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Title: Turbine blade with friction and impact vibration damping elements

Abstract

A turbine blade includes an airfoil body having an outer tip and a platform; and a part-span shroud positioned between the outer tip and the platform of the airfoil body. The part-span shroud has a first opening extending through the airfoil body and having a first inner surface. The airfoil body includes a second opening extending radially from the first opening and having a second inner surface. A first elongated vibration-damping element is disposed in the first opening, and a second elongated vibration-damping element disposed radially in the second opening. The second elongated vibration-damping element includes a free radially outer end and a radially inner end coupled to the first elongated vibration-damping element. The first elongated vibration-damping element frictionally damps vibration, and the second elongated vibration-damping element damps vibration using impact within the second opening.

Inventors:
; ;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1859935
Patent Number(s):
11143036
Application Number:
16/998,207
Assignee:
General Electric Company (Schenectady, NY)
Patent Classifications (CPCs):
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
F - MECHANICAL ENGINEERING F05 - INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04 F05D - INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
DOE Contract Number:  
FE0031613
Resource Type:
Patent
Resource Relation:
Patent File Date: 08/20/2020
Country of Publication:
United States
Language:
English

Citation Formats

Zhang, James, Wondrasek, Michael Anthony, and Delvaux, John McConnell. Turbine blade with friction and impact vibration damping elements. United States: N. p., 2021. Web.
Zhang, James, Wondrasek, Michael Anthony, & Delvaux, John McConnell. Turbine blade with friction and impact vibration damping elements. United States.
Zhang, James, Wondrasek, Michael Anthony, and Delvaux, John McConnell. Tue . "Turbine blade with friction and impact vibration damping elements". United States. https://www.osti.gov/servlets/purl/1859935.
@article{osti_1859935,
title = {Turbine blade with friction and impact vibration damping elements},
author = {Zhang, James and Wondrasek, Michael Anthony and Delvaux, John McConnell},
abstractNote = {A turbine blade includes an airfoil body having an outer tip and a platform; and a part-span shroud positioned between the outer tip and the platform of the airfoil body. The part-span shroud has a first opening extending through the airfoil body and having a first inner surface. The airfoil body includes a second opening extending radially from the first opening and having a second inner surface. A first elongated vibration-damping element is disposed in the first opening, and a second elongated vibration-damping element disposed radially in the second opening. The second elongated vibration-damping element includes a free radially outer end and a radially inner end coupled to the first elongated vibration-damping element. The first elongated vibration-damping element frictionally damps vibration, and the second elongated vibration-damping element damps vibration using impact within the second opening.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2021},
month = {10}
}

Works referenced in this record:

Self-tuning impact damper for rotating blades
patent, December 2004


Damping device for composite blade
patent, November 2011


Internally damped airfoiled component and method
patent, June 2020


Damper Pin for a Turbine Blade
patent-application, March 2017


Vibration Damping Coatings
patent, September 1973


Damped turbine engine frame
patent, February 1994


Structures for damping of turbine components
patent-application, February 2009


Gas Turbine Blade with Intra-Spin Snubber and Manufacturing Method for Producing the Same
patent-application, February 2012


Turbine blade damping
patent, July 1975


Piezo Actuated High Speed Air Valve Used for Blade and Component Excitation
patent-application, February 2018


Turbine blade with vibration damper
patent-application, April 2007


Programmable jet blade excitation system
patent, October 1988


Vibration-Suppressed Blade
patent, August 1973


Damped airfoil blade
patent, November 1992


Flat Bottom Damper Pin For Turbine Blades
patent-application, March 2014


Constrained layer, composite, acoustic damping material
patent-application, February 2006


Cooled snubber structure for turbine blades
patent, April 2014


Gas turbine blade with intra-span snubber
patent, July 2014


Turbine blade assembly with pin dampers
patent, January 2004


Bucket assembly for use in a turbine engine
patent, April 2017


Self retaining blade damper
patent, January 2001


Aerodynamic damping of vibrations in rotor blades
patent, July 1985


Turbine blade platform damper
patent, June 1993


Gas Turbine Engine with Airfoil Dampening System
patent-application, September 2016


Vibration damper coating
patent-application, April 2007


Damping arrangement for a blade of an axial turbine
patent, November 2007


Internally Damped Airfoiled Component and Method
patent-application, March 2016


Cooled Snubber Structure for Turbine Blades
patent-application, August 2011


Damping Apparatus
patent, September 1961


Vibration Damper for Blades and Vanes
patent, September 1954


Bucket Assembly for Use in a Turbine Engine
patent-application, April 2015


Damping arrangement for a blade of an axial turbine
patent-application, November 2007