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Design and Testing of an Ultra-Low NOx Gas Turbine Combustor PUBLIC ACCESS

[+] Author Affiliations
Kenneth O. Smith

Solar Turbines Incorporated, San Diego, CA

Leonard C. Angello

Electric Power Research Institute, Palo Alto, CA

F. Richard Kurzynske

Gas Research Institute, Chicago, IL

Paper No. 86-GT-263, pp. V003T06A019; 8 pages
doi:10.1115/86-GT-263
From:
  • ASME 1986 International Gas Turbine Conference and Exhibit
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Dusseldorf, West Germany, June 8–12, 1986
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7930-6
  • Copyright © 1986 by ASME

abstract

The design and initial rig testing of an ultra-low NOx gas turbine combustor primary zone are described. A lean premixed, swirl-stabilized combustor was evaluated over a range of pressures up to 10.7 × 105 Pa (10.6 atm) using natural gas. The program goal of reducing NOx emissions to 10 ppm (at 15% O2) with coincident low CO emissions was achieved at all combustor pressure levels. Appropriate combustor loading for ultra-low NOx operation was determined through emissions sampling within the primary zone. The work described represents a first step in developing an advanced gas turbine combustion system that can yield ultra-low NOx levels without the need for water injection and selective catalytic reduction.

Copyright © 1986 by ASME
This article is only available in the PDF format.

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