Man Diesel & Turbo Se

Man Turbo Ag

Man Turbomaschinen Ag Ghh Borsig

Michael Blaswich

Emil Aschenbruck

Jaman El Masalme

Andreas Kleinefeldt

Frank Reiss

Ulrich Orth

William F Cline

Ralf Müller

A turbomachine includes: a stator-side housing having: a plurality of stator-side guide vane supports fastened to the stator-side housing, stator-side guide vanes fastened to the stator-side guide vane supports, and axially spaced guide vane rings; and a rotor having a plurality of rotor-side moving blades. At least two guide vane supports are jointly fastened to and centered on a flange of the stator-side housing.

Turbomachine

A sealing segment for sealingly connecting two structural components parts which are movable relative to one another, with two sealing bodies which are connected to one another by a web and which can be arranged in recesses of the structural component parts in an articulated manner, and a sealing segment arrangement with a plurality of sealing segments of this type, and a flow machine with a sealing segment arrangement of this type.

Sealing segment and sealing-segment arrangement

A multipart bladed rotor () for a flow machine, particularly a gas turbine or steam turbine or an axial compressor, has at least two disks () whose front sides, which face one another, are connected to one another, particularly by positive engagement, in a separating plane () so as to be fixed with respect to rotation relative to one another, wherein a groove () for receiving a blade root () of at least one rotor blade is formed in the separating plane.

Multi-component bladed rotor for a turbomachine

A turbine rotor () for a gas turbine with a one-piece compressor housing () or a compressor housing () which is divided in a first plane, a one-piece turbine housing () connected to the compressor housing () or a turbine housing () which is divided in a second plane different from the first plane comprises a compressor area which includes at least two compressor disks (-) and a turbine area which includes at least one turbine disk (). The compressor disks and turbine disks are clamped together by a tie rod arrangement which includes at least one tie rod () which has a first fastening area, a second fastening area for clamping at least two compressor disks between the first fastening area and the second fastening area, and a third fastening area for clamping at least one turbine disk.

Turbine rotor for a gas turbine

The rotor () of a gas turbine containing a compressor part () and a turbine part () is mounted in an axial thrust bearing () and in two radial journal bearings (). One of the bearings is a journal bearing () arranged in the intake area of the compressor part () and the other journal bearing () together with the thrust bearing () is arranged in the area of the turbine part ().

Mounting of the rotor of a gas turbine

A pipeline duct through a discharge opening (,) of a vane support housing (,) and an opening (,) in an outer wall (,) of a compressor housing of a gas turbine. The upper part of the pipe (,) is firmly clamped with a flange (,) and seals (,) between the bleeder connection (,) and the outer wall (,) by means of fastening elements (,). The lower part of the pipe (,) is sealed by a piston ring (,). The piston ring (,) is guided by two fastening rings (,), which are mounted in the vane support housing (,) by fastening elements (,). The fastening rings (,) make possible a free movement of the pipe (,) and the housing (,) in relation to the vane support housing (,) in the horizontal direction due to their free spaces (,).

Growing community of inventors

Oberhausen, Germany

Michael Blaswich