JP2001027102A - タービン動翼の後縁冷却孔及び溝穴 - Google Patents

タービン動翼の後縁冷却孔及び溝穴

Info

Publication number
JP2001027102A
JP2001027102A JP2000197544A JP2000197544A JP2001027102A JP 2001027102 A JP2001027102 A JP 2001027102A JP 2000197544 A JP2000197544 A JP 2000197544A JP 2000197544 A JP2000197544 A JP 2000197544A JP 2001027102 A JP2001027102 A JP 2001027102A
Authority
JP
Japan
Prior art keywords
trailing edge
cooling
airfoil
lower portion
upper portion
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Withdrawn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
JP2000197544A
Other languages
English (en)
Japanese (ja)
Other versions
JP2001027102A5 (enExample
Inventor
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 JP2001027102A publication Critical patent/JP2001027102A/ja
Publication of JP2001027102A5 publication Critical patent/JP2001027102A5/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Withdrawn legal-status Critical Current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
    • F01D5/20—Specially-shaped blade tips to seal space between tips and stator
    • 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
    • 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
    • F01D5/187—Convection cooling
    • 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)
JP2000197544A 1999-06-30 2000-06-30 タービン動翼の後縁冷却孔及び溝穴 Withdrawn JP2001027102A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/345190 1999-06-30
US09/345,190 US6174135B1 (en) 1999-06-30 1999-06-30 Turbine blade trailing edge cooling openings and slots

Publications (2)

Publication Number Publication Date
JP2001027102A true JP2001027102A (ja) 2001-01-30
JP2001027102A5 JP2001027102A5 (enExample) 2007-08-16

Family

ID=23353951

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2000197544A Withdrawn JP2001027102A (ja) 1999-06-30 2000-06-30 タービン動翼の後縁冷却孔及び溝穴

Country Status (4)

Country Link
US (1) US6174135B1 (enExample)
EP (1) EP1065344B1 (enExample)
JP (1) JP2001027102A (enExample)
DE (1) DE60033089T2 (enExample)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005351277A (ja) * 2004-06-10 2005-12-22 General Electric Co <Ge> ガスタービンロータブレードを冷却するための方法及び装置
JP2010007650A (ja) * 2008-06-30 2010-01-14 Mitsubishi Heavy Ind Ltd タービン翼およびガスタービン

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2002221005A (ja) * 2001-01-26 2002-08-09 Ishikawajima Harima Heavy Ind Co Ltd 冷却タービン翼
US6561758B2 (en) 2001-04-27 2003-05-13 General Electric Company Methods and systems for cooling gas turbine engine airfoils
US6551062B2 (en) 2001-08-30 2003-04-22 General Electric Company Turbine airfoil for gas turbine engine
US6609891B2 (en) 2001-08-30 2003-08-26 General Electric Company Turbine airfoil for gas turbine engine
US6599092B1 (en) 2002-01-04 2003-07-29 General Electric Company Methods and apparatus for cooling gas turbine nozzles
US6602047B1 (en) 2002-02-28 2003-08-05 General Electric Company Methods and apparatus for cooling gas turbine nozzles
US6932570B2 (en) * 2002-05-23 2005-08-23 General Electric Company Methods and apparatus for extending gas turbine engine airfoils useful life
US6746209B2 (en) 2002-05-31 2004-06-08 General Electric Company Methods and apparatus for cooling gas turbine engine nozzle assemblies
US6923616B2 (en) * 2003-09-02 2005-08-02 General Electric Company Methods and apparatus for cooling gas turbine engine rotor assemblies
EP1512489B1 (de) * 2003-09-05 2006-12-20 Siemens Aktiengesellschaft Schaufel einer Turbine
US7008186B2 (en) 2003-09-17 2006-03-07 General Electric Company Teardrop film cooled blade
US6984112B2 (en) * 2003-10-31 2006-01-10 General Electric Company Methods and apparatus for cooling gas turbine rotor blades
US7600972B2 (en) * 2003-10-31 2009-10-13 General Electric Company Methods and apparatus for cooling gas turbine engine rotor assemblies
US6984103B2 (en) * 2003-11-20 2006-01-10 General Electric Company Triple circuit turbine blade
JP2005233141A (ja) * 2004-02-23 2005-09-02 Mitsubishi Heavy Ind Ltd 動翼およびその動翼を用いたガスタービン
US20050220618A1 (en) * 2004-03-31 2005-10-06 General Electric Company Counter-bored film-cooling holes and related method
US7118337B2 (en) * 2004-06-17 2006-10-10 Siemens Power Generation, Inc. Gas turbine airfoil trailing edge corner
US7806659B1 (en) 2007-07-10 2010-10-05 Florida Turbine Technologies, Inc. Turbine blade with trailing edge bleed slot arrangement
US8002525B2 (en) * 2007-11-16 2011-08-23 Siemens Energy, Inc. Turbine airfoil cooling system with recessed trailing edge cooling slot
FR2924156B1 (fr) * 2007-11-26 2014-02-14 Snecma Aube de turbomachine
US8257035B2 (en) * 2007-12-05 2012-09-04 Siemens Energy, Inc. Turbine vane for a gas turbine engine
US8206115B2 (en) * 2008-09-26 2012-06-26 General Electric Company Scalloped surface turbine stage with trailing edge ridges
US9133819B2 (en) 2011-07-18 2015-09-15 Kohana Technologies Inc. Turbine blades and systems with forward blowing slots
US9200523B2 (en) * 2012-03-14 2015-12-01 Honeywell International Inc. Turbine blade tip cooling
US9228437B1 (en) 2012-03-22 2016-01-05 Florida Turbine Technologies, Inc. Turbine airfoil with pressure side trailing edge cooling slots
US9045987B2 (en) 2012-06-15 2015-06-02 United Technologies Corporation Cooling for a turbine airfoil trailing edge
CN107429568B (zh) 2015-03-17 2019-11-29 西门子能源有限公司 用于涡轮发动机中的翼型件的在后缘冷却通道中具有收缩扩张出口槽的内部冷却系统
US10753210B2 (en) * 2018-05-02 2020-08-25 Raytheon Technologies Corporation Airfoil having improved cooling scheme
US10801334B2 (en) * 2018-09-12 2020-10-13 Raytheon Technologies Corporation Cooling arrangement with purge partition
US12123319B2 (en) * 2020-12-30 2024-10-22 Ge Infrastructure Technology Llc Cooling circuit having a bypass conduit for a turbomachine component
CN115075891A (zh) * 2022-05-29 2022-09-20 中国船舶重工集团公司第七0三研究所 一种压力侧排气的气冷涡轮导叶尾缘结构
US12448894B2 (en) 2024-01-26 2025-10-21 Ge Infrastructure Technology Llc Aerodynamic turbomachine component with cooling features and method of making

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4726104A (en) * 1986-11-20 1988-02-23 United Technologies Corporation Methods for weld repairing hollow, air cooled turbine blades and vanes
US4883404A (en) * 1988-03-11 1989-11-28 Sherman Alden O Gas turbine vanes and methods for making same
FR2678318B1 (fr) * 1991-06-25 1993-09-10 Snecma Aube refroidie de distributeur de turbine.
FR2689176B1 (fr) * 1992-03-25 1995-07-13 Snecma Aube refrigeree de turbo-machine.
US5503529A (en) * 1994-12-08 1996-04-02 General Electric Company Turbine blade having angled ejection slot
US5503527A (en) * 1994-12-19 1996-04-02 General Electric Company Turbine blade having tip slot
FR2743391B1 (fr) * 1996-01-04 1998-02-06 Snecma Aube refrigeree de distributeur de turbine
US5733102A (en) * 1996-12-17 1998-03-31 General Electric Company Slot cooled blade tip
US6059530A (en) * 1998-12-21 2000-05-09 General Electric Company Twin rib turbine blade
US6126397A (en) * 1998-12-22 2000-10-03 United Technologies Corporation Trailing edge cooling apparatus for a gas turbine airfoil
US6176677B1 (en) * 1999-05-19 2001-01-23 Pratt & Whitney Canada Corp. Device for controlling air flow in a turbine blade

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2005351277A (ja) * 2004-06-10 2005-12-22 General Electric Co <Ge> ガスタービンロータブレードを冷却するための方法及び装置
JP2010007650A (ja) * 2008-06-30 2010-01-14 Mitsubishi Heavy Ind Ltd タービン翼およびガスタービン

Also Published As

Publication number Publication date
EP1065344A3 (en) 2003-12-03
DE60033089D1 (de) 2007-03-15
EP1065344B1 (en) 2007-01-24
DE60033089T2 (de) 2007-10-11
EP1065344A2 (en) 2001-01-03
US6174135B1 (en) 2001-01-16

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