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:
Jun. 15, 2010

Filed:

Apr. 10, 2007
Applicants:

Randall Charles Bauer, Loveland, OH (US);

Gregory Terrence Garay, West Chester, OH (US);

Matthew Mark Weaver, Loveland, OH (US);

James Robert Bailey, Cincinnati, OH (US);

Bruce Clark Busbey, Greer, SC (US);

Inventors:

Randall Charles Bauer, Loveland, OH (US);

Gregory Terrence Garay, West Chester, OH (US);

Matthew Mark Weaver, Loveland, OH (US);

James Robert Bailey, Cincinnati, OH (US);

Bruce Clark Busbey, Greer, SC (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/26 (2006.01);
U.S. Cl.
CPC ...
Abstract

A turbine rotor blade includes a hollow airfoil joined to a platform and dovetail. A main flow channel extends longitudinally in span through the blade and is bound chordally by opposite partitions transversely bridging opposite sidewalls of the airfoil. A damper rib and transversely opposite damper pad are arranged together in a plurality of pairs spaced longitudinally apart in the airfoil and chordally positioned intermediate to the partitions to provide unobstructed forward and aft portions of the flow channel for channeling a coolant therethrough. The damper ribs and pads are configured to receive a wire damper through the channel to locally dampen vibration while minimizing obstruction of the coolant flow therethrough.


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