Nozzle assembly and method for forming nozzle assembly

Hafner, Matthew Troy

Advanced Search OptionsAdvanced Search queries use a traditional Term Search. For more info, see our FAQ.

All Fields:

Patent Title:

Abstract:

Assignee:

Inventor(s):

Patent Number:

Patent Classification (CPC):

All Classifications
A - human necessities
A01 - agriculture
A21 - baking
A22 - butchering
A23 - foods or foodstuffs
A24 - tobacco
A41 - wearing apparel
A42 - headwear
A43 - footwear
A44 - haberdashery
A45 - hand or travelling articles
A46 - brushware
A47 - furniture
A61 - medical or veterinary science
A62 - life-saving
A63 - sports
A99 - subject matter not otherwise provided for in this section
B - performing operations
B01 - physical or chemical processes or apparatus in general
B02 - crushing, pulverising, or disintegrating
B03 - separation of solid materials using liquids or using pneumatic tables or jigs
B04 - centrifugal apparatus or machines for carrying-out physical or chemical processes
B05 - spraying or atomising in general
B06 - generating or transmitting mechanical vibrations in general
B07 - separating solids from solids
B08 - cleaning
B09 - disposal of solid waste
B21 - mechanical metal-working without essentially removing material
B22 - casting
B23 - machine tools
B24 - grinding
B25 - hand tools
B26 - hand cutting tools
B27 - working or preserving wood or similar material
B28 - working cement, clay, or stone
B29 - working of plastics
B30 - presses
B31 - making articles of paper, cardboard or material worked in a manner analogous to paper
B32 - layered products
B33 - additive manufacturing technology
B41 - printing
B42 - bookbinding
B43 - writing or drawing implements
B44 - decorative arts
B60 - vehicles in general
B61 - railways
B62 - land vehicles for travelling otherwise than on rails
B63 - ships or other waterborne vessels
B64 - aircraft
B65 - conveying
B66 - hoisting
B67 - opening, closing {or cleaning} bottles, jars or similar containers
B68 - saddlery
B81 - microstructural technology
B82 - nanotechnology
B99 - subject matter not otherwise provided for in this section
C - chemistry
C01 - inorganic chemistry
C02 - treatment of water, waste water, sewage, or sludge
C03 - glass
C04 - cements
C05 - fertilisers
C06 - explosives
C07 - organic chemistry
C08 - organic macromolecular compounds
C09 - dyes
C10 - petroleum, gas or coke industries
C11 - animal or vegetable oils, fats, fatty substances or waxes
C12 - biochemistry
C13 - sugar industry
C14 - skins
C21 - metallurgy of iron
C22 - metallurgy
C23 - coating metallic material
C25 - electrolytic or electrophoretic processes
C30 - crystal growth
C40 - combinatorial technology
C99 - subject matter not otherwise provided for in this section
D - textiles
D01 - natural or man-made threads or fibres
D02 - yarns
D03 - weaving
D04 - braiding
D05 - sewing
D06 - treatment of textiles or the like
D07 - ropes
D10 - indexing scheme associated with sublasses of section d, relating to textiles
D21 - paper-making
D99 - subject matter not otherwise provided for in this section
E - fixed constructions
E01 - construction of roads, railways, or bridges
E02 - hydraulic engineering
E03 - water supply
E04 - building
E05 - locks
E06 - doors, windows, shutters, or roller blinds in general
E21 - earth drilling
E99 - subject matter not otherwise provided for in this section
F - mechanical engineering
F01 - machines or engines in general
F02 - combustion engines
F03 - machines or engines for liquids
F04 - positive - displacement machines for liquids
F05 - indexing schemes relating to engines or pumps in various subclasses of classes f01-f04
F15 - fluid-pressure actuators
F16 - engineering elements and units
F17 - storing or distributing gases or liquids
F21 - lighting
F22 - steam generation
F23 - combustion apparatus
F24 - heating
F25 - refrigeration or cooling
F26 - drying
F27 - furnaces
F28 - heat exchange in general
F41 - weapons
F42 - ammunition
F99 - subject matter not otherwise provided for in this section
G - physics
G01 - measuring
G02 - optics
G03 - photography
G04 - horology
G05 - controlling
G06 - computing
G07 - checking-devices
G08 - signalling
G09 - education
G10 - musical instruments
G11 - information storage
G12 - instrument details
G16 - information and communication technology [ict] specially adapted for specific application fields
G21 - nuclear physics
G99 - subject matter not otherwise provided for in this section
H - electricity
H01 - basic electric elements
H02 - generation
H03 - basic electronic circuitry
H04 - electric communication technique
H05 - electric techniques not otherwise provided for
H99 - subject matter not otherwise provided for in this section
Y - new / cross sectional technologies
Y02 - technologies or applications for mitigation or adaptation against climate change
Y04 - information or communication technologies having an impact on other technology areas
Y10 - technical subjects covered by former uspc

More Options ...

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:: Hafner, Matthew Troy

Issue Date:: 2020-12-01

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

Show more

F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
F01D25/005 - {Selecting particular materials}
F01D5/282 - {Selecting composite materials, e.g. blades with reinforcing filaments}
F01D5/284 - {Selection of ceramic materials}
F01D9/041 - {using blades
F01D9/042 - {fixing blades to stators
F01D9/044 - {permanently, e.g. by welding, brazing, casting or the like}

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
F05D2220/32 - in gas turbines
F05D2230/232 - by welding
F05D2240/128 - Nozzles
F05D2250/121 - square
F05D2250/141 - circular
F05D2250/60 - Structure
F05D2300/17 - Alloys
F05D2300/174 - Titanium alloys, e.g. TiAl
F05D2300/175 - Superalloys
F05D2300/6033 - Ceramic matrix composites [CMC]
F05D2300/604 - Amorphous

Show less

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.

Copy to clipboard


                    Hafner, Matthew Troy. Nozzle assembly and method for forming nozzle assembly.  United States.

Copy to clipboard


                    Hafner, Matthew Troy. Tue .  
        "Nozzle assembly and method for forming nozzle assembly".  United States.  https://www.osti.gov/servlets/purl/1771686.

Copy to clipboard


                    
@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         = {2020},

  month        = {12}

}

Copy to clipboard

Patent:

Save / Share:

Export Metadata

Save to My Library

Works referenced in this record:

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

Freeman, Ted J.; Walston, Jeffrey A.; Shi, Jun
US Patent Application 15/078446; 20170022829
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20170022829

Turbine Nozzle Assembly
patent-application, July 2011

Garci-Crespo, Andres Jose
US Patent Application 12/687407; 20110171018
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20110171018

Gas turbine vane platform element
patent, August 2012

Campbell, Christian X.; Schiavo, Anthony L.; Morrison, Jay A.
US Patent Document 8,251,652
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8251652

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

Zurmehly, George F.; Ortiz, Milton; Poon, Kin
US Patent Application 13/681675; 20140161623
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20140161623

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

Noe, Mark; Marusko, Mark; Jamision, Joshua
US Patent Application 12/347050; 20110027098
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20110027098

CMC Airfoil Joint
patent-application, December 2019

Walston, Jeffrey A.; Whittle, Michael; Vetters, Daniel K.
US Patent Application 15/995773; 20190368363
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20190368363

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

Freeman, Ted J.; Walston, Jeffrey A.; Shi, Jun
US Patent Application 15/015690; 20160230576
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20160230576

Gas Turbine Flowpath Structure
patent-application, August 2005

Haubert, Richard Clay
US Patent Application 10/769947; 20050169759
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20050169759

Ceramic matrix composite turbine engine vane
patent, November 2008

Shi, Jun; Ochs, Stuart S.; Green, Kevin E.
US Patent Document 7,452,189
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7452189

Ceramic matrix composite turbine vane
patent, November 2003

Widrig, Scott M.; Morrison, Jay A.; Albrecht, Harry A.
US Patent Document 6,648,597
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6648597

Turbine Blade with Heat Shield
patent-application, September 2017

Schetzel, Tara G.; Freeman, Ted J.; Thomas, David J.
US Patent Application 15/062670; 20170254207
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20170254207

Gas turbine engine vane and method of manufacture
patent, August 1998

Rhodes, Jeffrey F.
US Patent Document 5,797,725
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5797725

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

Greene, John; Cairo, Ronald Ralph; Dimascio, Paul Steven
US Patent Application 11/526501; 20090232644
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20090232644

Bi-Cast Turbine Vane
patent-application, January 2015

Freeman, Ted J.; Proctor, Robert F.; Landwehr, Sean E.
US Patent Application 14/144939; 20150016972
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150016972

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

McCaffrey, Michael G.; Propheter-Hinckley, Tracy A.; Surace, Raymond
US Patent Application 14/896738; 20160123165
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20160123165

Stator vane having reinforced braze joint
patent, July 1994

Correia, Victor Hugo Silva; McAllister, Kevin G.
US Patent Document 5,332,360
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5332360

Turbine Nozzle
patent, June 1960

Neate, Elroy P.
US Patent Document 2,942,844
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/2942844

Turbine Nozzle
patent, January 1963

Broffitt, Wilgus S.
US Patent Document 3,071,346
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3071346

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

Albrecht, Harry A.; Shteyman, Yevgeniy
US Patent Document 7,326,030
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7326030

CMC vane assembly apparatus and method
patent, October 2012

Schiavo, Anthony L.; Gonzalez, Malberto F.; Huang, Kuangwei
US Patent Document 8,292,580
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8292580

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

Whittle, Michael J.; Abbott, Michael G.; Warmuth, Austin R.
US Patent Application 16/227617; 20200200023
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20200200023

Similar Records in DOE Patents and OSTI.GOV collections:

Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same

Patent Stoia, Lucas John; Melton, Patrick Benedict; Johnson, Thomas Edward; ...

A turbomachine combustor nozzle includes a monolithic nozzle component having a plate element and a plurality of nozzle elements. Each of the plurality of nozzle elements includes a first end extending from the plate element to a second end. The plate element and plurality of nozzle elements are formed as a unitary component. A plate member is joined with the nozzle component. The plate member includes an outer edge that defines first and second surfaces and a plurality of openings extending between the first and second surfaces. The plurality of openings are configured and disposed to register with and receivemore » « less
Full Text Available
Fuel nozzle assembly for use in turbine engines and methods of assembling same

Patent Uhm, Jong Ho; Johnson, Thomas Edward

A fuel nozzle for use with a turbine engine is described herein. The fuel nozzle includes a housing that is coupled to a combustor liner defining a combustion chamber. The housing includes an endwall that at least partially defines the combustion chamber. A plurality of mixing tubes extends through the housing for channeling fuel to the combustion chamber. Each mixing tube of the plurality of mixing tubes includes an inner surface that extends between an inlet portion and an outlet portion. The outlet portion is oriented adjacent the housing endwall. At least one of the plurality of mixing tubes includesmore » « less
Full Text Available
Ceramic matrix composite turbine nozzle shell and method of assembly

Patent de Diego, Peter; Greene, John Ellington; Hobart, David Randall; ...

A method of manufacturing a ceramic matrix composite (CMC) turbine nozzle shell is provided. The method includes: assembling a primary outer nozzle platform, a primary inner nozzle platform, a core and trailing edge preform, and an airfoil-shaped body; joining the primary outer nozzle platform to a secondary outer nozzle platform of the airfoil-shaped body; and joining the primary inner nozzle platform to a secondary inner nozzle platform of the airfoil-shaped body. Composite plies circumferentially surround the airfoil-shaped body, and their longitudinal edges are cut into fingers that are folded down. The fingers are interleaved between secondary platform plies to formmore » « less
Full Text Available
Ceramic matrix composite turbine nozzle shell and method of assembly

Patent de Diego, Peter; Greene, III, John Ellington; Hafner, Matthew Troy; ...

A ceramic matrix composite turbine nozzle includes a primary outer nozzle platform; a primary inner nozzle platform; and an airfoil-shaped body extending between the primary inner and primary outer nozzle platforms. The body includes core plies defining a cavity; composite wrap plies circumscribing the core plies and defining an airfoil shape; a secondary outer nozzle platform in contact with the primary outer nozzle platform; and a secondary inner nozzle platform in contact with the primary inner nozzle platform. Each composite wrap ply has two layers of unidirectional fibers oriented transverse to each other and has first and second longitudinal edges.more » « less
Full Text Available
Exit chimney joint and method of forming the joint for closed circuit steam cooled gas turbine nozzles

Patent Burdgick, Steven Sebastian [Schenectady, NY]; Burns, James Lee [Schenectady, NY]

A nozzle segment for a gas turbine includes inner and outer band portions and a vane extending between the band portions. The inner and outer band portions are each divided into first and second plenums separated by an impingement plate. Cooling steam is supplied to the first cavity for flow through the apertures to cool the outer nozzle wall. The steam flows through a leading edge cavity in the vane into the first cavity of the inner band portion for flow through apertures of the impingement plate to cool the inner nozzle wall. Spent cooling steam flows through a pluralitymore » « less
Full Text Available

Similar Records

Title: Nozzle assembly and method for forming nozzle assembly

Abstract

Citation Formats

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

Gas turbine engine vane and method of manufacture patent, August 1998

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

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

Gas turbine engine vane and method of manufacture
patent, August 1998

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