
Document ID
19750017986
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Anderson, D. N.
(NASA Lewis Research Center Cleveland, OH, United States)
Tacina, R. R.
(NASA Lewis Research Center Cleveland, OH, United States)
Mroz, T. S.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1975
Subject Category
Inorganic And Physical Chemistry
Report/Patent Number
E-8381
NASA-TM-X-71747
Report Number: E-8381
Report Number: NASA-TM-X-71747
Accession Number
75N26058
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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