Resistive band for turbomachine blade
Abstract
A turbomachine system includes a rotor that defines a longitudinal axis of the turbomachine system. A first blade is coupled to the rotor, and the first blade has first and second laminated plies. A first band is coupled to the first blade and is configured to resist separation of the first and second laminated plies.
- Inventors:
- Issue Date:
- Research Org.:
- General Electric Company, Schenectady, NY (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 1212404
- Patent Number(s):
- 9,115,584
- Application Number:
- 13/454,979
- Assignee:
- General Electric Company (Schenectady, NY)
- DOE Contract Number:
- FC26-05NT42643
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 2012 Apr 24
- Country of Publication:
- United States
- Language:
- English
- Subject:
- 42 ENGINEERING
Citation Formats
Roberts, Herbert Chidsey, and Taxacher, Glenn Curtis. Resistive band for turbomachine blade. United States: N. p., 2015.
Web.
Roberts, Herbert Chidsey, & Taxacher, Glenn Curtis. Resistive band for turbomachine blade. United States.
Roberts, Herbert Chidsey, and Taxacher, Glenn Curtis. Tue .
"Resistive band for turbomachine blade". United States. https://www.osti.gov/servlets/purl/1212404.
@article{osti_1212404,
title = {Resistive band for turbomachine blade},
author = {Roberts, Herbert Chidsey and Taxacher, Glenn Curtis},
abstractNote = {A turbomachine system includes a rotor that defines a longitudinal axis of the turbomachine system. A first blade is coupled to the rotor, and the first blade has first and second laminated plies. A first band is coupled to the first blade and is configured to resist separation of the first and second laminated plies.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2015},
month = {8}
}
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