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Title: Thin-walled reinforcement lattice structure for hollow CMC buckets

Abstract

A hollow ceramic matrix composite (CMC) turbine bucket with an internal reinforcement lattice structure has improved vibration properties and stiffness. The lattice structure is formed of thin-walled plies made of CMC. The wall structures are arranged and located according to high stress areas within the hollow bucket. After the melt infiltration process, the mandrels melt away, leaving the wall structure to become the internal lattice reinforcement structure of the bucket.

Inventors:
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1366729
Patent Number(s):
9689265
Application Number:
13/442,077
Assignee:
GENERAL ELECTRIC COMPANY
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:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2012 Apr 09
Country of Publication:
United States
Language:
English
Subject:
47 OTHER INSTRUMENTATION

Citation Formats

de Diego, Peter. Thin-walled reinforcement lattice structure for hollow CMC buckets. United States: N. p., 2017. Web.
de Diego, Peter. Thin-walled reinforcement lattice structure for hollow CMC buckets. United States.
de Diego, Peter. Tue . "Thin-walled reinforcement lattice structure for hollow CMC buckets". United States. https://www.osti.gov/servlets/purl/1366729.
@article{osti_1366729,
title = {Thin-walled reinforcement lattice structure for hollow CMC buckets},
author = {de Diego, Peter},
abstractNote = {A hollow ceramic matrix composite (CMC) turbine bucket with an internal reinforcement lattice structure has improved vibration properties and stiffness. The lattice structure is formed of thin-walled plies made of CMC. The wall structures are arranged and located according to high stress areas within the hollow bucket. After the melt infiltration process, the mandrels melt away, leaving the wall structure to become the internal lattice reinforcement structure of the bucket.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Jun 27 00:00:00 EDT 2017},
month = {Tue Jun 27 00:00:00 EDT 2017}
}

Works referenced in this record:

Blades for Mounting in Fluid Flow Ducts
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Composite ceramic gas turbine blade
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Bimetallic turbine airfoil
patent, September 1994


Hollow composite turbine blade
patent, April 1995


Double-wall airfoil
patent, May 1997


Gas turbine blisk with ceramic foam blades and its preparation
patent, April 2003


Cooling of gas turbine engine aerofoils
patent, August 2003


Cluster bridged casting core
patent, March 2010


Air cooled turbine airfoil with sequential impingement cooling
patent, May 2012


Turbine blade for use in a gas turbine
patent-application, February 2006


Cooling Systems For Stacked Laminate CMC Vane
patent-application, June 2007


Segmented Ceramic Matrix Composite Turbine Airfoil Component
patent-application, July 2010