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:
Jul. 16, 2024

Filed:

May. 14, 2020
Applicant:

Siemens Energy Global Gmbh & Co. KG, Munich, DE;

Inventors:

Kevin Miny, Essen, DE;

Christian Rickelt, Duisburg, DE;

Bernhard Langenfeld, Mülheim an der Ruhr, DE;

Florian Kretschmer, Fuldabrück, DE;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/26 (2006.01); F04D 17/12 (2006.01); F04D 29/054 (2006.01); F04D 29/62 (2006.01); F16D 1/076 (2006.01);
U.S. Cl.
CPC ...
F04D 29/266 (2013.01); F04D 17/122 (2013.01); F04D 29/054 (2013.01); F04D 29/624 (2013.01); F16D 1/076 (2013.01);
Abstract

Rotor structure for a turbomachine, such as a centrifugal compressor, is provided. Disclosed embodiments make use of structural and/or operational relationships (e.g., distinct axially-extending zones in the radially-inner contour of respective impeller bodies configured to balance mass distribution about a rotor axis) designed to control relative radial and/or axial growth between corresponding interface locations along the rotor axis at which corresponding faces of respective hirth couplings mesh with one another. The ability to control relative radial and/or axial growth between corresponding interface locations may be effective for reducing rotor vibration and/or to establish more reliable contact patterns and reduced levels of mechanical stresses and distortion (e.g., angular distortion) at the hirth coupling interfaces.


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