JP4436500B2 - エーロフォイルの前縁隔離冷却 - Google Patents

エーロフォイルの前縁隔離冷却 Download PDF

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Publication number
JP4436500B2
JP4436500B2 JP32480999A JP32480999A JP4436500B2 JP 4436500 B2 JP4436500 B2 JP 4436500B2 JP 32480999 A JP32480999 A JP 32480999A JP 32480999 A JP32480999 A JP 32480999A JP 4436500 B2 JP4436500 B2 JP 4436500B2
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JP
Japan
Prior art keywords
passage
leading edge
airfoil
cooling air
side wall
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 - Fee Related
Application number
JP32480999A
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English (en)
Japanese (ja)
Other versions
JP2000161004A (ja
JP2000161004A5 (enExample
Inventor
ロバート・フランシス・マニング
ポール・ジョセフ・アクアヴィヴァ
ダニエル・エドワード・ディマース
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 JP2000161004A publication Critical patent/JP2000161004A/ja
Publication of JP2000161004A5 publication Critical patent/JP2000161004A5/ja
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Publication of JP4436500B2 publication Critical patent/JP4436500B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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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
    • 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
    • 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
    • F05D2260/202—Heat transfer, e.g. cooling by film cooling

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
JP32480999A 1998-11-16 1999-11-16 エーロフォイルの前縁隔離冷却 Expired - Fee Related JP4436500B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/192229 1998-11-16
US09/192,229 US6183198B1 (en) 1998-11-16 1998-11-16 Airfoil isolated leading edge cooling

Publications (3)

Publication Number Publication Date
JP2000161004A JP2000161004A (ja) 2000-06-13
JP2000161004A5 JP2000161004A5 (enExample) 2006-12-28
JP4436500B2 true JP4436500B2 (ja) 2010-03-24

Family

ID=22708786

Family Applications (1)

Application Number Title Priority Date Filing Date
JP32480999A Expired - Fee Related JP4436500B2 (ja) 1998-11-16 1999-11-16 エーロフォイルの前縁隔離冷却

Country Status (4)

Country Link
US (1) US6183198B1 (enExample)
EP (1) EP1001136B1 (enExample)
JP (1) JP4436500B2 (enExample)
DE (1) DE69923914T2 (enExample)

Families Citing this family (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10027842A1 (de) 2000-06-05 2001-12-20 Alstom Power Nv Verfahren zum Kühlen einer Gasturbinenanlage sowie Gasturbinenanlage zur Durchführung des Verfahrens
US6595748B2 (en) 2001-08-02 2003-07-22 General Electric Company Trichannel airfoil leading edge cooling
US6971851B2 (en) * 2003-03-12 2005-12-06 Florida Turbine Technologies, Inc. Multi-metered film cooled blade tip
US6832889B1 (en) * 2003-07-09 2004-12-21 General Electric Company Integrated bridge turbine blade
US6929446B2 (en) * 2003-10-22 2005-08-16 General Electric Company Counterbalanced flow turbine nozzle
US7195458B2 (en) * 2004-07-02 2007-03-27 Siemens Power Generation, Inc. Impingement cooling system for a turbine blade
US7478994B2 (en) * 2004-11-23 2009-01-20 United Technologies Corporation Airfoil with supplemental cooling channel adjacent leading edge
US7293961B2 (en) * 2005-12-05 2007-11-13 General Electric Company Zigzag cooled turbine airfoil
US7481622B1 (en) * 2006-06-21 2009-01-27 Florida Turbine Technologies, Inc. Turbine airfoil with a serpentine flow path
US7780413B2 (en) * 2006-08-01 2010-08-24 Siemens Energy, Inc. Turbine airfoil with near wall inflow chambers
US7520725B1 (en) * 2006-08-11 2009-04-21 Florida Turbine Technologies, Inc. Turbine airfoil with near-wall leading edge multi-holes cooling
US7497663B2 (en) * 2006-10-26 2009-03-03 General Electric Company Rotor blade profile optimization
US7926289B2 (en) * 2006-11-10 2011-04-19 General Electric Company Dual interstage cooled engine
US7690892B1 (en) * 2006-11-16 2010-04-06 Florida Turbine Technologies, Inc. Turbine airfoil with multiple impingement cooling circuit
JP5022097B2 (ja) * 2007-05-07 2012-09-12 三菱重工業株式会社 タービン用翼
US20090293495A1 (en) * 2008-05-29 2009-12-03 General Electric Company Turbine airfoil with metered cooling cavity
US8070442B1 (en) * 2008-10-01 2011-12-06 Florida Turbine Technologies, Inc. Turbine airfoil with near wall cooling
WO2010052784A1 (ja) * 2008-11-07 2010-05-14 三菱重工業株式会社 タービン用翼
GB0905736D0 (en) * 2009-04-03 2009-05-20 Rolls Royce Plc Cooled aerofoil for a gas turbine engine
DE102010046331A1 (de) * 2010-09-23 2012-03-29 Rolls-Royce Deutschland Ltd & Co Kg Gekühlte Turbinenschaufeln für ein Gasturbinentriebwerk
US20130156602A1 (en) * 2011-12-16 2013-06-20 United Technologies Corporation Film cooled turbine component
US9296039B2 (en) 2012-04-24 2016-03-29 United Technologies Corporation Gas turbine engine airfoil impingement cooling
US9528381B2 (en) * 2013-12-30 2016-12-27 General Electric Company Structural configurations and cooling circuits in turbine blades
US11220912B2 (en) * 2020-04-16 2022-01-11 Raytheon Technologies Corporation Airfoil with y-shaped rib
CN113236372B (zh) * 2021-06-07 2022-06-10 南京航空航天大学 带有射流振荡器的燃气轮机涡轮导叶叶片及工作方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4153386A (en) * 1974-12-11 1979-05-08 United Technologies Corporation Air cooled turbine vanes
FR2725474B1 (fr) * 1984-03-14 1996-12-13 Snecma Aube de distributeur de turbine refroidie
US5690473A (en) * 1992-08-25 1997-11-25 General Electric Company Turbine blade having transpiration strip cooling and method of manufacture
US5356265A (en) 1992-08-25 1994-10-18 General Electric Company Chordally bifurcated turbine blade
US5387085A (en) 1994-01-07 1995-02-07 General Electric Company Turbine blade composite cooling circuit
US5591007A (en) 1995-05-31 1997-01-07 General Electric Company Multi-tier turbine airfoil
US5498133A (en) 1995-06-06 1996-03-12 General Electric Company Pressure regulated film cooling

Also Published As

Publication number Publication date
US6183198B1 (en) 2001-02-06
JP2000161004A (ja) 2000-06-13
EP1001136A2 (en) 2000-05-17
DE69923914D1 (de) 2005-04-07
EP1001136B1 (en) 2005-03-02
DE69923914T2 (de) 2006-04-06
EP1001136A3 (en) 2001-11-28

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