DOE Patents title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: Method of forming a ceramic matrix composite and a ceramic matrix component

Abstract

A method of forming a ceramic matrix composite component includes providing a formed ceramic member having a cavity, filling at least a portion of the cavity with a ceramic foam. The ceramic foam is deposited on a barrier layer covering at least one internal passage of the cavity. The method includes processing the formed ceramic member and ceramic foam to obtain a ceramic matrix composite component. Also provided is a method of forming a ceramic matrix composite blade and a ceramic matrix composite component.

Inventors:
;
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1360965
Patent Number(s):
9663404
Application Number:
13/342,498
Assignee:
General Electric Company
Patent Classifications (CPCs):
C - CHEMISTRY C04 - CEMENTS C04B - LIME, MAGNESIA
F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
DOE Contract Number:  
FC26-05NT42643
Resource Type:
Patent
Resource Relation:
Patent File Date: 2012 Jan 03
Country of Publication:
United States
Language:
English
Subject:
36 MATERIALS SCIENCE

Citation Formats

de Diego, Peter, and Zhang, James. Method of forming a ceramic matrix composite and a ceramic matrix component. United States: N. p., 2017. Web.
de Diego, Peter, & Zhang, James. Method of forming a ceramic matrix composite and a ceramic matrix component. United States.
de Diego, Peter, and Zhang, James. Tue . "Method of forming a ceramic matrix composite and a ceramic matrix component". United States. https://www.osti.gov/servlets/purl/1360965.
@article{osti_1360965,
title = {Method of forming a ceramic matrix composite and a ceramic matrix component},
author = {de Diego, Peter and Zhang, James},
abstractNote = {A method of forming a ceramic matrix composite component includes providing a formed ceramic member having a cavity, filling at least a portion of the cavity with a ceramic foam. The ceramic foam is deposited on a barrier layer covering at least one internal passage of the cavity. The method includes processing the formed ceramic member and ceramic foam to obtain a ceramic matrix composite component. Also provided is a method of forming a ceramic matrix composite blade and a ceramic matrix composite component.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2017},
month = {5}
}

Works referenced in this record:

Safety Device for Elevators
patent, July 1895


Composite ceramic gas turbine blade
patent, August 1981


Hollow composite turbine blade
patent, April 1995


Exhaust manifold with integral catalytic converter
patent, December 1997


Ceramic catalytic converter
patent, March 1999


Structure with ceramic foam thermal barrier coating, and its preparation
patent, August 2002


Gas turbine stationary shroud made of a ceramic foam material, and its preparation
patent, August 2002


Method of manufacturing a ceramic matrix composite
patent, December 2002


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


Turbine blade or turbine vane made of a ceramic foam joined to a metallic nonfoam, and preparation thereof
patent, November 2003


High temperature resistant airfoil apparatus for a hypersonic space vehicle
patent, January 2004


Golf club and other structures, and novel methods for making such structures
patent, April 2004


Thermal barrier coating
patent, May 2004


Turbine blade with ceramic foam blade tip seal, and its preparation
patent, June 2004


Thermal barrier coating material, gas turbine parts and gas turbine
patent, July 2005


Doppler radar sensing system for monitoring turbine generator components
patent, August 2006


Investment casting
patent, December 2006


Turbine blade for extreme temperature conditions
patent, March 2007


Thermal barrier coating with reduced sintering and increased impact resistance, and process of making same
patent, December 2007


Thermal barrier coating system method of manufacturing the same
patent, April 2008


Airfoil support
patent, August 2008


Functionally gradient SiC/SiC ceramic matrix composites with tailored properties for turbine engine applications
patent, October 2009


CMC articles having small complex features
patent, October 2009


Turbine bucket tip cap
patent, November 2010


Process of producing a ceramic matrix composite article and article formed thereby
patent, October 2011


Gas turbine shroud support apparatus
patent, November 2011


Coated turbine blade
patent, December 2011


Ceramic oxide pre-forms, metal matrix composites, and methods for making the same
patent-application, June 2002


High temperature resistant airfoil apparatus for a hypersonic space vehicle
patent-application, March 2004


Integrated ceramic/metallic components and methods of making same
patent-application, November 2005


Ceramic foam-filled sandwich panels and method
patent-application, November 2007


Composite Structures having Reinforced Edge Bonded Joints and Method for Making the Same
patent-application, January 2009


Foamed Tools
patent-application, April 2010


Heat-Managing Composite Structures
patent-application, September 2010


Ceramic Matrix Composite Blade Having Integral Platform Structures And Methods Of Fabrication
patent-application, February 2011


Methods of Making Filter Apparatus and Fabricating a Porous Ceramic Article
patent-application, May 2012


Annulus Filler System
patent-application, October 2012


Hot Gas Path Component for Turbine System
patent-application, April 2013


Ceramic Matrix Composite, Method Of Making A Ceramic Matrix Composite, And A Pre-Preg Composite Ply
patent-application, April 2014


Cooled Ceramic Matrix Composite Airfoil
patent-application, September 2014


Hot Gas Path Component For Turbine System
patent-application, October 2014


Composite Blades for Gas Turbine Engines
patent-application, May 2016