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Title: 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}
}

Patent:

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