DE60039202D1 - Methode zur Kühlung einer Wand in einer Gasturbine - Google Patents

Methode zur Kühlung einer Wand in einer Gasturbine

Info

Publication number
DE60039202D1
DE60039202D1 DE60039202T DE60039202T DE60039202D1 DE 60039202 D1 DE60039202 D1 DE 60039202D1 DE 60039202 T DE60039202 T DE 60039202T DE 60039202 T DE60039202 T DE 60039202T DE 60039202 D1 DE60039202 D1 DE 60039202D1
Authority
DE
Germany
Prior art keywords
cooling
wall
gas turbine
turbine
gas
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60039202T
Other languages
English (en)
Inventor
Ronald S Lafleur
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of DE60039202D1 publication Critical patent/DE60039202D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186Film cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • F01D25/12Cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/18Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187Convection cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/202Heat transfer, e.g. cooling by film cooling
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2212Improvement of heat transfer by creating turbulence
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2214Improvement of heat transfer by increasing the heat transfer surface
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/20Heat transfer, e.g. cooling
    • F05D2260/221Improvement of heat transfer
    • F05D2260/2214Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141Improvement of heat transfer by increasing the heat transfer surface using fins or ribs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE60039202T 1999-10-05 2000-10-05 Methode zur Kühlung einer Wand in einer Gasturbine Expired - Lifetime DE60039202D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/412,274 US6254334B1 (en) 1999-10-05 1999-10-05 Method and apparatus for cooling a wall within a gas turbine engine

Publications (1)

Publication Number Publication Date
DE60039202D1 true DE60039202D1 (de) 2008-07-24

Family

ID=23632342

Family Applications (3)

Application Number Title Priority Date Filing Date
DE60039202T Expired - Lifetime DE60039202D1 (de) 1999-10-05 2000-10-05 Methode zur Kühlung einer Wand in einer Gasturbine
DE60040324T Expired - Lifetime DE60040324D1 (de) 1999-10-05 2000-10-05 Wand-Kühlkreislauf
DE60041091T Expired - Lifetime DE60041091D1 (de) 1999-10-05 2000-10-05 Wand-Kühlkreislauf

Family Applications After (2)

Application Number Title Priority Date Filing Date
DE60040324T Expired - Lifetime DE60040324D1 (de) 1999-10-05 2000-10-05 Wand-Kühlkreislauf
DE60041091T Expired - Lifetime DE60041091D1 (de) 1999-10-05 2000-10-05 Wand-Kühlkreislauf

Country Status (4)

Country Link
US (1) US6254334B1 (de)
EP (3) EP1091091B1 (de)
JP (1) JP2001107704A (de)
DE (3) DE60039202D1 (de)

Families Citing this family (121)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19737845C2 (de) * 1997-08-29 1999-12-02 Siemens Ag Verfahren zum Herstellen einer Gasturbinenschaufel, sowie nach dem Verfahren hergestellte Gasturbinenschaufel
US6402470B1 (en) * 1999-10-05 2002-06-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
DE10001109B4 (de) * 2000-01-13 2012-01-19 Alstom Technology Ltd. Gekühlte Schaufel für eine Gasturbine
GB0114503D0 (en) * 2001-06-14 2001-08-08 Rolls Royce Plc Air cooled aerofoil
US6581369B1 (en) 2001-08-27 2003-06-24 General Electric Company Heat recovery in test cells for gas turbine engines
US6974308B2 (en) * 2001-11-14 2005-12-13 Honeywell International, Inc. High effectiveness cooled turbine vane or blade
US6681577B2 (en) 2002-01-16 2004-01-27 General Electric Company Method and apparatus for relieving stress in a combustion case in a gas turbine engine
US6705831B2 (en) * 2002-06-19 2004-03-16 United Technologies Corporation Linked, manufacturable, non-plugging microcircuits
US7137776B2 (en) * 2002-06-19 2006-11-21 United Technologies Corporation Film cooling for microcircuits
US7593030B2 (en) * 2002-07-25 2009-09-22 Intouch Technologies, Inc. Tele-robotic videoconferencing in a corporate environment
US6981846B2 (en) 2003-03-12 2006-01-03 Florida Turbine Technologies, Inc. Vortex cooling of turbine blades
US7014424B2 (en) * 2003-04-08 2006-03-21 United Technologies Corporation Turbine element
US6808367B1 (en) 2003-06-09 2004-10-26 Siemens Westinghouse Power Corporation Cooling system for a turbine blade having a double outer wall
US6832889B1 (en) 2003-07-09 2004-12-21 General Electric Company Integrated bridge turbine blade
US6896487B2 (en) * 2003-08-08 2005-05-24 United Technologies Corporation Microcircuit airfoil mainbody
US6981840B2 (en) * 2003-10-24 2006-01-03 General Electric Company Converging pin cooled airfoil
US6984103B2 (en) * 2003-11-20 2006-01-10 General Electric Company Triple circuit turbine blade
US7011502B2 (en) * 2004-04-15 2006-03-14 General Electric Company Thermal shield turbine airfoil
US7118326B2 (en) * 2004-06-17 2006-10-10 Siemens Power Generation, Inc. Cooled gas turbine vane
US7478994B2 (en) * 2004-11-23 2009-01-20 United Technologies Corporation Airfoil with supplemental cooling channel adjacent leading edge
GB2428749B (en) 2005-08-02 2007-11-28 Rolls Royce Plc A component comprising a multiplicity of cooling passages
US20070227706A1 (en) * 2005-09-19 2007-10-04 United Technologies Corporation Compact heat exchanger
DE102005050118B4 (de) * 2005-10-18 2009-04-09 Werkzeugbau Siegfried Hofmann Gmbh Anordnung zur Temperierung eines metallischen Körpers sowie Verwendung derselben
US7311498B2 (en) * 2005-11-23 2007-12-25 United Technologies Corporation Microcircuit cooling for blades
US7364405B2 (en) 2005-11-23 2008-04-29 United Technologies Corporation Microcircuit cooling for vanes
US7600966B2 (en) * 2006-01-17 2009-10-13 United Technologies Corporation Turbine airfoil with improved cooling
EP1813869A3 (de) * 2006-01-25 2013-08-14 Rolls-Royce plc Wandelemente für Gasturbinenbrennkammer
US7607890B2 (en) 2006-06-07 2009-10-27 United Technologies Corporation Robust microcircuits for turbine airfoils
EP1881157B1 (de) * 2006-07-18 2014-02-12 United Technologies Corporation Serpentinenartige Mikrokanäle zur lokalen Wärmeabfuhr
US7581928B1 (en) 2006-07-28 2009-09-01 United Technologies Corporation Serpentine microcircuits for hot gas migration
US7581927B2 (en) * 2006-07-28 2009-09-01 United Technologies Corporation Serpentine microcircuit cooling with pressure side features
US7686582B2 (en) 2006-07-28 2010-03-30 United Technologies Corporation Radial split serpentine microcircuits
US7780413B2 (en) * 2006-08-01 2010-08-24 Siemens Energy, Inc. Turbine airfoil with near wall inflow chambers
US9133715B2 (en) * 2006-09-20 2015-09-15 United Technologies Corporation Structural members in a pedestal array
US7563072B1 (en) * 2006-09-25 2009-07-21 Florida Turbine Technologies, Inc. Turbine airfoil with near-wall spiral flow cooling circuit
US8197184B2 (en) * 2006-10-18 2012-06-12 United Technologies Corporation Vane with enhanced heat transfer
US7669425B2 (en) * 2006-10-25 2010-03-02 Siemens Energy, Inc. Closed loop turbine cooling fluid reuse system for a turbine engine
US7722325B2 (en) * 2006-11-08 2010-05-25 United Technologies Corporation Refractory metal core main body trench
US7556476B1 (en) * 2006-11-16 2009-07-07 Florida Turbine Technologies, Inc. Turbine airfoil with multiple near wall compartment cooling
US20080135721A1 (en) * 2006-12-06 2008-06-12 General Electric Company Casting compositions for manufacturing metal casting and methods of manufacturing thereof
US8413709B2 (en) 2006-12-06 2013-04-09 General Electric Company Composite core die, methods of manufacture thereof and articles manufactured therefrom
US7938168B2 (en) * 2006-12-06 2011-05-10 General Electric Company Ceramic cores, methods of manufacture thereof and articles manufactured from the same
US7624787B2 (en) * 2006-12-06 2009-12-01 General Electric Company Disposable insert, and use thereof in a method for manufacturing an airfoil
US20100034647A1 (en) * 2006-12-07 2010-02-11 General Electric Company Processes for the formation of positive features on shroud components, and related articles
US7487819B2 (en) * 2006-12-11 2009-02-10 General Electric Company Disposable thin wall core die, methods of manufacture thereof and articles manufactured therefrom
US8884182B2 (en) 2006-12-11 2014-11-11 General Electric Company Method of modifying the end wall contour in a turbine using laser consolidation and the turbines derived therefrom
US7753650B1 (en) 2006-12-20 2010-07-13 Florida Turbine Technologies, Inc. Thin turbine rotor blade with sinusoidal flow cooling channels
US8757974B2 (en) * 2007-01-11 2014-06-24 United Technologies Corporation Cooling circuit flow path for a turbine section airfoil
US7837441B2 (en) * 2007-02-16 2010-11-23 United Technologies Corporation Impingement skin core cooling for gas turbine engine blade
US7946815B2 (en) * 2007-03-27 2011-05-24 Siemens Energy, Inc. Airfoil for a gas turbine engine
US7789625B2 (en) * 2007-05-07 2010-09-07 Siemens Energy, Inc. Turbine airfoil with enhanced cooling
US7854591B2 (en) * 2007-05-07 2010-12-21 Siemens Energy, Inc. Airfoil for a turbine of a gas turbine engine
US7717675B1 (en) * 2007-05-24 2010-05-18 Florida Turbine Technologies, Inc. Turbine airfoil with a near wall mini serpentine cooling circuit
US10156143B2 (en) * 2007-12-06 2018-12-18 United Technologies Corporation Gas turbine engines and related systems involving air-cooled vanes
EP2265800B1 (de) 2008-03-31 2017-11-01 Ansaldo Energia IP UK Limited Kühlkanalanordnung innerhalb eines hohlgegossenen gussteils
JP5182931B2 (ja) * 2008-05-30 2013-04-17 三菱重工業株式会社 タービン用翼
EP2143883A1 (de) * 2008-07-10 2010-01-13 Siemens Aktiengesellschaft Turbinenschaufel und entsprechender Gusskern
US8096770B2 (en) * 2008-09-25 2012-01-17 Siemens Energy, Inc. Trailing edge cooling for turbine blade airfoil
US8303253B1 (en) * 2009-01-22 2012-11-06 Florida Turbine Technologies, Inc. Turbine airfoil with near-wall mini serpentine cooling channels
US8182224B1 (en) * 2009-02-17 2012-05-22 Florida Turbine Technologies, Inc. Turbine blade having a row of spanwise nearwall serpentine cooling circuits
US8147196B2 (en) * 2009-05-05 2012-04-03 Siemens Energy, Inc. Turbine airfoil with a compliant outer wall
US9528382B2 (en) * 2009-11-10 2016-12-27 General Electric Company Airfoil heat shield
US8790083B1 (en) * 2009-11-17 2014-07-29 Florida Turbine Technologies, Inc. Turbine airfoil with trailing edge cooling
US8511994B2 (en) * 2009-11-23 2013-08-20 United Technologies Corporation Serpentine cored airfoil with body microcircuits
US8944141B2 (en) * 2010-12-22 2015-02-03 United Technologies Corporation Drill to flow mini core
US8961133B2 (en) 2010-12-28 2015-02-24 Rolls-Royce North American Technologies, Inc. Gas turbine engine and cooled airfoil
US10060264B2 (en) * 2010-12-30 2018-08-28 Rolls-Royce North American Technologies Inc. Gas turbine engine and cooled flowpath component therefor
US9017027B2 (en) 2011-01-06 2015-04-28 Siemens Energy, Inc. Component having cooling channel with hourglass cross section
US8764394B2 (en) 2011-01-06 2014-07-01 Siemens Energy, Inc. Component cooling channel
US9011077B2 (en) 2011-04-20 2015-04-21 Siemens Energy, Inc. Cooled airfoil in a turbine engine
US8807945B2 (en) 2011-06-22 2014-08-19 United Technologies Corporation Cooling system for turbine airfoil including ice-cream-cone-shaped pedestals
US20130052036A1 (en) * 2011-08-30 2013-02-28 General Electric Company Pin-fin array
US9249675B2 (en) * 2011-08-30 2016-02-02 General Electric Company Pin-fin array
US8840363B2 (en) 2011-09-09 2014-09-23 Siemens Energy, Inc. Trailing edge cooling system in a turbine airfoil assembly
US8882448B2 (en) 2011-09-09 2014-11-11 Siemens Aktiengesellshaft Cooling system in a turbine airfoil assembly including zigzag cooling passages interconnected with radial passageways
US8882461B2 (en) 2011-09-12 2014-11-11 Honeywell International Inc. Gas turbine engines with improved trailing edge cooling arrangements
US8840371B2 (en) * 2011-10-07 2014-09-23 General Electric Company Methods and systems for use in regulating a temperature of components
US20130243575A1 (en) * 2012-03-13 2013-09-19 United Technologies Corporation Cooling pedestal array
BR112014026360A2 (pt) 2012-04-23 2017-06-27 Gen Electric aerofólio de turbina e pá de turbina
US20130302177A1 (en) * 2012-05-08 2013-11-14 Robert Frederick Bergholz, JR. Turbine airfoil trailing edge bifurcated cooling holes
US10100645B2 (en) 2012-08-13 2018-10-16 United Technologies Corporation Trailing edge cooling configuration for a gas turbine engine airfoil
US9267381B2 (en) * 2012-09-28 2016-02-23 Honeywell International Inc. Cooled turbine airfoil structures
US8936067B2 (en) 2012-10-23 2015-01-20 Siemens Aktiengesellschaft Casting core for a cooling arrangement for a gas turbine component
US8951004B2 (en) 2012-10-23 2015-02-10 Siemens Aktiengesellschaft Cooling arrangement for a gas turbine component
US9995150B2 (en) 2012-10-23 2018-06-12 Siemens Aktiengesellschaft Cooling configuration for a gas turbine engine airfoil
EP2971543B1 (de) 2013-03-15 2020-08-19 United Technologies Corporation Gasturbinentriebwerkskomponente mit geformten sockeln
US8985949B2 (en) 2013-04-29 2015-03-24 Siemens Aktiengesellschaft Cooling system including wavy cooling chamber in a trailing edge portion of an airfoil assembly
CN106661945A (zh) 2014-09-04 2017-05-10 西门子公司 带有在燃气涡轮翼型的尾部冷却腔中形成近壁冷却通道的插入件的内部冷却系统
CN107075955A (zh) * 2014-09-04 2017-08-18 西门子公司 具有在燃气涡轮机翼型件的后部冷却腔中形成近壁冷却通道的插入件的包括散热肋的内部冷却系统
EP3189214A1 (de) * 2014-09-04 2017-07-12 Siemens Aktiengesellschaft Internes kühlsystem mit einsatz zur formung von nahwandigen kühlkanälen in den mittelgurtkühlhohlräumen einer gasturbinenschaufel
US20160090843A1 (en) * 2014-09-30 2016-03-31 General Electric Company Turbine components with stepped apertures
US10392942B2 (en) 2014-11-26 2019-08-27 Ansaldo Energia Ip Uk Limited Tapered cooling channel for airfoil
WO2016160029A1 (en) 2015-04-03 2016-10-06 Siemens Aktiengesellschaft Turbine blade trailing edge with low flow framing channel
US10323524B2 (en) * 2015-05-08 2019-06-18 United Technologies Corporation Axial skin core cooling passage for a turbine engine component
US10502066B2 (en) 2015-05-08 2019-12-10 United Technologies Corporation Turbine engine component including an axially aligned skin core passage interrupted by a pedestal
US10174620B2 (en) 2015-10-15 2019-01-08 General Electric Company Turbine blade
US10871075B2 (en) * 2015-10-27 2020-12-22 Pratt & Whitney Canada Corp. Cooling passages in a turbine component
US9938836B2 (en) 2015-12-22 2018-04-10 General Electric Company Turbine airfoil with trailing edge cooling circuit
US9909427B2 (en) 2015-12-22 2018-03-06 General Electric Company Turbine airfoil with trailing edge cooling circuit
US10704395B2 (en) * 2016-05-10 2020-07-07 General Electric Company Airfoil with cooling circuit
US10808571B2 (en) * 2017-06-22 2020-10-20 Raytheon Technologies Corporation Gaspath component including minicore plenums
US10502093B2 (en) * 2017-12-13 2019-12-10 Pratt & Whitney Canada Corp. Turbine shroud cooling
US10648343B2 (en) * 2018-01-09 2020-05-12 United Technologies Corporation Double wall turbine gas turbine engine vane platform cooling configuration with main core resupply
US10753210B2 (en) * 2018-05-02 2020-08-25 Raytheon Technologies Corporation Airfoil having improved cooling scheme
US11339718B2 (en) * 2018-11-09 2022-05-24 Raytheon Technologies Corporation Minicore cooling passage network having trip strips
US11092017B2 (en) 2018-11-09 2021-08-17 Raytheon Technologies Corporation Mini core passage with protrusion
US11149556B2 (en) 2018-11-09 2021-10-19 Raytheon Technologies Corporation Minicore cooling passage network having sloped impingement surface
US11566527B2 (en) 2018-12-18 2023-01-31 General Electric Company Turbine engine airfoil and method of cooling
US10767492B2 (en) 2018-12-18 2020-09-08 General Electric Company Turbine engine airfoil
US11499433B2 (en) 2018-12-18 2022-11-15 General Electric Company Turbine engine component and method of cooling
US11352889B2 (en) 2018-12-18 2022-06-07 General Electric Company Airfoil tip rail and method of cooling
US11174736B2 (en) 2018-12-18 2021-11-16 General Electric Company Method of forming an additively manufactured component
CN110080828B (zh) * 2019-04-15 2021-09-03 西北工业大学 一种带线轴型扰流柱及双倒圆出口的网格缝气膜冷却结构
US10844728B2 (en) 2019-04-17 2020-11-24 General Electric Company Turbine engine airfoil with a trailing edge
US11486257B2 (en) * 2019-05-03 2022-11-01 Raytheon Technologies Corporation Cooling passage configuration
US12050062B2 (en) 2021-10-06 2024-07-30 Ge Infrastructure Technology Llc Stacked cooling assembly for gas turbine combustor
US11486259B1 (en) 2021-11-05 2022-11-01 General Electric Company Component with cooling passage for a turbine engine
US11560803B1 (en) 2021-11-05 2023-01-24 General Electric Company Component with cooling passage for a turbine engine
US11859511B2 (en) * 2021-11-05 2024-01-02 Rolls-Royce North American Technologies Inc. Co and counter flow heat exchanger
CN113914938B (zh) * 2021-12-10 2022-02-22 中国航发燃气轮机有限公司 一种燃气轮机透平气冷叶片
JP2023172704A (ja) * 2022-05-24 2023-12-06 三菱重工業株式会社 タービン翼及びガスタービン

Family Cites Families (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1257041A (de) * 1968-03-27 1971-12-15
US3819295A (en) 1972-09-21 1974-06-25 Gen Electric Cooling slot for airfoil blade
US3902820A (en) 1973-07-02 1975-09-02 Westinghouse Electric Corp Fluid cooled turbine rotor blade
US3973874A (en) 1974-09-25 1976-08-10 General Electric Company Impingement baffle collars
CH584347A5 (de) 1974-11-08 1977-01-31 Bbc Sulzer Turbomaschinen
US4042162A (en) 1975-07-11 1977-08-16 General Motors Corporation Airfoil fabrication
US4353679A (en) 1976-07-29 1982-10-12 General Electric Company Fluid-cooled element
US4080095A (en) 1976-09-02 1978-03-21 Westinghouse Electric Corporation Cooled turbine vane
US4221539A (en) 1977-04-20 1980-09-09 The Garrett Corporation Laminated airfoil and method for turbomachinery
US4203706A (en) 1977-12-28 1980-05-20 United Technologies Corporation Radial wafer airfoil construction
US4185369A (en) 1978-03-22 1980-01-29 General Electric Company Method of manufacture of cooled turbine or compressor buckets
US4278400A (en) * 1978-09-05 1981-07-14 United Technologies Corporation Coolable rotor blade
GB2163219B (en) 1981-10-31 1986-08-13 Rolls Royce Cooled turbine blade
US4487550A (en) 1983-01-27 1984-12-11 The United States Of America As Represented By The Secretary Of The Air Force Cooled turbine blade tip closure
US4542867A (en) 1983-01-31 1985-09-24 United Technologies Corporation Internally cooled hollow airfoil
US4529358A (en) 1984-02-15 1985-07-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Vortex generating flow passage design for increased film cooling effectiveness
US4601638A (en) 1984-12-21 1986-07-22 United Technologies Corporation Airfoil trailing edge cooling arrangement
US4669957A (en) 1985-12-23 1987-06-02 United Technologies Corporation Film coolant passage with swirl diffuser
GB2192705B (en) 1986-07-18 1990-06-06 Rolls Royce Plc Porous sheet structure for a combustion chamber
US4768700A (en) 1987-08-17 1988-09-06 General Motors Corporation Diffusion bonding method
US5405242A (en) * 1990-07-09 1995-04-11 United Technologies Corporation Cooled vane
US5383766A (en) * 1990-07-09 1995-01-24 United Technologies Corporation Cooled vane
US5695320A (en) 1991-12-17 1997-12-09 General Electric Company Turbine blade having auxiliary turbulators
US5370499A (en) 1992-02-03 1994-12-06 General Electric Company Film cooling of turbine airfoil wall using mesh cooling hole arrangement
US5403159A (en) 1992-11-30 1995-04-04 United Technoligies Corporation Coolable airfoil structure
US5344283A (en) 1993-01-21 1994-09-06 United Technologies Corporation Turbine vane having dedicated inner platform cooling
US5649806A (en) * 1993-11-22 1997-07-22 United Technologies Corporation Enhanced film cooling slot for turbine blade outer air seals
US5340074A (en) 1993-12-15 1994-08-23 Accessories Associates, Inc. Eyeglass display hanger
JP3651490B2 (ja) * 1993-12-28 2005-05-25 株式会社東芝 タービン冷却翼
US5484258A (en) 1994-03-01 1996-01-16 General Electric Company Turbine airfoil with convectively cooled double shell outer wall
US5413458A (en) 1994-03-29 1995-05-09 United Technologies Corporation Turbine vane with a platform cavity having a double feed for cooling fluid
US5820337A (en) 1995-01-03 1998-10-13 General Electric Company Double wall turbine parts
EP0742347A3 (de) * 1995-05-10 1998-04-01 Allison Engine Company, Inc. Turbinenschaufelkühlung
US5772397A (en) * 1996-05-08 1998-06-30 Alliedsignal Inc. Gas turbine airfoil with aft internal cooling
US5771577A (en) 1996-05-17 1998-06-30 General Electric Company Method for making a fluid cooled article with protective coating
US5822853A (en) 1996-06-24 1998-10-20 General Electric Company Method for making cylindrical structures with cooling channels
WO1998025009A1 (de) * 1996-12-02 1998-06-11 Siemens Aktiengesellschaft Turbinenschaufel sowie verwendung in einer gasturbinenanlage
US5813836A (en) 1996-12-24 1998-09-29 General Electric Company Turbine blade
US5931638A (en) * 1997-08-07 1999-08-03 United Technologies Corporation Turbomachinery airfoil with optimized heat transfer
US5976337A (en) * 1997-10-27 1999-11-02 Allison Engine Company Method for electrophoretic deposition of brazing material
EP0945595A3 (de) * 1998-03-26 2001-10-10 Mitsubishi Heavy Industries, Ltd. Gekühlte Gasturbinenschaufel
US6213714B1 (en) * 1999-06-29 2001-04-10 Allison Advanced Development Company Cooled airfoil
US6402470B1 (en) * 1999-10-05 2002-06-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine

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JP2001107704A (ja) 2001-04-17
EP1091091B1 (de) 2008-09-24
DE60041091D1 (de) 2009-01-22
EP1619353B1 (de) 2008-12-10
EP1617043B1 (de) 2008-06-11
EP1617043A1 (de) 2006-01-18
EP1091091A3 (de) 2004-03-24
EP1091091A2 (de) 2001-04-11
DE60040324D1 (de) 2008-11-06
US6254334B1 (en) 2001-07-03
EP1619353A1 (de) 2006-01-25

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