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Title: Resistive band for turbomachine blade

Patent ·
OSTI ID:1212404

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.

Research Organization:
General Electric Co., Schenectady, NY (United States)
Sponsoring Organization:
USDOE
DOE Contract Number:
FC26-05NT42643
Assignee:
General Electric Company (Schenectady, NY)
Patent Number(s):
9,115,584
Application Number:
13/454,979
OSTI ID:
1212404
Resource Relation:
Patent File Date: 2012 Apr 24
Country of Publication:
United States
Language:
English

References (11)

Root Pads For Composite Blades patent August 1973
Impact resistant blade patent January 1978
Composite fastener patent March 1992
Turbomachine blade made of composite material patent March 1994
Composite structure manufacture patent February 1996
Stitching head including needle guide for producing a reinforcement in a composite component patent May 1996
Method for producing a reinforcement in the form of a sheet for a composite component patent June 1998
Stitched composite fan blade patent August 2002
Tailored attachment mechanism for composite airfoils patent February 2005
Control of resin flow during molding of composite articles patent August 2007
Composite Fan Blade Dovetail Boot patent-application September 2011

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