JP2001140601A - 翼形部前縁のスロット式衝突冷却 - Google Patents

翼形部前縁のスロット式衝突冷却

Info

Publication number
JP2001140601A
JP2001140601A JP2000297785A JP2000297785A JP2001140601A JP 2001140601 A JP2001140601 A JP 2001140601A JP 2000297785 A JP2000297785 A JP 2000297785A JP 2000297785 A JP2000297785 A JP 2000297785A JP 2001140601 A JP2001140601 A JP 2001140601A
Authority
JP
Japan
Prior art keywords
airfoil
cooling air
rib
leading edge
longitudinally
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.)
Withdrawn
Application number
JP2000297785A
Other languages
English (en)
Japanese (ja)
Other versions
JP2001140601A5 (https=
Inventor
David Graham William Fargher
デビッド・グラハム・ウィリアム・ファーガー
Ching-Pang Lee
チン−パン・リー
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of JP2001140601A publication Critical patent/JP2001140601A/ja
Publication of JP2001140601A5 publication Critical patent/JP2001140601A5/ja
Withdrawn legal-status Critical Current

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
    • F01D5/187—Convection cooling
    • 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
    • F05D2260/201—Heat transfer, e.g. cooling by impingement of a fluid
    • 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)
JP2000297785A 1999-09-30 2000-09-29 翼形部前縁のスロット式衝突冷却 Withdrawn JP2001140601A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/410,241 US6290463B1 (en) 1999-09-30 1999-09-30 Slotted impingement cooling of airfoil leading edge
US09/410241 1999-09-30

Publications (2)

Publication Number Publication Date
JP2001140601A true JP2001140601A (ja) 2001-05-22
JP2001140601A5 JP2001140601A5 (https=) 2007-11-15

Family

ID=23623871

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2000297785A Withdrawn JP2001140601A (ja) 1999-09-30 2000-09-29 翼形部前縁のスロット式衝突冷却

Country Status (3)

Country Link
US (1) US6290463B1 (https=)
EP (1) EP1088964A3 (https=)
JP (1) JP2001140601A (https=)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110033305A1 (en) * 2008-02-28 2011-02-10 Fathi Ahmad Turbine vane for a stationary gas turbine

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US6582584B2 (en) 1999-08-16 2003-06-24 General Electric Company Method for enhancing heat transfer inside a turbulated cooling passage
US6890153B2 (en) * 2003-04-29 2005-05-10 General Electric Company Castellated turbine airfoil
US7137779B2 (en) * 2004-05-27 2006-11-21 Siemens Power Generation, Inc. Gas turbine airfoil leading edge cooling
US20050265840A1 (en) * 2004-05-27 2005-12-01 Levine Jeffrey R Cooled rotor blade with leading edge impingement cooling
US7217094B2 (en) * 2004-10-18 2007-05-15 United Technologies Corporation Airfoil with large fillet and micro-circuit cooling
US7478994B2 (en) * 2004-11-23 2009-01-20 United Technologies Corporation Airfoil with supplemental cooling channel adjacent leading edge
US7189060B2 (en) * 2005-01-07 2007-03-13 Siemens Power Generation, Inc. Cooling system including mini channels within a turbine blade of a turbine engine
US7416390B2 (en) * 2005-03-29 2008-08-26 Siemens Power Generation, Inc. Turbine blade leading edge cooling system
US7387492B2 (en) * 2005-12-20 2008-06-17 General Electric Company Methods and apparatus for cooling turbine blade trailing edges
US8757974B2 (en) * 2007-01-11 2014-06-24 United Technologies Corporation Cooling circuit flow path for a turbine section airfoil
US7670113B1 (en) 2007-05-31 2010-03-02 Florida Turbine Technologies, Inc. Turbine airfoil with serpentine trailing edge cooling circuit
GB0813839D0 (en) 2008-07-30 2008-09-03 Rolls Royce Plc An aerofoil and method for making an aerofoil
US8152451B2 (en) * 2008-11-29 2012-04-10 General Electric Company Split fairing for a gas turbine engine
US7988419B1 (en) * 2008-12-15 2011-08-02 Florida Turbine Technologies, Inc. Turbine blade with serpentine flow cooling
US8118553B2 (en) * 2009-03-20 2012-02-21 Siemens Energy, Inc. Turbine airfoil cooling system with dual serpentine cooling chambers
US8511968B2 (en) * 2009-08-13 2013-08-20 Siemens Energy, Inc. Turbine vane for a gas turbine engine having serpentine cooling channels with internal flow blockers
US8628298B1 (en) * 2011-07-22 2014-01-14 Florida Turbine Technologies, Inc. Turbine rotor blade with serpentine cooling
US8840370B2 (en) 2011-11-04 2014-09-23 General Electric Company Bucket assembly for turbine system
CN104204412B (zh) * 2012-03-22 2016-09-28 通用电器技术有限公司 涡轮叶片
US9470095B2 (en) * 2012-04-24 2016-10-18 United Technologies Corporation Airfoil having internal lattice network
US9376922B2 (en) 2013-01-09 2016-06-28 General Electric Company Interior configuration for turbine rotor blade
EP2863010A1 (de) * 2013-10-21 2015-04-22 Siemens Aktiengesellschaft Turbinenschaufel
US9726023B2 (en) * 2015-01-26 2017-08-08 United Technologies Corporation Airfoil support and cooling scheme
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
EP3124744A1 (de) * 2015-07-29 2017-02-01 Siemens Aktiengesellschaft Leitschaufel mit prallgekühlter plattform
US10753210B2 (en) * 2018-05-02 2020-08-25 Raytheon Technologies Corporation Airfoil having improved cooling scheme
US10787932B2 (en) * 2018-07-13 2020-09-29 Honeywell International Inc. Turbine blade with dust tolerant cooling system
US10731478B2 (en) * 2018-12-12 2020-08-04 Solar Turbines Incorporated Turbine blade with a coupled serpentine channel
US11629602B2 (en) * 2021-06-17 2023-04-18 Raytheon Technologies Corporation Cooling schemes for airfoils for gas turbine engines
CN115324658B (zh) * 2022-08-01 2025-11-21 中国联合重型燃气轮机技术有限公司 一种适用于燃气轮机上下进气的冲击型透平静叶、透平和燃气轮机
US12540552B2 (en) 2023-03-07 2026-02-03 Rtx Corporation Airfoils with axial leading edge impingement slots
US12065944B1 (en) 2023-03-07 2024-08-20 Rtx Corporation Airfoils with mixed skin passageway cooling

Family Cites Families (14)

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Publication number Priority date Publication date Assignee Title
US3045965A (en) * 1959-04-27 1962-07-24 Rolls Royce Turbine blades, vanes and the like
GB960071A (en) * 1961-08-30 1964-06-10 Rolls Royce Improvements relating to cooled blades such as axial flow gas turbine blades
GB1033759A (en) * 1965-05-17 1966-06-22 Rolls Royce Aerofoil-shaped blade
US3623825A (en) * 1969-11-13 1971-11-30 Avco Corp Liquid-metal-filled rotor blade
US3781129A (en) 1972-09-15 1973-12-25 Gen Motors Corp Cooled airfoil
US3921271A (en) * 1973-01-02 1975-11-25 Gen Electric Air-cooled turbine blade and method of making same
GB1564608A (en) 1975-12-20 1980-04-10 Rolls Royce Means for cooling a surface by the impingement of a cooling fluid
US4314794A (en) 1979-10-25 1982-02-09 Westinghouse Electric Corp. Transpiration cooled blade for a gas turbine engine
DE3211139C1 (de) 1982-03-26 1983-08-11 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Axialturbinenschaufel,insbesondere Axialturbinenlaufschaufel fuer Gasturbinentriebwerke
GB2259118B (en) * 1991-08-24 1995-06-21 Rolls Royce Plc Aerofoil cooling
US5387085A (en) * 1994-01-07 1995-02-07 General Electric Company Turbine blade composite cooling circuit
US5603606A (en) * 1994-11-14 1997-02-18 Solar Turbines Incorporated Turbine cooling system
US5591007A (en) 1995-05-31 1997-01-07 General Electric Company Multi-tier turbine airfoil
US5902093A (en) 1997-08-22 1999-05-11 General Electric Company Crack arresting rotor blade

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20110033305A1 (en) * 2008-02-28 2011-02-10 Fathi Ahmad Turbine vane for a stationary gas turbine
US8602741B2 (en) * 2008-02-28 2013-12-10 Siemens Aktiengesellscaft Turbine vane for a stationary gas turbine

Also Published As

Publication number Publication date
US6290463B1 (en) 2001-09-18
EP1088964A2 (en) 2001-04-04
EP1088964A3 (en) 2003-09-17

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