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Catalyst durability evaluation for advanced gas turbine enginesCatalytic combustion has demonstrated the ability to provide low NO(x) emissions while maintaining high combustion efficiency. Recently, under joint NASA Lewis, EPA, and Acurex sponsorship, a catalytic reactor was tested for 1000 hours to demonstrate durability in combustion environments representative of advanced automotive gas turbine engines. At a 740K air preheat temperature and a propane fuel/air ratio of 0.028 by mass, the adiabatic flame temperature was held at about 1700K. The graded cell monolithic reactor measured 5 cm in diameter by 10.2 cm in length and was operated at a reference velocity of 13.4 m/s at 1 atmosphere pressure. Measured NO(x) levels remained below 5 ppm while unburned hydrocarbon concentrations registered near zero and carbon monoxide levels were nominally below 20 ppm. The durability test included several parametric turndown studies and ended with a series of on/off cycling tests to further characterize reactor performance.
Document ID
19830044052
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Snow, G. C.
(Acurex Corp. Mountain View, CA, United States)
Pessagno, S. L.
(Acurex Corp. Energy and Environmental Div., Mountain View, CA, United States)
Date Acquired
August 11, 2013
Publication Date
October 1, 1982
Subject Category
Mechanical Engineering
Report/Patent Number
ASME PAPER 82-JPGC-GT-21
Meeting Information
Meeting: Joint Power Generation Conference
Location: Denver, CO
Start Date: October 17, 1982
End Date: October 21, 1982
Sponsors: American Society of Mechanical Engineers
Accession Number
83A25270
Funding Number(s)
CONTRACT_GRANT: DEN3-83
CONTRACT_GRANT: EPA-68-02-3122
Distribution Limits
Public
Copyright
Other

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