Alstom Technology Limited

Abb Schweiz Ag

Christopher Ganz

Wolfgang Weisenstein

Mehmet Mercangoez

Ioannis Lymperopoulos

Andrea Cortinovis

In a gas turbine having a combustion chamber ( ) and a first row of guide vanes ( ) arranged on the outflow side of the combustion chamber ( ), a plurality of temperature sensors ( ) for measuring temperature value, and a plurality of means ( ) for introducing fuel into the combustion chamber ( ), which means can be controlled on the basis of the temperature values, the temperature sensors ( ) are spectrometers, are designed to measure a combustion-gas temperature and are arranged so as to measure a gas temperature which prevails immediately in front of the first row of guide vanes ( ).

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Zurich, Switzerland

Christopher Ganz