Blade and airfoil damping configurations
Abstract
The present embodiments set forth a blade including an airfoil, the airfoil including a tip cap, a pressure sidewall and a suction sidewall extending axially between corresponding leading and trailing edges and radially between the base and the tip cap. The blade, including the airfoil and base, being formed in at least two airfoil parts, each of the two airfoil parts including contacting edges engaging each other respective contacting edges, the contacting edges defining a joint for preloading each of the at least two parts with each other and with the base. The at least two airfoil parts forming the airfoil being retained to each other by an interference fit at the joint. The interference fit providing frictional damping of vibrations in the blade during blade operation.
- Inventors:
- Issue Date:
- Research Org.:
- General Electric Co., Schenectady, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1892954
- Patent Number(s):
- 11339665
- Application Number:
- 16/816,568
- 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: 03/12/2020
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Hart, Andrew Clifford, Li, Jing, Chakrabarti, Suryarghya, Balkcum, III, James Tyson, and Feigl, Markus. Blade and airfoil damping configurations. United States: N. p., 2022.
Web.
Hart, Andrew Clifford, Li, Jing, Chakrabarti, Suryarghya, Balkcum, III, James Tyson, & Feigl, Markus. Blade and airfoil damping configurations. United States.
Hart, Andrew Clifford, Li, Jing, Chakrabarti, Suryarghya, Balkcum, III, James Tyson, and Feigl, Markus. Tue .
"Blade and airfoil damping configurations". United States. https://www.osti.gov/servlets/purl/1892954.
@article{osti_1892954,
title = {Blade and airfoil damping configurations},
author = {Hart, Andrew Clifford and Li, Jing and Chakrabarti, Suryarghya and Balkcum, III, James Tyson and Feigl, Markus},
abstractNote = {The present embodiments set forth a blade including an airfoil, the airfoil including a tip cap, a pressure sidewall and a suction sidewall extending axially between corresponding leading and trailing edges and radially between the base and the tip cap. The blade, including the airfoil and base, being formed in at least two airfoil parts, each of the two airfoil parts including contacting edges engaging each other respective contacting edges, the contacting edges defining a joint for preloading each of the at least two parts with each other and with the base. The at least two airfoil parts forming the airfoil being retained to each other by an interference fit at the joint. The interference fit providing frictional damping of vibrations in the blade during blade operation.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2022},
month = {5}
}
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