Patents by Inventor Siegfried Bode

Siegfried Bode has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Patent number: 9086219
    Abstract: 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.
    Type: Grant
    Filed: May 10, 2006
    Date of Patent: July 21, 2015
    Assignee: SIEMENS AKTIENGESELLSCHAFT
    Inventors: Eberhard Deuker, Stefan Pernau, Siegfried Bode, Andreas Diebels, Thomas Hahner, Thomas Hesse, Werner Krebs, Bernd Prade, Peter-Andreas Schneider, Dieter Simon, Berthold Sturm, Heinrich Thölking, Dieter Warnack, Andreas Bauer, Joachim Lepers, Martin Müller
  • Publication number: 20130104554
    Abstract: A burner assembly for a gas turbine is provided. The burner assembly has a combustor, a centrally arranged pilot burner and plurality of main burners surrounding the pilot burner. Each main burner has a cylindrical housing having a lance which is centrally arranged therein and has a fuel channel for liquid fuel. The lance is supported on the housing by swirl blades and an attachment is arranged on the lance in the direction of the combustor. The liquid fuel nozzle is arranged in the attachment downstream of the swirl blades and connected to the fuel channel. For the improved mixing of the fuel with the air, the liquid fuel nozzle is designed as a full jet nozzle and the full jet nozzle has a length and a diameter, the ratio of the length to the diameter is at least 1.5.
    Type: Application
    Filed: July 1, 2011
    Publication date: May 2, 2013
    Inventors: Siegfried Bode, Timothy A. Fox, Thomas Grieb, Matthias Hase, Jürgen Meisl, Sebastian Pfadler
  • Publication number: 20090301097
    Abstract: 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.
    Type: Application
    Filed: May 10, 2006
    Publication date: December 10, 2009
    Inventors: Eberhard Deuker, Stefan Pernau, Siegfried Bode, Andreas Diebels, Thomas Hahner, Thomas Hesse, Werner Krebs, Bernd Prade, Peter-Andreas Schneider, Dieter Simon, Berthold Sturm, Heinrich Thölkin, Dieter Warnack, Andreas Bauer, Joachim Lepers, Martin Müller