SG134207A1 - Turbine airfoil with improved cooling - Google Patents

Turbine airfoil with improved cooling

Info

Publication number
SG134207A1
SG134207A1 SG200607891-9A SG2006078919A SG134207A1 SG 134207 A1 SG134207 A1 SG 134207A1 SG 2006078919 A SG2006078919 A SG 2006078919A SG 134207 A1 SG134207 A1 SG 134207A1
Authority
SG
Singapore
Prior art keywords
minicores
turbine airfoil
cooling
improved cooling
airfoil
Prior art date
Application number
SG200607891-9A
Other languages
English (en)
Inventor
Matthew A Devore
Corneil S Paauwe
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
Publication of SG134207A1 publication Critical patent/SG134207A1/en

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/186—Film cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2212—Improvement of heat transfer by creating turbulence
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
SG200607891-9A 2006-01-17 2006-11-14 Turbine airfoil with improved cooling SG134207A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/333,140 US7600966B2 (en) 2006-01-17 2006-01-17 Turbine airfoil with improved cooling

Publications (1)

Publication Number Publication Date
SG134207A1 true SG134207A1 (en) 2007-08-29

Family

ID=37698028

Family Applications (1)

Application Number Title Priority Date Filing Date
SG200607891-9A SG134207A1 (en) 2006-01-17 2006-11-14 Turbine airfoil with improved cooling

Country Status (7)

Country Link
US (1) US7600966B2 (ko)
EP (1) EP1808574B1 (ko)
JP (1) JP2007192213A (ko)
KR (1) KR100830276B1 (ko)
CN (1) CN101004143B (ko)
DE (1) DE602006021127D1 (ko)
SG (1) SG134207A1 (ko)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2009121715A1 (de) * 2008-03-31 2009-10-08 Alstom Technology Ltd Kühlkanalanordnung innerhalb eines hohlgegossenen gussteils
US8215181B1 (en) * 2008-09-04 2012-07-10 Rolls-Royce North American Technologies, Inc. Evaluation technique for bonded, dual wall static and rotating airfoil materials
DE102008052409A1 (de) * 2008-10-21 2010-04-22 Rolls-Royce Deutschland Ltd & Co Kg Strömungsarbeitsmaschine mit saugseitennaher Randenergetisierung
GB2467790B (en) 2009-02-16 2011-06-01 Rolls Royce Plc Vane
US8562286B2 (en) 2010-04-06 2013-10-22 United Technologies Corporation Dead ended bulbed rib geometry for a gas turbine engine
US8944141B2 (en) * 2010-12-22 2015-02-03 United Technologies Corporation Drill to flow mini core
US9759072B2 (en) 2012-08-30 2017-09-12 United Technologies Corporation Gas turbine engine airfoil cooling circuit arrangement
US9115590B2 (en) 2012-09-26 2015-08-25 United Technologies Corporation Gas turbine engine airfoil cooling circuit
US10012106B2 (en) 2014-04-03 2018-07-03 United Technologies Corporation Enclosed baffle for a turbine engine component
US10808571B2 (en) 2017-06-22 2020-10-20 Raytheon Technologies Corporation Gaspath component including minicore plenums
US10731474B2 (en) 2018-03-02 2020-08-04 Raytheon Technologies Corporation Airfoil with varying wall thickness
US10968752B2 (en) * 2018-06-19 2021-04-06 Raytheon Technologies Corporation Turbine airfoil with minicore passage having sloped diffuser orifice
US11180998B2 (en) * 2018-11-09 2021-11-23 Raytheon Technologies Corporation Airfoil with skincore passage resupply
US11092017B2 (en) * 2018-11-09 2021-08-17 Raytheon Technologies Corporation Mini core passage with protrusion
US11293347B2 (en) 2018-11-09 2022-04-05 Raytheon Technologies Corporation Airfoil with baffle showerhead and cooling passage network having aft inlet
US10975710B2 (en) * 2018-12-05 2021-04-13 Raytheon Technologies Corporation Cooling circuit for gas turbine engine component
US11028702B2 (en) * 2018-12-13 2021-06-08 Raytheon Technologies Corporation Airfoil with cooling passage network having flow guides
US11486257B2 (en) * 2019-05-03 2022-11-01 Raytheon Technologies Corporation Cooling passage configuration
DE102019125779B4 (de) * 2019-09-25 2024-03-21 Man Energy Solutions Se Schaufel einer Strömungsmaschine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5392515A (en) * 1990-07-09 1995-02-28 United Technologies Corporation Method of manufacturing an air cooled vane with film cooling pocket construction
EP1091091A2 (en) * 1999-10-05 2001-04-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
EP1091092A2 (en) * 1999-10-05 2001-04-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
EP1505257A2 (en) * 2003-08-08 2005-02-09 United Technologies Corporation Gas turbine blade circuit cooling

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4542867A (en) 1983-01-31 1985-09-24 United Technologies Corporation Internally cooled hollow airfoil
US6000908A (en) * 1996-11-05 1999-12-14 General Electric Company Cooling for double-wall structures
CA2288557C (en) * 1998-11-12 2007-02-06 Mitsubishi Heavy Industries, Ltd. Gas turbine combustor cooling structure
US6164912A (en) * 1998-12-21 2000-12-26 United Technologies Corporation Hollow airfoil for a gas turbine engine
WO2000053896A1 (de) * 1999-03-09 2000-09-14 Siemens Aktiengesellschaft Turbinenschaufel und verfahren zur herstellung einer turbinenschaufel
US6932571B2 (en) * 2003-02-05 2005-08-23 United Technologies Corporation Microcircuit cooling for a turbine blade tip
US6890154B2 (en) 2003-08-08 2005-05-10 United Technologies Corporation Microcircuit cooling for a turbine blade
US7255534B2 (en) * 2004-07-02 2007-08-14 Siemens Power Generation, Inc. Gas turbine vane with integral cooling system

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5392515A (en) * 1990-07-09 1995-02-28 United Technologies Corporation Method of manufacturing an air cooled vane with film cooling pocket construction
EP1091091A2 (en) * 1999-10-05 2001-04-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
EP1091092A2 (en) * 1999-10-05 2001-04-11 United Technologies Corporation Method and apparatus for cooling a wall within a gas turbine engine
EP1505257A2 (en) * 2003-08-08 2005-02-09 United Technologies Corporation Gas turbine blade circuit cooling

Also Published As

Publication number Publication date
EP1808574A2 (en) 2007-07-18
DE602006021127D1 (de) 2011-05-19
US20070166161A1 (en) 2007-07-19
KR100830276B1 (ko) 2008-05-19
JP2007192213A (ja) 2007-08-02
KR20070076393A (ko) 2007-07-24
US7600966B2 (en) 2009-10-13
EP1808574B1 (en) 2011-04-06
CN101004143B (zh) 2011-06-15
EP1808574A3 (en) 2008-05-21
CN101004143A (zh) 2007-07-25

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