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:
Apr. 16, 2024

Filed:

May. 14, 2020
Applicant:

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

Inventors:

Mark J. Kuzdzal, Allegany, NY (US);

David J. Peer, Smethport, PA (US);

Marcus Meyer, Duisburg, DE;

Sebastian Huth, Mönchengladbach, DE;

James M. Sorokes, Olean, NY (US);

Kevin Miny, Essen, DE;

Martin Reimann, Essen, DE;

Roman Mensing, Düsseldorf, DE;

Jesus Pacheco, Houston, TX (US);

Steven Nove, Fulshear, TX (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 17/12 (2006.01); F04D 29/053 (2006.01); F04D 29/054 (2006.01); F04D 29/28 (2006.01); F04D 29/62 (2006.01);
U.S. Cl.
CPC ...
F04D 17/12 (2013.01); F04D 29/053 (2013.01); F04D 29/054 (2013.01); F04D 29/286 (2013.01); F04D 29/624 (2013.01);
Abstract

Compressor rotor structure and methodology for harmonizing compressor aerodynamics and rotordynamics are provided. Disclosed embodiments benefit from a compressor design effective for improving rotordynamics (e.g., stiffer rotor structure) without reducing a usable aerodynamics range of the compressor. This design may involve variation of the rotor structure along the rotor axis to locate respective surfaces defined by respective inlets of the one or more impellers at a varying distance relative to the rotor axis based on respective ratios selected for the configuration of the impeller bodies. This arrangement may be effective for improving rotordynamics while satisfactorily meeting the respective varying aerodynamics requirements at the various compression stages by the impeller bodies.


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