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Combustion System Development for Dry Low-NOx Emission and High Turbine Inlet Temperatures FREE

[+] Author Affiliations
Bernard Becker, Wilhelm Schulten, Bernhard Schetter

SIEMENS AG, Mülheim, Germany

Paper No. 96-TA-026, pp. V001T02A006; 6 pages
doi:10.1115/96-TA-026
From:
  • ASME 1996 Turbo Asia Conference
  • ASME 1996 Turbo Asia Conference
  • Jakarta, Indonesia, November 5–7, 1996
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7877-4
  • Copyright © 1996 by ASME

abstract

The last 10 years of combustor development are characterised by the introduction of lean premixed burners for dry low-NOx emissions. This was easy to achieve as long as sufficient excess air was available. The modern gas turbine with its high turbine inlet temperature and increased need for component cooling sees a competition for air between combustion and requirements in other areas.

The paper describes how these problems have been solved by changing the design of burners and combustion chambers. The goal of minimising the hot surface area for a given combustor volume is achieved with the annular combustors. The number of burners has been selected in order to achieve good cross ignition, uniform temperature distribution and reasonably short residence times with the minimum of components. Test results and experience with operation and maintenance are also reported.

Copyright © 1996 by ASME
This article is only available in the PDF format.

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