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Title: Turbomachine blade reinforcement

Patent ·
OSTI ID:1321818

Embodiments of the present disclosure include a system having a turbomachine blade segment including a blade and a mounting segment coupled to the blade, wherein the mounting segment has a plurality of reinforcement pins laterally extending at least partially through a neck of the mounting segment.

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):
9,435,209
Application Number:
13/660,989
OSTI ID:
1321818
Resource Relation:
Patent File Date: 2012 Oct 25
Country of Publication:
United States
Language:
English

References (8)

Composite airfoil with woven insert patent January 1994
Composite with through the thickness reinforcement patent November 1995
Method for joining composite materials patent August 2000
Ceramic matrix composite having improved interlaminar strength patent September 2003
Through thickness reinforcement of SiC/SiC CMC's through in-situ matrix plugs manufactured using fugitive fibers patent June 2009
Hollow CMC airfoil with internal stitch patent October 2009
Ceramic Matrix Composite Wall With Post Laminate Stitching patent-application January 2010
Ceramic Matrix Composite Blade Having Integral Platform Structures And Methods Of Fabrication patent-application February 2011

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