Siemens Aktiengesellschaft

Siemens Energy, Inc.

Joachim Lepers

Bernd Prade

Clifford E Johnson

Werner Krebs

Samer P Wasif

Eberhard Deuker

Andreas Bauer

Peter-Andreas Schneider

Martin Müller

Berthold Sturm

Dieter Simon

Andreas Diebels

Thomas Hesse

Dieter Warnack

Heinrich Thölking

Thomas Hahner

Siegfried Bode

Stefan Pernau

Martin Mueller

Heinrich Thoelking

A regulating device for regulating the course of a gas turbine plant has at least one sensor for sensing a measurement variable and for outputting a measurement signal which represents the measurement variable; at least one adjusting system for influencing air and/or fuel supply to a combustion chamber of the gas turbine plant on the basis of a correcting variable; and a regulator connected to the at least one sensor so as to receive the measurement variable and to the at least one adjusting system for outputting the correcting variable, the regulator being designed to determine the correcting variable on the basis of the measurement variable received and its deviation from a pilot variable. At least one sensor is designed to sense the variation in time of at least one burner or combustion chamber parameter as measurement variable.

Method and device for regulating the operating line of a gas turbine combustion chamber

A combustor assembly is provided comprising a combustor casing; a liner coupled to the combustor casing; a burner assembly coupled to the combustor casing; and at least one resonator assembly. The resonator assembly comprises a resonator outer plate having at least one opening, a resonator side wall coupled to the resonator outer plate, and a resonator inner plate defined by a portion of the liner. The resonator inner plate is coupled to the resonator side wall and has at least one slot formed therein having an aspect ratio of at least 4:1.

Combustor assembly including one or more resonator assemblies and process for forming same

Growing community of inventors

Düsseldorf, Germany

Joachim Lepers