Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions

Dyson, Thomas Earl; Rathay, Nicholas William; Fredmonski, Adam John

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):

More Options ...

Title: Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions

Abstract

A turbomachine blade, and a coupon for a turbomachine blade, are disclosed. The blade may include an airfoil body having a pressure side and a suction side connected by a leading edge and a trailing edge, a coolant feed passage defined in the airfoil body, and a coolant reuse passage defined in the airfoil body. The blade may also include a first cooling circuit defined in the airfoil body. The first cooling circuit may include a rearward passage extending toward the trailing edge from and fluidly coupled to the coolant feed passage, and a radially spreading return passage extending away from the trailing edge toward and fluidly coupled to the coolant reuse passage. The cooling circuit may also include a radially extending turn passage coupling the rearward passage and the radially spreading return passage. A first set of obstructions may be positioned in the radially extending turn passage.

Inventors:: Dyson, Thomas Earl; Rathay, Nicholas William; Fredmonski, Adam John

Issue Date:: 2023-11-14

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

Sponsoring Org.:: USDOE

OSTI Identifier:: 2293858

Patent Number(s):: 11814965

Application Number:: 17/454,363

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
F01D5/147 - {Construction, i.e. structural features, e.g. of weight-saving hollow blades
F01D5/18 - Hollow blades, {i.e. blades with cooling or heating channels or cavities
F01D5/187 - {Convection cooling}

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
F05D2240/304 - related to the trailing edge of a rotor blade
F05D2250/185 - serpentine-like
F05D2260/202 - by film cooling
F05D2260/2212 - by creating turbulence
F05D2260/232 - characterized by the cooling medium
F05D2260/608 - Aeration, ventilation, dehumidification or moisture removal of closed spaces

Show less

DOE Contract Number:: FE0031616

Resource Type:: Patent

Resource Relation:: Patent File Date: 11/10/2021

Country of Publication:: United States

Language:: English

Citation Formats


                    Dyson, Thomas Earl, Rathay, Nicholas William, and Fredmonski, Adam John. Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions.  United States: N. p., 2023. 
        Web.

Copy to clipboard


                    Dyson, Thomas Earl, Rathay, Nicholas William, & Fredmonski, Adam John. Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions.  United States.

Copy to clipboard


                    Dyson, Thomas Earl, Rathay, Nicholas William, and Fredmonski, Adam John. Tue .  
        "Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions".  United States.  https://www.osti.gov/servlets/purl/2293858.

Copy to clipboard


                    
@article{osti_2293858,

  title        = {Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions},

  author       = {Dyson, Thomas Earl and Rathay, Nicholas William and Fredmonski, Adam John},

  abstractNote = {A turbomachine blade, and a coupon for a turbomachine blade, are disclosed. The blade may include an airfoil body having a pressure side and a suction side connected by a leading edge and a trailing edge, a coolant feed passage defined in the airfoil body, and a coolant reuse passage defined in the airfoil body. The blade may also include a first cooling circuit defined in the airfoil body. The first cooling circuit may include a rearward passage extending toward the trailing edge from and fluidly coupled to the coolant feed passage, and a radially spreading return passage extending away from the trailing edge toward and fluidly coupled to the coolant reuse passage. The cooling circuit may also include a radially extending turn passage coupling the rearward passage and the radially spreading return passage. A first set of obstructions may be positioned in the radially extending turn passage.},

  doi          = {},

  journal      = {},
number       = ,

  volume       = ,

  place        = {United States},

  year         = {2023},

  month        = {11}

}

Copy to clipboard

Patent:

Save / Share:

Export Metadata

Save to My Library

Works referenced in this record:

Turbomachine blade with trailing edge cooling circuit
patent, October 2019

Weber, David Wayne
US Patent Document 10,450,950
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10450950

Gas Turbine Engine Airfoil Cooling Circuit
patent-application, May 2014

Spangler, Brandon W.; Zelesky, Mark F.; Otero, Edwin
US Patent Application 13/627072; 20140127013
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20140127013

Turbine airfoil trailing edge coolant passage created by cover
patent, March 2019

Snider, Zachary John; Foster, Gregory Thomas; Weber, Joseph Anthony
US Patent Document 10,233,761
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10233761

Cooling of turbine blades
patent, July 1990

Lilleker, Jonathan R.; Henshaw, Harry; Winter, John L.
US Patent Document 4,940,388
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4940388

Ribbed turbine blade tip
patent, December 1999

Lee, Ching-Pang
US Patent Document 5,997,251
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5997251

Turbine blade with multi-impingement cooling
patent, March 2013

Liang, George
US Patent Document 8,398,370
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8398370

Rotor blade for a gas turbine engine
patent, November 1981

Tubbs, Henry
US Patent Document 4,302,153
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4302153

Dual cut-back trailing edge for airfoils
patent, December 2010

Spangler, Brandon W.; Pietraszkiewicz, Edward F.
US Patent Document 7,845,906
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7845906

Method And System For Providing Cooling For Turbine Components
patent-application, April 2015

Morgan, Victor; Harris, John; Healy, Michael
US Patent Application 14/046437; 20150096305
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150096305

Varying geometries for cooling circuits of turbine blades
patent, October 2019

Weber, David Wayne; Dutta, Sandip; Leary, Brendon James
US Patent Document 10,450,875
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10450875

Turbine Airfoil with Near Wall Inflow Chambers
patent-application,

Liang, George
04/29/2010, vp
US Patent Application 11/497122; 20100104419
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100104419

Turbine vane with near wall multiple impingement cooling
patent, December 2013

Liang, George
US Patent Document 8,608,430
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8608430

Turbine Airfoil Cooling System with Axial Flowing Serpentine Cooling Chambers
patent-application, February 2008

Liang, George
US Patent Application 11/509228; 20080050241
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20080050241

Wavy flow cooling concept for turbine airfoils
patent, August 2010

Liang, George
US Patent Document 7,785,070
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7785070

Cooling circuits for a multi-wall blade
patent, July 2019

Weber, David Wayne; Foster, Gregory Thomas
US Patent Document 10,352,176
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10352176

Edge coupon including cooling circuit for airfoil
patent, March 2020

Hoskin, Robert Frank; Weber, David Wayne; Foster, Gregory Thomas
US Patent Document 10,598,028
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10598028

Closed circuit steam cooled bucket
patent, July 1996

Jacala, Ariel Caesar Prepena; Davis, Richard M.; Sullivan, Michael
US Patent Document 5,536,143
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5536143

Slant-tier turbine airfoil
patent, October 1999

Lee, Ching-Pang; Durgin, George A.; Harris, Robert
US Patent Document 5,967,752
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5967752

Turbine Stator Vane with Closed-Loop Sequential Impingement Cooling Insert
patent-application, August 2017

Downs, James P.
US Patent Application 15/253210; 20170234154
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20170234154

Turbine airfoil with trailing edge cooling
patent, July 2014

Liang, George
US Patent Document 8,790,083
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8790083

Airfoil with a Trailing Edge Supplement Structure
patent-application, February 2015

Kirtley, Kevin Richard; Schick, David Richard; Smith, Aaron Ezekiel
Us Patent Application 13/963276; 20150041590 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150041590

Turbine blade with tip vent
patent, August 1988

Braddy, Bruce T.; Eldrid, Sacheveral Q.
US Patent Document 4,761,116
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4761116

Axial serpentine cooled airfoil
patent, August 2000

Manning, Robert Francis; Acquaviva, Paul J.; Demers, Daniel Edward
US Patent Document 6,099,252
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6099252

Airfoil for a Turbine System
patent-application, February 2015

Wassynger, Stephen Paul; Harris, Jr., John Wesley; Healy, Michael James
US Patent Application 13/963322; 20150044059 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150044059

Spring-backed abradable seal for turbomachinery
patent, April 2003

Turnquist, Norman Arnold; Aksit, Mahmut Faruk; Ghasripoor, Farshad
US Patent Document 6,547,522
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6547522

Hot gas path component trailing edge having near wall cooling features
patent, May 2018

Lacy, Benjamin Paul; Kottilingam, Srikanth Chandrudu; Miranda, Carlos Miguel
US Patent Document 9,970,302
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/9970302

Cooling circuit for turbine stator vane trailing edge
patent, November 1995

Cunha, Francisco J.; De Angelis, David A.
US Patent Document 5,464,322
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5464322

Cooled component, casting core for manufacturing such a component, as well as method for manufacturing such a component
patent, April 2003

Haehnle, Hartmut; El-Nashar, Ibrahim; Kellerer, Rudolf
US Patent Document 6,547,525
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6547525

Axially Cooled Airfoil
patent-application, February 2013

Dutta, Sandip; Smith, Aaron Ezekiel
US Patent Application 13/216403; 20130082035
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20130052035

Turbine rotor blade with super cooling
patent, October 2014

Liang, George
US Patent Document 8,864,469
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8864469

Controlled Temperature Fluid Flow Directing Member
patent, May 1956

Roush, Milton S.
US Patent Document 2744723
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/2744723

Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities
patent, April 2019

Weber, David Wayne; Leary, Brendon James
US Patent Document 10,273,810
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10273810

Hollow Turbine or Compressor Vane
patent, November 1965

Smuland, Robert John; Davidson, Ralph Lester
US Patent Document 3220697
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3220697

Turbine airfoil with a near wall mini serpentine cooling circuit
patent, May 2010

Liang, George
US Patent Document 7,717,675
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7717675

Cooling circuit for a large highly twisted and tapered rotor blade
patent, March 2010

Liang, George
US Patent Document 7,682,133
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7682133

Turbine blade with impingement cooling
patent, July 2011

Liang, George
US Patent Document 7,985,049
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7985049

Serpentine Cooling Channel Construction for Open-circuit Liquid Cooled Turbine Buckets
patent, November 1974

Grondahl, Clayton M.
US Patent Document 3849025
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3849025

Closed-circuit steam-cooled bucket with integrally cooled shroud for gas turbines and methods of steam-cooling the buckets and shrouds
patent, September 1994

Jacala, Ariel Caesar Prepena; Chiu, R. Paul
US Patent Document 5,350,277
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5350277

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

Turbine airfoil trailing edge with micro cooling channels
patent, December 2002

Schafrik, Robert Edward; Darolia, Ramgopal; Lee, Ching-Pang
US Patent Document 6,499,949
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6499949

Turbine rotor blade with serpentine cooling
patent, January 2014

Liang, George
US Patent Document 8,628,298
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8628298

Turbine vane with dirt separator
patent, March 2012

Liang, George
US Patent Document 8,142,153
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8142153

Cooled turbine blade
patent, August 1987

Clifford, Rodney J.; Charters, Ian J.
US Patent Document 4,684,322
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4684322

Gas turbine engine airfoil cooling circuit
patent, September 2015

Propheter-Hinckley, Tracy A.; Perez, Rafael A.; Pietraszkiewicz, Edward F.
US Patent Document 9,145,780
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/9145780

Turbine blade assembly
patent, August 1993

Van Heusden, Gary S.; Brown, Thomas A.; Smith, Lloyd W.
US Patent Document 5,236,309
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5236309

Large twisted turbine rotor blade
patent, November 2012

Liang, George
US Patent Document 8,317,472
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8317472

Method and apparatus for cooling an airfoil
patent, June 2001

Auxier, Thomas A.; Downs, James P.; Kvasnak, William S.
US Patent Document 6,247,896
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6247896

Turbine blade with near wall cooling channels
patent, March 2014

Liang, George
US Patent Document 8,678,766
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8678766

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

Downs, James P.; Fedock, John A.
US Patent Document 8,322,988
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8322988

Three piece bonded thin wall cooled blade
patent, October 2013

Liang, George
US Patent Document 8,562,295
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8562295

Turbine airfoil with near-wall serpentine cooling
patent, November 2011

Liang, George
US Patent Document 8,047,788
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8047788

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

Turbine Blade and Engine Component
patent-application, May 2013

Fujimoto, Shu
US Patent Application 13/808641; 20130108471
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20130108471

Gas turbine blade
patent, May 2001

Koga, Akinori; Kawagishi, Hiroyuki; Okamura, Takanari
US Patent Document 6,227,804
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6227804

Gas Turbine Engine Component
patent-application, April 2014

Tibbott, Ian; Jackson, Dougal
US Patent Application 14/044460; 20140093379
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20140093379

Turbine blade with serpentine cooling circuit
patent, June 2011

Liang, George
US Patent Document 7,955,053
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7955053

Gas Turbine Engine Having Support Structure with Swept Leading Edge
patent-application, September 2015

Veiga, Brent
US Patent Application 14/430798; 20150252728
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150252728

Turbine Blade
patent-application, July 2009

Beeck, Alexander R.; Hoffman, Stefan
US Patent Application 12/226537; 20090185903
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20090185903

Components with Microchannel Cooling
patent-application, October 2013

Bunker, Ronald Scott
US Patent Application 13/448469; 20130272850
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20130272850

Turbine blade cooling system having multiple serpentine trailing edge cooling channels
patent, October 2008

Liang, George
US Patent Document 7,435,053
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7435053

Blade for a Gas Turbine Engine
patent-application, November 2008

Liang, George
US Patent Application 11/804426; 20080286115
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20080286115

Turbine blade with multiple near wall serpentine flow cooling
patent, May 2013

Liang, George
US Patent Document 8,444,386
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8444386

Engine component with hollow turbulators
patent, March 2020

Clark, Emily Rosette; Winka, James Richard; Getsinger, Daniel Robinson
US Patent Document 10,577,944
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10577944

Cooling circuit for and method of cooling a gas turbine bucket
patent, July 2002

Jacala, Ariel Caesar Prepena
US Patent Document 6,422,817
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/6422817

Gas turbine guide vane
patent, May 1977

Franklin, Clifford John
US Patent Document 4,021,139
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/4021139

Gas turbine moving blade
patent, June 1999

Tomita, Yasuoki; Ichiryu, Taku; Suenaga, Kiyoshi
US Patent Document 5,915,923
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5915923

Partially wrapped trailing edge cooling circuits with pressure side impingements
patent, May 2019

Weber, David Wayne; Leary, Brendon James
US Patent Document 10,301,946
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10301946

Recovery Tip Turbine Blade
patent-application, December 2010

Kuhne, Craig Miller; Bubnick, Joseph Steven; Vachhani, Alisha
US Patent Application 12/472611; 20100303625
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100303625

Cooling circuits for a multi-wall blade
patent, March 2019

Weber, David Wayne; Hanet, Robert Peter; Foster, Gregory Thomas
US Patent Document 10,240,465
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10240465

Turbine Vane for a Gas Turbine Engine Having Serpentine Cooing Channels within the Outer Wall
patent-application, September 2010

Liang, George
US Patent Application 12/396660; 20100226755
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20100226755

Pressurized Serpentine Cooling Channel Construction for Open-circuit Liquid Cooed Turbine Buckets
patent, October 1974

Grondahl, Clayton M.; Moore, John
US Patent Document 3844679
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/3844679

Method and System for Providing Cooling for Turbine Components
patent-application, March 2015

Morgan, Victo John; Lacy, Benjamin Paul
US Patent Application 14/016769; 20150059357 A1
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20150059357

Turbine blade with multi-vortex tip cooling and sealing
patent, October 2011

Liang, George
US Patent Document 8,043,059
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/8043059

Network Cooled Coated Wall
patent-application, March 2005

Lee, Ching-Pang; Darolia, Ramgopal
US Patent Application 03/17/2005; 10664192
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20050058534

Blade Cooling Passage for a Turbine
patent-application, January 2009

Pietraszkiewicz, Edward F.; Kohli, Atul
US Patent Application 11/781499; 20090028702
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20090028702

Turbine blade
patent, March 1992

Anzai, Shunichi; Kawaike, Kazuhiko; Ikeguchi, Takashi
US Patent Document 5,100,293
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/5100293

Multi-turn cooling circuits for turbine blades
patent, June 2019

Weber, David Wayne; Dutta, Sandip
US Patent Document 10,309,227
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10309227

Turbine airfoil coolant passage created in cover
patent, November 2019

Snider, Zachary John; Foster, Gregory Thomas; Kottilingam, Srikanth Chandrudu
US Patent Document 10,465,521
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10465521

Method for Manufacturing an Oxide/Oxide Composite Material Turbomachine lade Provided with Internal Channels
patent-application, June 2014

Podgorski, Michael; Jacques, Bruno; Dambrine, Gerard
US Patent Application 14/099094; 20140161626
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/20140161626

Turbine vane with coupon having corrugated surface(s)
patent, October 2019

Jones, Jeffrey Clarence; Fredmonski, Adam John
US Patent Document 10,443,399
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/10443399

Turbine blade with a serpentine flow and impingement cooling circuit
patent, May 2009

Liang, George
US Patent Document 7,530,789
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/7530789

Turbine rotor blade with tip cooling
patent, September 2016

Liang, George
US Patent Document 9,447,692
URL: https://image-ppubs.uspto.gov/dirsearch-public/print/downloadPdf/9447692

Similar Records in DOE Patents and OSTI.GOV collections:

Partially turbulated trailing edge cooling passages for gas turbine nozzles

Patent Thatcher, Jonathan Carl [Schenectady, NY]; Burdgick, Steven Sebastian [Schenectady, NY]

A plurality of passages are spaced one from the other along the length of a trailing edge of a nozzle vane in a gas turbine. The passages lie in communication with a cavity in the vane for flowing cooling air from the cavity through the passages through the tip of the trailing edge into the hot gas path. Each passage is partially turbulated and includes ribs in an aft portion thereof to provide enhanced cooling effects adjacent the tip of the trailing edge. The major portions of the passages are smooth bore. By this arrangement, reduced temperature gradients across themore » « less
Full Text Available
Hot gas path component trailing edge having near wall cooling features

Patent Lacy, Benjamin Paul; Kottilingam, Srikanth Chandrudu; Miranda, Carlos Miguel; ...

A hot gas path component includes a substrate having an outer surface and an inner surface. The inner surface defines an interior space. The outer surface defines a pressure side surface and a suction side surface. The pressure and suction side surfaces are joined together at a leading edge and at a trailing edge. A first cooling passage is formed in the suction side surface of the substrate. It is coupled in flow communication to the interior space. A second cooling passage, separate from the first cooling passage, is formed in the pressure side surface. The second cooling passage ismore » « less
Full Text Available
Internal cooling system with converging-diverging exit slots in trailing edge cooling channel for an airfoil in a turbine engine

Patent Lee, Ching-Pang; Myers, Caleb; Johnson, Erik; ...

An airfoil (10) is disclosed for a gas turbine engine in which the airfoil (10) includes an internal cooling system (14) with one or more converging-diverging exit slots (20) configured to increase the effectiveness of the cooling system (14) at the trailing edge (34) of the airfoil (10) by increasing the contact of cooling fluids with internal surfaces (24, 30) of the pressure and suction sides (36, 38) of the airfoil (10). In at least one embodiment, the trailing edge cooling channel (18) may include one or more converging-diverging exit slots (20) to further pressurize the trailing edge cooling channelmore » « less
Full Text Available
Trailing edge cooling using angled impingement on surface enhanced with cast chevron arrangements

Patent Lee, Ching-Pang; Heneveld, Benjamin E.; Brown, Glenn E.; ...

A gas turbine engine component, including: a pressure side (12) having an interior surface (34); a suction side (14) having an interior surface (36); a trailing edge portion (30); and a plurality of suction side and pressure side impingement orifices (24) disposed in the trailing edge portion (30). Each suction side impingement orifice is configured to direct an impingement jet (48) at an acute angle (52) onto a target area (60) that encompasses a tip (140) of a chevron (122) within a chevron arrangement (120) formed in the suction side interior surface. Each pressure side impingement orifice is configured tomore » « less
Full Text Available
Turbine airfoil with leading edge cooling passage(s) coupled via plenum to film cooling holes, and related method

Patent Lacy, Benjamin Paul; Sezer, Ibrahim; VanTassel, Brad Wilson

A turbine airfoil includes a body including a wall defining pressure and suction sides, and a leading edge extending between the pressure and suction sides. A cooling circuit inside the wall of the body includes at least one of: a) a suction side to pressure side cooling sub-circuit including a first cooling passage(s) extending from the suction side to the pressure side around the leading edge to a first plenum, and a plurality of first film cooling holes communicating with the first plenum and extending through the wall on the pressure side; and b) a pressure side to suction sidemore » « less
Full Text Available

Similar Records

Title: Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions

Abstract

Citation Formats

Turbomachine blade with trailing edge cooling circuit patent, October 2019

Gas Turbine Engine Airfoil Cooling Circuit patent-application, May 2014

Turbine airfoil trailing edge coolant passage created by cover patent, March 2019

Cooling of turbine blades patent, July 1990

Ribbed turbine blade tip patent, December 1999

Turbine blade with multi-impingement cooling patent, March 2013

Rotor blade for a gas turbine engine patent, November 1981

Dual cut-back trailing edge for airfoils patent, December 2010

Method And System For Providing Cooling For Turbine Components patent-application, April 2015

Varying geometries for cooling circuits of turbine blades patent, October 2019

Turbine Airfoil with Near Wall Inflow Chambers patent-application,

Turbine vane with near wall multiple impingement cooling patent, December 2013

Turbine Airfoil Cooling System with Axial Flowing Serpentine Cooling Chambers patent-application, February 2008

Wavy flow cooling concept for turbine airfoils patent, August 2010

Cooling circuits for a multi-wall blade patent, July 2019

Edge coupon including cooling circuit for airfoil patent, March 2020

Closed circuit steam cooled bucket patent, July 1996

Slant-tier turbine airfoil patent, October 1999

Turbine Stator Vane with Closed-Loop Sequential Impingement Cooling Insert patent-application, August 2017

Turbine airfoil with trailing edge cooling patent, July 2014

Airfoil with a Trailing Edge Supplement Structure patent-application, February 2015

Turbine blade with tip vent patent, August 1988

Axial serpentine cooled airfoil patent, August 2000

Airfoil for a Turbine System patent-application, February 2015

Spring-backed abradable seal for turbomachinery patent, April 2003

Hot gas path component trailing edge having near wall cooling features patent, May 2018

Cooling circuit for turbine stator vane trailing edge patent, November 1995

Cooled component, casting core for manufacturing such a component, as well as method for manufacturing such a component patent, April 2003

Axially Cooled Airfoil patent-application, February 2013

Turbine rotor blade with super cooling patent, October 2014

Controlled Temperature Fluid Flow Directing Member patent, May 1956

Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities patent, April 2019

Hollow Turbine or Compressor Vane patent, November 1965

Turbine airfoil with a near wall mini serpentine cooling circuit patent, May 2010

Cooling circuit for a large highly twisted and tapered rotor blade patent, March 2010

Turbine blade with impingement cooling patent, July 2011

Serpentine Cooling Channel Construction for Open-circuit Liquid Cooled Turbine Buckets patent, November 1974

Closed-circuit steam-cooled bucket with integrally cooled shroud for gas turbines and methods of steam-cooling the buckets and shrouds patent, September 1994

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

Turbine airfoil trailing edge with micro cooling channels patent, December 2002

Turbine rotor blade with serpentine cooling patent, January 2014

Turbine vane with dirt separator patent, March 2012

Cooled turbine blade patent, August 1987

Gas turbine engine airfoil cooling circuit patent, September 2015

Turbine blade assembly patent, August 1993

Large twisted turbine rotor blade patent, November 2012

Method and apparatus for cooling an airfoil patent, June 2001

Turbine blade with near wall cooling channels patent, March 2014

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

Three piece bonded thin wall cooled blade patent, October 2013

Turbine airfoil with near-wall serpentine cooling patent, November 2011

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

Turbine Blade and Engine Component patent-application, May 2013

Gas turbine blade patent, May 2001

Gas Turbine Engine Component patent-application, April 2014

Turbine blade with serpentine cooling circuit patent, June 2011

Gas Turbine Engine Having Support Structure with Swept Leading Edge patent-application, September 2015

Turbine Blade patent-application, July 2009

Components with Microchannel Cooling patent-application, October 2013

Turbine blade cooling system having multiple serpentine trailing edge cooling channels patent, October 2008

Blade for a Gas Turbine Engine patent-application, November 2008

Turbine blade with multiple near wall serpentine flow cooling patent, May 2013

Engine component with hollow turbulators patent, March 2020

Cooling circuit for and method of cooling a gas turbine bucket patent, July 2002

Gas turbine guide vane patent, May 1977

Gas turbine moving blade patent, June 1999

Partially wrapped trailing edge cooling circuits with pressure side impingements patent, May 2019

Recovery Tip Turbine Blade patent-application, December 2010

Cooling circuits for a multi-wall blade patent, March 2019

Turbine Vane for a Gas Turbine Engine Having Serpentine Cooing Channels within the Outer Wall patent-application, September 2010

Pressurized Serpentine Cooling Channel Construction for Open-circuit Liquid Cooed Turbine Buckets patent, October 1974

Method and System for Providing Cooling for Turbine Components patent-application, March 2015

Turbine blade with multi-vortex tip cooling and sealing patent, October 2011

Network Cooled Coated Wall patent-application, March 2005

Blade Cooling Passage for a Turbine patent-application, January 2009

Turbine blade patent, March 1992

Multi-turn cooling circuits for turbine blades patent, June 2019

Turbomachine blade with trailing edge cooling circuit
patent, October 2019

Gas Turbine Engine Airfoil Cooling Circuit
patent-application, May 2014

Turbine airfoil trailing edge coolant passage created by cover
patent, March 2019

Cooling of turbine blades
patent, July 1990

Ribbed turbine blade tip
patent, December 1999

Turbine blade with multi-impingement cooling
patent, March 2013

Rotor blade for a gas turbine engine
patent, November 1981

Dual cut-back trailing edge for airfoils
patent, December 2010

Method And System For Providing Cooling For Turbine Components
patent-application, April 2015

Varying geometries for cooling circuits of turbine blades
patent, October 2019

Turbine Airfoil with Near Wall Inflow Chambers
patent-application,

Turbine vane with near wall multiple impingement cooling
patent, December 2013

Turbine Airfoil Cooling System with Axial Flowing Serpentine Cooling Chambers
patent-application, February 2008

Wavy flow cooling concept for turbine airfoils
patent, August 2010

Cooling circuits for a multi-wall blade
patent, July 2019

Edge coupon including cooling circuit for airfoil
patent, March 2020

Closed circuit steam cooled bucket
patent, July 1996

Slant-tier turbine airfoil
patent, October 1999

Turbine Stator Vane with Closed-Loop Sequential Impingement Cooling Insert
patent-application, August 2017

Turbine airfoil with trailing edge cooling
patent, July 2014

Airfoil with a Trailing Edge Supplement Structure
patent-application, February 2015

Turbine blade with tip vent
patent, August 1988

Axial serpentine cooled airfoil
patent, August 2000

Airfoil for a Turbine System
patent-application, February 2015

Spring-backed abradable seal for turbomachinery
patent, April 2003

Hot gas path component trailing edge having near wall cooling features
patent, May 2018

Cooling circuit for turbine stator vane trailing edge
patent, November 1995

Cooled component, casting core for manufacturing such a component, as well as method for manufacturing such a component
patent, April 2003

Axially Cooled Airfoil
patent-application, February 2013

Turbine rotor blade with super cooling
patent, October 2014

Controlled Temperature Fluid Flow Directing Member
patent, May 1956

Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities
patent, April 2019

Hollow Turbine or Compressor Vane
patent, November 1965

Turbine airfoil with a near wall mini serpentine cooling circuit
patent, May 2010

Cooling circuit for a large highly twisted and tapered rotor blade
patent, March 2010

Turbine blade with impingement cooling
patent, July 2011

Serpentine Cooling Channel Construction for Open-circuit Liquid Cooled Turbine Buckets
patent, November 1974

Closed-circuit steam-cooled bucket with integrally cooled shroud for gas turbines and methods of steam-cooling the buckets and shrouds
patent, September 1994

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

Turbine airfoil trailing edge with micro cooling channels
patent, December 2002

Turbine rotor blade with serpentine cooling
patent, January 2014

Turbine vane with dirt separator
patent, March 2012

Cooled turbine blade
patent, August 1987

Gas turbine engine airfoil cooling circuit
patent, September 2015

Turbine blade assembly
patent, August 1993

Large twisted turbine rotor blade
patent, November 2012

Method and apparatus for cooling an airfoil
patent, June 2001

Turbine blade with near wall cooling channels
patent, March 2014

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

Three piece bonded thin wall cooled blade
patent, October 2013

Turbine airfoil with near-wall serpentine cooling
patent, November 2011

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

Turbine Blade and Engine Component
patent-application, May 2013

Gas turbine blade
patent, May 2001

Gas Turbine Engine Component
patent-application, April 2014

Turbine blade with serpentine cooling circuit
patent, June 2011

Gas Turbine Engine Having Support Structure with Swept Leading Edge
patent-application, September 2015

Turbine Blade
patent-application, July 2009

Components with Microchannel Cooling
patent-application, October 2013

Turbine blade cooling system having multiple serpentine trailing edge cooling channels
patent, October 2008

Blade for a Gas Turbine Engine
patent-application, November 2008

Turbine blade with multiple near wall serpentine flow cooling
patent, May 2013

Engine component with hollow turbulators
patent, March 2020

Cooling circuit for and method of cooling a gas turbine bucket
patent, July 2002

Gas turbine guide vane
patent, May 1977

Gas turbine moving blade
patent, June 1999

Partially wrapped trailing edge cooling circuits with pressure side impingements
patent, May 2019

Recovery Tip Turbine Blade
patent-application, December 2010

Cooling circuits for a multi-wall blade
patent, March 2019

Turbine Vane for a Gas Turbine Engine Having Serpentine Cooing Channels within the Outer Wall
patent-application, September 2010

Pressurized Serpentine Cooling Channel Construction for Open-circuit Liquid Cooed Turbine Buckets
patent, October 1974

Method and System for Providing Cooling for Turbine Components
patent-application, March 2015

Turbine blade with multi-vortex tip cooling and sealing
patent, October 2011

Network Cooled Coated Wall
patent-application, March 2005

Blade Cooling Passage for a Turbine
patent-application, January 2009

Turbine blade
patent, March 1992

Multi-turn cooling circuits for turbine blades
patent, June 2019

Turbine airfoil coolant passage created in cover
patent, November 2019

Method for Manufacturing an Oxide/Oxide Composite Material Turbomachine lade Provided with Internal Channels
patent-application, June 2014

Turbine vane with coupon having corrugated surface(s)
patent, October 2019