Siemens Aktiengesellschaft

Roderich Bryk

Mirko Milazar

Oliver Schneider

Sascha Dungs

Uwe Kahlstorf

Nicolas Savilius

Norbert Thamm

Gerhard Simon

Martin Hartmann

Vadim Shevchenko

Shilun Sheng

Oliver Lüsebrink

Otmar Gossmann

Karl Klein

Burkhard Voss

Oliver Strohmeier

Harald Höll

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.

Axially segmented guide vane mount for a gas turbine

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.

Guide blade carrier

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.

Gas turbine and method for damping oscillations of an annular combustion chamber

Growing community of inventors

Düren, Germany

Roderich Bryk