METHOD AND APPARATUS FOR REGULATING THE FUNCTIONING OF A GAS TURBINE COMBUSTOR

The method involves comparing a detected control variable with a preset reference variable for determining a correcting variable. The determined correcting variable is output to one adjusting device e.g. adjusting valves and guide vane assembly, influencing air- and/or fuel supply to a combustion ch...

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Bibliographische Detailangaben
Hauptverfasser:	DIEBELS, ANDREAS, LEPERS, JOACHIM, MUELLER, MARTIN, DEUKER, EBERHARD, BAUER, ANDREAS, STURM, BERTHOLD, PERNAU, STEFAN, PRADE, BERND, SCHNEIDER, PETER-ANDREAS, WARNACK, DIETER, HESSE, THOMAS, SIMON, DIETER, BODE, SIEGFRIED, KREBS, WERNER, HAHNER, THOMAS, THOELKING, HEINRICH
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING REGULATING OR CONTROLLING COMBUSTION WEAPONS
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Beschreibung
Zusammenfassung:	The method involves comparing a detected control variable with a preset reference variable for determining a correcting variable. The determined correcting variable is output to one adjusting device e.g. adjusting valves and guide vane assembly, influencing air- and/or fuel supply to a combustion chamber (12), such that an approximation of the flame generated in the chamber to the stability limit is derived from the control variable. The correcting variable is determined by a regulator (29) based on a received measurement variable and its deviation from a reference variable. An independent claim is also included for a device for regulating the course of a gas turbine plant.