The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Jan. 26, 2016

Filed:

Jul. 20, 2011
Applicants:

Stefan Braun, Neukirchen-Vluyn, DE;

Christopher Butzeck, Mülheim, DE;

Jürgen Hahn, Bochum, DE;

Peter Schröder, Essen, DE;

Hubertus Michael Wigger, Köln, DE;

Inventors:

Stefan Braun, Neukirchen-Vluyn, DE;

Christopher Butzeck, Mülheim, DE;

Jürgen Hahn, Bochum, DE;

Peter Schröder, Essen, DE;

Hubertus Michael Wigger, Köln, DE;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/02 (2006.01); F01D 11/22 (2006.01); F16D 1/10 (2006.01);
U.S. Cl.
CPC ...
F01D 5/026 (2013.01); F01D 11/22 (2013.01); F16D 1/101 (2013.01); F05D 2260/37 (2013.01); F16D 2001/103 (2013.01);
Abstract

A gas turbine rotor for a gas turbine is provided. The gas turbine rotor includes a compressor rotor shaft, a turbine rotor shaft and a coupling device frictionally connecting the two rotor shafts, wherein the coupling device is designed in such a way that the friction connection also exists when the two rotor shafts are displaced relative to one another. In this case, the turbine rotor shaft is lengthened at the end facing the compressor rotor shaft in such a way that the turbine rotor shaft overlaps with the compressor rotor shaft in the axial direction and the coupling device connects this lengthened end of the turbine shaft to the compressor rotor shaft in the radial direction.


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