Patents by Inventor Roderich Bryk

Roderich Bryk 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).

  • Axially segmented guide vane mount for a gas turbine
    Patent number: 8870526
    Abstract: A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.
    Type: Grant
    Filed: September 10, 2009
    Date of Patent: October 28, 2014
    Assignee: Siemens Aktiengesellschaft
    Inventors: Roderich Bryk, Sascha Dungs, Martin Hartmann, Uwe Kahlstorf, Karl Klein, Oliver Lüsebrink, Mirko Milazar, Nicolas Savilius, Oliver Schneider, Shilun Sheng, Vadim Shevchenko, Gerhard Simon, Norbert Thamm
  • Guide blade carrier
    Patent number: 8672616
    Abstract: A stator blade carrier, particularly for a gas turbine, is provided. The stator blade carrier includes a number of axial segments and is intended to attain a particularly high degree of operational reliability and long service life. To this end, two neighboring axial segments are connected to a number of tie rods, each enclosed by a support tube, wherein a spherical disk is arranged on at least one end of the respective support tube and mounted in a conical socket supported on the respective axial segment.
    Type: Grant
    Filed: September 16, 2009
    Date of Patent: March 18, 2014
    Assignee: Siemens Aktiengesellschaft
    Inventors: Roderich Bryk, Oliver Strohmeier
  • Axially segmented guide vane mount for a gas turbine
    Publication number: 20110268580
    Abstract: A stator blade carrier for a gas turbine is provided. The stator blade carrier includes a plurality of axial segments. At least one axial segment is designed as a tubular lattice structure. This allows a simpler design technically and a more flexible adaptation to the temperature profile present on the stator blade carrier to maintain operational safety.
    Type: Application
    Filed: September 10, 2009
    Publication date: November 3, 2011
    Inventors: Roderich Bryk, Sascha Dungs, Martin Hartmann, Uwe Kahlstorf, Karl Klein, Oliver Lüsebrink, Mirko Milazar, Nicolas Savilius, Oliver Schneider, Shilun Sheng, Vadim Shevchenko, Gerhard Simon, Norbert Thamm
  • Guide blade carrier
    Publication number: 20110236213
    Abstract: A stator blade carrier, particularly for a gas turbine, is provided. The stator blade carrier includes a number of axial segments and is intended to attain a particularly high degree of operational reliability and long service life. To this end, two neighboring axial segments are connected to a number of tie rods, each enclosed by a support tube, wherein a spherical disk is arranged on at least one end of the respective support tube and mounted in a conical socket supported on the respective axial segment.
    Type: Application
    Filed: September 16, 2009
    Publication date: September 29, 2011
    Inventors: Roderich Bryk, Oliiver Strohmeier
  • Gas turbine and method for damping oscillations of an annular combustion chamber
    Patent number: 6988366
    Abstract: A gas turbine includes an annular combustion chamber and an outer wall of an annular combustion chamber. A straining ring is arranged on the outer wall of the annular combustion chamber and enables oscillations of the outer wall to be damped via friction. The effects of combustion oscillations produced by damaging vibrations of the annular combustion chamber are thus reduced. A method is further for damping an oscillation of an outer wall of an annular combustion chamber.
    Type: Grant
    Filed: October 5, 2001
    Date of Patent: January 24, 2006
    Assignee: Siemens Aktiengesellschaft
    Inventors: Roderich Bryk, Otmar Gossmann, Harald Höll, Burkhard Voss
  • Gas turbine and method for damping oscillations of an annular combustion chamber
    Publication number: 20040025514
    Abstract: A gas turbine includes an annular combustion chamber and an outer wall of an annular combustion chamber. A straining ring is arranged on the outer wall of the annular combustion chamber and enables oscillations of the outer wall to be damped via friction. The effects of combustion oscillations produced by damaging vibrations of the annular combustion chamber are thus reduced. A method is further for damping an oscillation of an outer wall of an annular combustion chamber.
    Type: Application
    Filed: August 25, 2003
    Publication date: February 12, 2004
    Inventors: Roderich Bryk, Otmar Gobmann, Harald Holl, Burkhard Voss