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Industrial RB211 Dry Low Emission Combustion PUBLIC ACCESS

[+] Author Affiliations
Jeff D. Willis, Ian J. Toon, Tom Schweiger, David A. Owen

Rolls-Royce Industrial and Marine Gas Turbines Ltd., Ansty, Nr Coventry, UK

Paper No. 93-GT-391, pp. V03CT17A052; 8 pages
doi:10.1115/93-GT-391
From:
  • ASME 1993 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3C: General
  • Cincinnati, Ohio, USA, May 24–27, 1993
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7892-7
  • Copyright © 1993 by ASME

abstract

The inital combustor development of a pre-mix lean burn arrangement for an aero-derivative gas generator is described. The emission targets of the practical system were for the NOx and CO to be less than 25 vppm (15% O2) over a wide range of powers and ambient temperatures. From combustion rig testing of a two stage (in series) system at 1,5 and 20 atmospheres the baseload engine emissions are predicted to be NOx = 17 vppm (15% O2) and CO = 5 vppm with a turn down of 30% power. To achieve a wider power turn down a three stage (in series) system is required.

Copyright © 1993 by ASME
Topics: Combustion , Emissions
This article is only available in the PDF format.

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