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ASME 1998 International Gas Turbine and Aeroengine Congress and Exhibition | 1998

Field Experience of the Sequential Combustion System for the GT24/GT26 Gas Turbine Family

Franz Joos; Philipp Brunner; Marcel Stalder; Stefan Tschirren

The first units of the Sequential Combustion System gas turbine family are in commercial operation. The first gas turbine GT24 (60Hz, 165MW-class) started the commercial operation, while the first GT26 (50Hz, 265MW-class) demonstrates its performance at the GT test facility. More engines are presently in the commissioning phase or will be in the near future. These turbines are designed to offer increased output at high GT efficiency. To acheive this, the sequential combustion system, a reheat process with two combustors, has been developed. Whereas the first combustor is based on the proven EV-combustor technology, extensive research and development efforts have been carried out in developing the lean premixed self-igniting second combustor (SEV).This paper is a follow-up of the ASME paper 96-GT-315, which described the basic research work concerning the lean premixing SEV-burners with self-ignition. The present paper reports the experience gained during commissioning of the first engines.The performance of the two combustors, as well as the measured emissions, are discussed and compared with the expected values and rig test results.Finally, the potential of the sequential combustion system to reach low NOx levels is demonstrated by unveiling the results of the extensive testing program during the commissioning phase.Copyright


Archive | 2002

Method for running up a gas turbine plant

Marcel Stalder; Dieter Rebhan; Thomas Kueenzi; Hans Peter Knoepfel


Archive | 2001

Combustion chamber and method for operating said combustion chamber

Marcel Stalder; Daniel Burri; Urs Benz


Archive | 2002

Method for igniting a thermal turbomachine

Marcel Stalder; Urs Benz; Franz Joos; Pirmin Schiessel; Jaan Hellat; Guenter Sybon


Archive | 2001

Combustor and method for operating the same

Marcel Stalder; Daniel Burri; Urs Benz


Archive | 1998

Ignition burner for a combustion chamber

Marcel Stalder; Günter Dr. Sybon


Archive | 2004

Method of operating a gas turbine with different fuels, and gas turbine.

Dieter Rebhan; Marcel Stalder


Archive | 1999

Damping device for the reduction of the oscillation amplitude of acoustic waves for a burner

Franz Joos; Marcel Stalder


Archive | 1996

Air-blast spray nozzle

Franz Joos; Marcel Stalder


Archive | 2003

Method for igniting the combustion chamber of a gas turbine installation and an ignition device for carrying out said method

Franz Joos; Marcel Stalder

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