Siemens Aktiengesellschaft

Vadim Shevchenko

Walter Loch

Peter Schröder

Mirko Milazar

Oliver Schneider

Sascha Dungs

Francois Benkler

Martin Hartmann

Bernd Vonnemann

Uwe Kahlstorf

Nicolas Savilius

Thomas-Dieter Tenrahm

Uwe Sieber

Norbert Thamm

Gerhard Simon

Oliver Lüsebrink

Shilun Sheng

Torsten Matthias

Roderich Bryk

Karl Klein

Sabine Rintzel

Markus Paus

Werner Polanz

Joachim Simmchen

Bernd Pollack

Joachim Braun

Alexandra Küpper

Achim Schirrmacher

Peter Schroeder

Markus Hofmann

Thomas Brandenburg

Frank Mildner

Bernward Mertens

Daniel Ecke

Thomas Tenrahm

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

The invention relates to a device for support of an adjusting ring which encompasses at a distance a basically circular blade carrier, which adjusting ring is rotatable in the circumferential direction around a center axis which is identical with the blade carrier, in order to adjust radially extending blades of a ring of a turbo-engine, wherein a plurality of levers are provided between the blade carrier and the adjusting ring, which levers are distributed over the circumference, extend tangentially in each case, and which on their free ends have a rotatable roller in each case, which are rollable in the circumferential direction on the adjusting ring or on the blade carrier. According to the invention, the lever is tightly clamped on one side to disclose a wear-free and reliable device for support of an adjusting ring which encompasses at a distance a circular blade carrier.

Device for support of an adjusting ring which encompasses at a distance a circular blade carrier

The invention refers to a device for determining the angular position of a compressor stator blade, which is rotatable around its longitudinal axis and arranged in a compressor, with which is associated a measuring surface which rotates synchronously with it. For a reliable, simple and approximately error-free recording of the angular positions, the angular position of the compressor stator blade can be determined via the device in an automated manner. For this purpose, it has at least one mounting unit provided for aligned fastening of the device on the compressor, and at least one measuring and evaluating unit which comprises at least two distance sensors which each record a distance to the measuring surface which is rotatable from the reference position, as a result the angular position of the measuring surface, relative to the reference position depends upon the two recorded distances, is determined by the measuring and evaluating unit.

Device for determining the angular position of a rotatable compressor stator blade

A device () for the demounting of blades (), which are pushed in with a blade root () on a wheel disk () of a blade wheel () of a turbine or of a compressor, is designed with a support () which is designed to be brought to bear against at least one component of the turbine, and is designed with an actuator () which is coupled to the support () and is designed for moving the blade root () mechanically out of the wheel disk ().

Device for the demounting of blades of a turbine or of a compressor

Growing community of inventors

Dortmund, Germany

Vadim Shevchenko