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Development of an Experimental LPP Gas Turbine Combustor PUBLIC ACCESS

[+] Author Affiliations
Patrik Johansson, Anders Sjunnesson, Stefan Olovsson

Volvo Flygmotor AB, Trollhättan, Sweden

Paper No. 94-GT-284, pp. V003T06A022; 7 pages
doi:10.1115/94-GT-284
From:
  • ASME 1994 International Gas Turbine and Aeroengine Congress and Exposition
  • Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations
  • The Hague, Netherlands, June 13–16, 1994
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7885-9
  • Copyright © 1994 by ASME

abstract

The design of a generic experimental LPP-combustor (Lean Premixed Prevaporized) is described. The combustor was tested at inlet pressures between 3 and 7 bar and with an inlet temperature between 500 K and 700 K. Tests were run with Diesel No.2 and Jet A-1 fuels comparing emissions of CO and NOx. The tests showed low NOx and CO values for a range of conditions although difficulties of using the LPP-technique close to the final boiling point of the fuel were encountered. To increase the understanding of the flow situation inside the combustor, numerical simulations using a large eddy simulation code was also performed. The main interest in the calculations was the evaporation process of the liquid fuel.

Copyright © 1994 by ASME
This article is only available in the PDF format.

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