Mtu Aero Engines Gmbh

Man Energy Solutions Se

Mtu Aero Engines Ag

Harald Passrucker

Roland Wunderer

Sergio Elorza Gomez

Rudolf Konrad Selmeier

Bjoern Grueber

Peter Eibelshauser

Manfred Dupslaff

Klaus Breitschwerdt

Thorsten Poehler

Wilfried Schutte

A compressor, in particular, of a turbomachine. The compressor comprises at least one blade ring and at least two ring segments, wherein the blade ring has at least two equally large ring segments. The compressor also comprises blades, which are arranged in the ring segments of the blade ring in such a way that a first number of blades is arranged in a first ring segment and a second number of blades is arranged in a second ring segment. The first number of blades is not equal to the second number of blades.

Compressor

A blading for a turbomachine, particularly for a gas turbine, wherein thickened areas and depressions are formed and disposed on a lateral wall having a plurality of blades such that at least one depression or thickened area is disposed at a blade pressure side and at least one thickened area or depression is disposed at a blade suction side for each blade of the plurality of blades.

Blading

A blading for a turbomachine, particularly for a gas turbine, wherein thickened areas and depressions formed and disposed on a lateral wall having a plurality of blades such that at least one depression is disposed on a blade pressure side and at least one thickened area is disposed on a blade suction side for each blade of the plurality of blades.

The present invention relates to a blade of a turbomachine, in particular an adjustable guide blade or vane of a gas turbine, having at least one thickened area () on a pressure side (D) of the blade profile (P), wherein the thickened area () is disposed in a radially outer-lying, housing-side region of the blade (), wherein the thickened area () is designed at a distance from a front edge () and a rear edge () of the blade ().

Blade

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Munich, Germany

Harald Passrucker