Turbine component and methods of making and cooling a turbine component

Dutta, Sandip; Zhang, James; Itzel, Gary Michael; Delvaux, John McConnell; Hafner, Matthew Troy

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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
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C - chemistry
C01 - inorganic chemistry
C02 - treatment of water, waste water, sewage, or sludge
C03 - glass
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C10 - petroleum, gas or coke industries
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C12 - biochemistry
C13 - sugar industry
C14 - skins
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C22 - metallurgy
C23 - coating metallic material
C25 - electrolytic or electrophoretic processes
C30 - crystal growth
C40 - combinatorial technology
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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
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E01 - construction of roads, railways, or bridges
E02 - hydraulic engineering
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E06 - doors, windows, shutters, or roller blinds in general
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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
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F17 - storing or distributing gases or liquids
F21 - lighting
F22 - steam generation
F23 - combustion apparatus
F24 - heating
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F26 - drying
F27 - furnaces
F28 - heat exchange in general
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F42 - ammunition
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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
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H01 - basic electric elements
H02 - generation
H03 - basic electronic circuitry
H04 - electric communication technique
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Y02 - technologies or applications for mitigation or adaptation against climate change
Y04 - information or communication technologies having an impact on other technology areas
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Title: Turbine component and methods of making and cooling a turbine component

Abstract

A turbine component includes a root and an airfoil extending from the root to a tip opposite the root. The airfoil forms a leading edge and a trailing edge portion extending to a trailing edge. Radial cooling channels in the trailing edge portion of the airfoil permit radial flow of a cooling fluid through the trailing edge portion. Each radial cooling channel has a first end at a lower surface at a root edge of the trailing edge portion or at an upper surface at a tip edge of the trailing edge portion and a second end opposite the first end at the lower surface or the upper surface. A method of making a turbine component and a method of cooling a turbine component are also disclosed.

Inventors:: Dutta, Sandip; Zhang, James; Itzel, Gary Michael; Delvaux, John McConnell; Hafner, Matthew Troy

Issue Date:: Tue Nov 12 00:00:00 EST 2019

Research Org.:: General Electric Co., Schenectady, NY (United States)

Sponsoring Org.:: USDOE

OSTI Identifier:: 1600268

Patent Number(s):: 10472973

Application Number:: 15/174,271

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

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F - MECHANICAL ENGINEERING F01 - MACHINES OR ENGINES IN GENERAL F01D - NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
F01D25/12 - Cooling
F01D5/147 - {Construction, i.e. structural features, e.g. of weight-saving hollow blades
F01D5/187 - {Convection cooling}
F01D5/282 - {Selecting composite materials, e.g. blades with reinforcing filaments}
F01D9/02 - Nozzles

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
F05D2220/30 - in turbines
F05D2230/22 - by sintering
F05D2230/237 - Brazing
F05D2230/31 - Layer deposition
F05D2240/122 - related to the trailing edge of a stator vane
F05D2240/304 - related to the trailing edge of a rotor blade
F05D2250/183 - zigzag
F05D2250/184 - sinusoidal
F05D2250/185 - serpentine-like
F05D2260/20 - Heat transfer, e.g. cooling
F05D2260/204 - by the use of microcircuits
F05D2300/175 - Superalloys
F05D2300/6033 - Ceramic matrix composites [CMC]

Show less

DOE Contract Number:: FE0024006

Resource Type:: Patent

Resource Relation:: Patent File Date: 06/06/2016

Country of Publication:: United States

Language:: English

Subject:: 36 MATERIALS SCIENCE; 33 ADVANCED PROPULSION SYSTEMS

Citation Formats


                    Dutta, Sandip, Zhang, James, Itzel, Gary Michael, Delvaux, John McConnell, and Hafner, Matthew Troy. Turbine component and methods of making and cooling a turbine component.  United States: N. p., 2019. 
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                    Dutta, Sandip, Zhang, James, Itzel, Gary Michael, Delvaux, John McConnell, & Hafner, Matthew Troy. Turbine component and methods of making and cooling a turbine component.  United States.

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                    Dutta, Sandip, Zhang, James, Itzel, Gary Michael, Delvaux, John McConnell, and Hafner, Matthew Troy. Tue .  
        "Turbine component and methods of making and cooling a turbine component".  United States.  https://www.osti.gov/servlets/purl/1600268.

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@article{osti_1600268,

  title        = {Turbine component and methods of making and cooling a turbine component},

  author       = {Dutta, Sandip and Zhang, James and Itzel, Gary Michael and Delvaux, John McConnell and Hafner, Matthew Troy},

  abstractNote = {A turbine component includes a root and an airfoil extending from the root to a tip opposite the root. The airfoil forms a leading edge and a trailing edge portion extending to a trailing edge. Radial cooling channels in the trailing edge portion of the airfoil permit radial flow of a cooling fluid through the trailing edge portion. Each radial cooling channel has a first end at a lower surface at a root edge of the trailing edge portion or at an upper surface at a tip edge of the trailing edge portion and a second end opposite the first end at the lower surface or the upper surface. A method of making a turbine component and a method of cooling a turbine component are also disclosed.},

  doi          = {},

  journal      = {},
number       = ,

  volume       = ,

  place        = {United States},

  year         = {Tue Nov 12 00:00:00 EST 2019},

  month        = {Tue Nov 12 00:00:00 EST 2019}

}

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Works referenced in this record:

Two piece hollow turbine blade with serpentine cooling circuits
patent, January 2011

Liang, George
US Patent Document 7,862,299
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7862299

Internally cooled airfoil
patent, September 1993

Winstanley, David K.; Phillips, John
US Patent Document 5,246,340
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5246340

Ceramic composite vane with metallic substructure
patent, February 2003

Morrison, Jay A.; Merrill, Gary B.; Lane, Jay E.
US Patent Document 6,514,046
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6514046

Turbine bucket profile yielding improved throat
patent, May 2016

Gustafson, Ross James; Jayana, Srinivasa Govardhan; Kareff, Spencer Aaron
US Patent Document 9,347,320
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/9347320

Method for repairing a turbomachinery blade tip
patent, July 1980

Zelahy, John W.
US Patent Document 4,214,355
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4214355

Turbine blades made from multiple single crystal cast superalloy segments
patent, December 2001

Burke, Michael A.; Freyer, Paula; Hebbar, Mohan A.
US Patent Document 6,331,217
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6331217

Component of Coupon for Being Used Under High Thermal and Stress Load and Method for Manufacturing Such Component of Coupon
patent-application, May 2013

Szwedowicz, Jaroslaw Leszek; Rickenbacher, Lukas Emanuel
US Patent Application 13/664662; 20130108460 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20130108460

Turbine airfoil with serpentine trailing edge cooling circuit
patent, March 2010

Liang, George
US Patent Document 7,670,113
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7670113

Component or Coupon for Being Used Under High Thermal and Stress Load and Method for Manufacturing Such Component of Coupon
patent-application, March 2016

Szwedowicz, Jaroslaw Leszek; Richenbacher, Lukas Emanuel
US Patent Application 14/959004; 20160082547 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20160082547

Ceramic Matrix Composite Structure Having Integral Cooling Passages And Method Of Manufacture
patent-application, March 2003

Morrison, Jay; Butner, Steven C.; Campbell, Christian X.
US Patent Application 09/962733; 20030059577 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20030059577

Turbine Bucket Profile Yielding Improved Throat
patent-application, April 2015

Gustafson, Ross James; Jayana, Srinivasa Govardhan; Kareff, Spence Aaron
US Patent Application 14/061146; 20150107266 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150107266

Turbine Blade Cooling System Having Multiple Serpentine Trailing Edge Cooling Channels
patent-application, October 2006

Liang, George
US Patent Application 11/092776; 20060222493 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20060222493

Process For Forming A Shell Of A Turbine Airfoil
patent-application, August 2009

Wilson, Jr., Jack W.; Brown, Wesley D.
US Patent Application 12/355353; 20090193657 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20090193657

Cooled Vane Structure for High Temperature Turbines
patent, October 1970

Kercher, David M.
US Patent Document 3533712 A
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3533712

Bucket Tip/Collection Slot Combination for Open-Circuit Liquid-Cooled Gas Turbines
patent, May 1973

Kydd, Paul H.
US Patent Document 3736071 A
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3736071

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Similar Records

Title: Turbine component and methods of making and cooling a turbine component

Abstract

Citation Formats

Two piece hollow turbine blade with serpentine cooling circuits patent, January 2011

Internally cooled airfoil patent, September 1993

Ceramic composite vane with metallic substructure patent, February 2003

Turbine bucket profile yielding improved throat patent, May 2016

Method for repairing a turbomachinery blade tip patent, July 1980

Turbine blades made from multiple single crystal cast superalloy segments patent, December 2001

Component of Coupon for Being Used Under High Thermal and Stress Load and Method for Manufacturing Such Component of Coupon patent-application, May 2013

Turbine airfoil with serpentine trailing edge cooling circuit patent, March 2010

Component or Coupon for Being Used Under High Thermal and Stress Load and Method for Manufacturing Such Component of Coupon patent-application, March 2016

Ceramic Matrix Composite Structure Having Integral Cooling Passages And Method Of Manufacture patent-application, March 2003

Turbine Bucket Profile Yielding Improved Throat patent-application, April 2015

Turbine Blade Cooling System Having Multiple Serpentine Trailing Edge Cooling Channels patent-application, October 2006

Process For Forming A Shell Of A Turbine Airfoil patent-application, August 2009

Cooled Vane Structure for High Temperature Turbines patent, October 1970

Bucket Tip/Collection Slot Combination for Open-Circuit Liquid-Cooled Gas Turbines patent, May 1973

Two piece hollow turbine blade with serpentine cooling circuits
patent, January 2011

Internally cooled airfoil
patent, September 1993

Ceramic composite vane with metallic substructure
patent, February 2003

Turbine bucket profile yielding improved throat
patent, May 2016

Method for repairing a turbomachinery blade tip
patent, July 1980

Turbine blades made from multiple single crystal cast superalloy segments
patent, December 2001

Component of Coupon for Being Used Under High Thermal and Stress Load and Method for Manufacturing Such Component of Coupon
patent-application, May 2013

Turbine airfoil with serpentine trailing edge cooling circuit
patent, March 2010

Component or Coupon for Being Used Under High Thermal and Stress Load and Method for Manufacturing Such Component of Coupon
patent-application, March 2016

Ceramic Matrix Composite Structure Having Integral Cooling Passages And Method Of Manufacture
patent-application, March 2003

Turbine Bucket Profile Yielding Improved Throat
patent-application, April 2015

Turbine Blade Cooling System Having Multiple Serpentine Trailing Edge Cooling Channels
patent-application, October 2006

Process For Forming A Shell Of A Turbine Airfoil
patent-application, August 2009

Cooled Vane Structure for High Temperature Turbines
patent, October 1970

Bucket Tip/Collection Slot Combination for Open-Circuit Liquid-Cooled Gas Turbines
patent, May 1973