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:
Aug. 02, 2022

Filed:

Dec. 20, 2018
Applicant:

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

Inventor:

Yuekun Zhou, Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/10 (2006.01); F01D 5/22 (2006.01); F01D 5/26 (2006.01); F01D 5/30 (2006.01); F01D 25/06 (2006.01);
U.S. Cl.
CPC ...
F01D 5/10 (2013.01); F01D 5/22 (2013.01); F01D 5/26 (2013.01); F01D 5/3007 (2013.01); F01D 25/06 (2013.01); F05D 2230/60 (2013.01); F05D 2230/70 (2013.01); F05D 2230/72 (2013.01); F05D 2230/80 (2013.01); F05D 2260/961 (2013.01); F05D 2300/6033 (2013.01);
Abstract

A bladed rotor system for a turbomachine includes a circumferential row of blades mounted on a rotor disc, and includes a plurality of under-platform dampers. Each damper is located between adjacent blade platforms. The plurality of dampers includes a first set of dampers and a second set of dampers. The dampers of the first set are distinguished from the dampers of the second set by a cross-sectional material distribution in the damper that is unique to the respective set. Dampers of the first set and the second set are positioned alternately in a periodic fashion in a circumferential direction, to provide a frequency mistuning to stabilize flutter of the blades.


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