Invention Grant
- Patent Title: Damper pin for a turbine blade
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Application No.: US14844317Application Date: 2015-09-03
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Publication No.: US10385701B2Publication Date: 2019-08-20
- Inventor: Spencer A. Kareff , Brian Denver Potter , Ariel Caesar Prepena Jacala
- Applicant: General Electric Company
- Applicant Address: US NY Schenectady
- Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee: GENERAL ELECTRIC COMPANY
- Current Assignee Address: US NY Schenectady
- Agency: Dority & Manning, P.A.
- Main IPC: F01D5/22
- IPC: F01D5/22

Abstract:
A damper pin for damping adjacent turbine blades coupled to a rotor shaft includes a first end portion that is axially spaced from a second end portion and a spring member that extends axially from an inner surface of the first end portion to an inner surface of the second end portion. The first end portion, the spring member and the second end portion define a generally arcuate top portion of the damper pin. The top portion is configured to contact with a groove defined between the adjacent turbine blades.
Public/Granted literature
- US20170067348A1 DAMPER PIN FOR A TURBINE BLADE Public/Granted day:2017-03-09
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