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Title: Nozzle assembly and method for forming nozzle assembly

Abstract

A nozzle assembly is disclosed, including a CMC nozzle shell, a nozzle spar, and an endwall. The CMC nozzle shell includes a CMC composition and an interior cavity. The nozzle spar is partially disposed within the interior cavity and includes a metallic composition, a cross-sectional conformation, a plurality of spacers protruding from the cross-sectional conformation, the plurality of spacers contacting the CMC nozzle shell, and a spar cap. The endwall includes at least one surface in lateral contact with the spar cap and maintains a lateral orientation of the CMC nozzle shell and the nozzle spar relative to the endwall. The lateral orientation maintains a predetermined throat area of the nozzle assembly. A method for forming the nozzle assembly includes inserting the nozzle spar into the interior cavity, rotating the CMC nozzle shell and the nozzle spar laterally relative to the endwall, and maintaining the lateral orientation.

Inventors:
Issue Date:
Research Org.:
General Electric Co., Schenectady, NY (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1771686
Patent Number(s):
10851658
Application Number:
15/425,545
Assignee:
General Electric Company (Schenectady, NY)
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:  
FE0024006
Resource Type:
Patent
Resource Relation:
Patent File Date: 02/06/2017
Country of Publication:
United States
Language:
English

Citation Formats

Hafner, Matthew Troy. Nozzle assembly and method for forming nozzle assembly. United States: N. p., 2020. Web.
Hafner, Matthew Troy. Nozzle assembly and method for forming nozzle assembly. United States.
Hafner, Matthew Troy. Tue . "Nozzle assembly and method for forming nozzle assembly". United States. https://www.osti.gov/servlets/purl/1771686.
@article{osti_1771686,
title = {Nozzle assembly and method for forming nozzle assembly},
author = {Hafner, Matthew Troy},
abstractNote = {A nozzle assembly is disclosed, including a CMC nozzle shell, a nozzle spar, and an endwall. The CMC nozzle shell includes a CMC composition and an interior cavity. The nozzle spar is partially disposed within the interior cavity and includes a metallic composition, a cross-sectional conformation, a plurality of spacers protruding from the cross-sectional conformation, the plurality of spacers contacting the CMC nozzle shell, and a spar cap. The endwall includes at least one surface in lateral contact with the spar cap and maintains a lateral orientation of the CMC nozzle shell and the nozzle spar relative to the endwall. The lateral orientation maintains a predetermined throat area of the nozzle assembly. A method for forming the nozzle assembly includes inserting the nozzle spar into the interior cavity, rotating the CMC nozzle shell and the nozzle spar laterally relative to the endwall, and maintaining the lateral orientation.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {Tue Dec 01 00:00:00 EST 2020},
month = {Tue Dec 01 00:00:00 EST 2020}
}

Works referenced in this record:

Nozzle Guide Vane with Composite Heat Shields
patent-application, January 2017


Turbine Nozzle Assembly
patent-application, July 2011


Gas turbine vane platform element
patent, August 2012


Turbine Engines with Ceramic Vanes and Methods for Manufacturing the Same
patent-application, June 2014


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


CMC Airfoil Joint
patent-application, December 2019


Vane Assemblies for Gas Turbine Engines
patent-application, August 2006


Gas Turbine Flowpath Structure
patent-application, August 2005


Ceramic matrix composite turbine engine vane
patent, November 2008


Ceramic matrix composite turbine vane
patent, November 2003


Turbine Blade with Heat Shield
patent-application, September 2017


CMC Vane Insulator and Method of Use
patent-application, September 2009


Bi-Cast Turbine Vane
patent-application, January 2015


Variable Area Gas Turbine Engine Component Having Movable Spar and Shell
patent-application, May 2006


Stator vane having reinforced braze joint
patent, July 1994


Turbine Nozzle
patent, June 1960


Turbine Nozzle
patent, January 1963


Support system for a composite airfoil in a turbine engine
patent, February 2008


CMC vane assembly apparatus and method
patent, October 2012


Sliding Ceramic Matrix composite Vane Assembly for Gas Turbine Engines
patent-application, June 2020