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Variable Geometry Fuel Injector for Low Emissions Gas Turbines FREE

[+] Author Affiliations
K. Smith, R. Steele, J. Rogers

Solar Turbines Incorporated, San Diego, CA

Paper No. 99-GT-269, pp. V002T02A040; 6 pages
doi:10.1115/99-GT-269
From:
  • ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition
  • Volume 2: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • Indianapolis, Indiana, USA, June 7–10, 1999
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7859-0
  • Copyright © 1999 by ASME

abstract

To extend the stable operating range of a lean premixed combustion system, variable geometry can be used to adjust the combustor air flow distribution as gas turbine operating conditions vary. This paper describes the design and preliminary testing of a lean premixed fuel injector that provides the variable geometry function. Test results from both rig and engine evaluations using natural gas are presented. The variable geometry injector has proven successful in the short-term testing conducted to date. Longer term field tests are planned to demonstrate durability.

Copyright © 1999 by ASME
This article is only available in the PDF format.

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