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}
}
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