DE60306825D1 - Verfahren und Vorrichtung für die Kühlung von Gasturbinenleitschaufeln - Google Patents
Verfahren und Vorrichtung für die Kühlung von GasturbinenleitschaufelnInfo
- Publication number
- DE60306825D1 DE60306825D1 DE60306825T DE60306825T DE60306825D1 DE 60306825 D1 DE60306825 D1 DE 60306825D1 DE 60306825 T DE60306825 T DE 60306825T DE 60306825 T DE60306825 T DE 60306825T DE 60306825 D1 DE60306825 D1 DE 60306825D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- cooling gas
- guide vanes
- turbine guide
- vanes
- 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
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
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/04—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/21—Manufacture essentially without removing material by casting
-
- 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
- F05D2240/00—Components
- F05D2240/10—Stators
- F05D2240/12—Fluid guiding means, e.g. vanes
- F05D2240/128—Nozzles
-
- 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
- F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs
-
- 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)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US85996 | 2002-02-28 | ||
US10/085,996 US6602047B1 (en) | 2002-02-28 | 2002-02-28 | Methods and apparatus for cooling gas turbine nozzles |
Publications (2)
Publication Number | Publication Date |
---|---|
DE60306825D1 true DE60306825D1 (de) | 2006-08-31 |
DE60306825T2 DE60306825T2 (de) | 2007-02-22 |
Family
ID=27622825
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE60306825T Expired - Lifetime DE60306825T2 (de) | 2002-02-28 | 2003-02-26 | Verfahren und Vorrichtung für die Kühlung von Gasturbinenleitschaufeln |
Country Status (5)
Country | Link |
---|---|
US (1) | US6602047B1 (de) |
EP (1) | EP1340884B1 (de) |
JP (1) | JP4416417B2 (de) |
CN (1) | CN100357567C (de) |
DE (1) | DE60306825T2 (de) |
Families Citing this family (45)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US6969230B2 (en) * | 2002-12-17 | 2005-11-29 | General Electric Company | Venturi outlet turbine airfoil |
US6824352B1 (en) * | 2003-09-29 | 2004-11-30 | Power Systems Mfg, Llc | Vane enhanced trailing edge cooling design |
US6984102B2 (en) * | 2003-11-19 | 2006-01-10 | General Electric Company | Hot gas path component with mesh and turbulated cooling |
US20060042932A1 (en) * | 2004-08-25 | 2006-03-02 | Rosenzweig Mark A | Apparatus and method for electroplating a workpiece |
US7775053B2 (en) * | 2004-09-20 | 2010-08-17 | United Technologies Corporation | Heat transfer augmentation in a compact heat exchanger pedestal array |
US7246999B2 (en) * | 2004-10-06 | 2007-07-24 | General Electric Company | Stepped outlet turbine airfoil |
US7156620B2 (en) * | 2004-12-21 | 2007-01-02 | Pratt & Whitney Canada Corp. | Internally cooled gas turbine airfoil and method |
US7156619B2 (en) * | 2004-12-21 | 2007-01-02 | Pratt & Whitney Canada Corp. | Internally cooled gas turbine airfoil and method |
US7575414B2 (en) | 2005-04-01 | 2009-08-18 | General Electric Company | Turbine nozzle with trailing edge convection and film cooling |
US7377743B2 (en) * | 2005-12-19 | 2008-05-27 | General Electric Company | Countercooled turbine nozzle |
JP4957131B2 (ja) * | 2006-09-06 | 2012-06-20 | 株式会社Ihi | 冷却構造 |
ATE447662T1 (de) * | 2007-01-18 | 2009-11-15 | Siemens Ag | Leitschaufel für eine gasturbine |
US20090067978A1 (en) * | 2007-05-24 | 2009-03-12 | Suljak Jr George T | Variable area turbine vane arrangement |
US7934906B2 (en) * | 2007-11-14 | 2011-05-03 | Siemens Energy, Inc. | Turbine blade tip cooling system |
WO2009121715A1 (de) * | 2008-03-31 | 2009-10-08 | Alstom Technology Ltd | Kühlkanalanordnung innerhalb eines hohlgegossenen gussteils |
FR2933884B1 (fr) * | 2008-07-16 | 2012-07-27 | Snecma | Procede de fabrication d'une piece d'aubage. |
CH700321A1 (de) * | 2009-01-30 | 2010-07-30 | Alstom Technology Ltd | Gekühlte schaufel für eine gasturbine. |
US8167560B2 (en) | 2009-03-03 | 2012-05-01 | Siemens Energy, Inc. | Turbine airfoil with an internal cooling system having enhanced vortex forming turbulators |
US8348613B2 (en) * | 2009-03-30 | 2013-01-08 | United Technologies Corporation | Airflow influencing airfoil feature array |
EP2378073A1 (de) | 2010-04-14 | 2011-10-19 | Siemens Aktiengesellschaft | Lauf- oder Leitschaufel für eine Turbomaschine |
EP2397653A1 (de) | 2010-06-17 | 2011-12-21 | Siemens Aktiengesellschaft | Plattformsegment zur Stützung einer Gasturbinenleitschaufel und Kühlungsverfahren |
DE102010036316B4 (de) * | 2010-07-09 | 2015-06-11 | Saint-Gobain Diamantwerkzeuge Gmbh | Düse für Kühlschmiermittel |
US8882461B2 (en) | 2011-09-12 | 2014-11-11 | Honeywell International Inc. | Gas turbine engines with improved trailing edge cooling arrangements |
US8790084B2 (en) | 2011-10-31 | 2014-07-29 | General Electric Company | Airfoil and method of fabricating the same |
ITMI20120010A1 (it) * | 2012-01-05 | 2013-07-06 | Gen Electric | Profilo aerodinamico di turbina a fessura |
EP2682565B8 (de) | 2012-07-02 | 2016-09-21 | General Electric Technology GmbH | Gekühlte Schaufel für eine Gasturbine |
US9759072B2 (en) | 2012-08-30 | 2017-09-12 | United Technologies Corporation | Gas turbine engine airfoil cooling circuit arrangement |
US9458725B2 (en) | 2013-10-04 | 2016-10-04 | General Electric Company | Method and system for providing cooling for turbine components |
US20150322797A1 (en) * | 2014-05-09 | 2015-11-12 | United Technologies Corporation | Blade element cross-ties |
JP2018512536A (ja) * | 2015-03-17 | 2018-05-17 | シーメンス エナジー インコーポレイテッド | タービンエンジン内の翼のための後縁冷却チャネルにおいて収束・拡開出口スロットを備える内部冷却システム |
US9957900B2 (en) * | 2015-05-11 | 2018-05-01 | General Electric Company | System and method for flow control in turbine |
GB201514793D0 (en) * | 2015-08-20 | 2015-10-07 | Rolls Royce Plc | Cooling of turbine blades and method for turbine blade manufacture |
US20170107827A1 (en) * | 2015-10-15 | 2017-04-20 | General Electric Company | Turbine blade |
US10443398B2 (en) * | 2015-10-15 | 2019-10-15 | General Electric Company | Turbine blade |
US11248472B2 (en) * | 2015-10-30 | 2022-02-15 | Siemens Energy Global GmbH & Co. KG | Turbine airfoil with trailing edge cooling featuring axial partition walls |
JP6685425B2 (ja) * | 2016-03-22 | 2020-04-22 | シーメンス アクチエンゲゼルシヤフトSiemens Aktiengesellschaft | 後縁骨組み特徴を備えるタービン翼 |
US10156146B2 (en) * | 2016-04-25 | 2018-12-18 | General Electric Company | Airfoil with variable slot decoupling |
RU2627490C1 (ru) * | 2016-11-15 | 2017-08-08 | Ильдар Хайдарович Бадамшин | Способ повышения ресурса газотурбинного двигателя по числу запусков |
US10612390B2 (en) | 2017-01-26 | 2020-04-07 | United Technologies Corporation | Trailing edge pressure and flow regulator |
EP3645838B1 (de) | 2017-06-30 | 2022-06-01 | Siemens Energy Global GmbH & Co. KG | Turbinenschaufel mit hinterkantenmerkmalen und gusskern |
US10830072B2 (en) * | 2017-07-24 | 2020-11-10 | General Electric Company | Turbomachine airfoil |
EP3492702A1 (de) * | 2017-11-29 | 2019-06-05 | Siemens Aktiengesellschaft | Innengekühlte turbomaschinenkomponente |
US10787932B2 (en) * | 2018-07-13 | 2020-09-29 | Honeywell International Inc. | Turbine blade with dust tolerant cooling system |
US11352902B2 (en) * | 2020-08-27 | 2022-06-07 | Aytheon Technologies Corporation | Cooling arrangement including alternating pedestals for gas turbine engine components |
KR102488973B1 (ko) * | 2021-01-11 | 2023-01-13 | 두산에너빌리티 주식회사 | 터빈용 에어포일 및 이를 포함하는 터빈 |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2476207A1 (fr) * | 1980-02-19 | 1981-08-21 | Snecma | Perfectionnement aux aubes de turbines refroidies |
US4514144A (en) * | 1983-06-20 | 1985-04-30 | General Electric Company | Angled turbulence promoter |
US4515523A (en) * | 1983-10-28 | 1985-05-07 | Westinghouse Electric Corp. | Cooling arrangement for airfoil stator vane trailing edge |
JPS6285102A (ja) * | 1985-10-11 | 1987-04-18 | Hitachi Ltd | ガスタ−ビン冷却翼 |
US4726104A (en) | 1986-11-20 | 1988-02-23 | United Technologies Corporation | Methods for weld repairing hollow, air cooled turbine blades and vanes |
GB2242941B (en) * | 1990-04-11 | 1994-05-04 | Rolls Royce Plc | A cooled gas turbine engine aerofoil |
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 |
US5772397A (en) * | 1996-05-08 | 1998-06-30 | Alliedsignal Inc. | Gas turbine airfoil with aft internal cooling |
US6241466B1 (en) * | 1999-06-01 | 2001-06-05 | General Electric Company | Turbine airfoil breakout cooling |
US6174135B1 (en) | 1999-06-30 | 2001-01-16 | General Electric Company | Turbine blade trailing edge cooling openings and slots |
US6270317B1 (en) * | 1999-12-18 | 2001-08-07 | General Electric Company | Turbine nozzle with sloped film cooling |
DE19963349A1 (de) * | 1999-12-27 | 2001-06-28 | Abb Alstom Power Ch Ag | Schaufel für Gasturbinen mit Drosselquerschnitt an Hinterkante |
US6428273B1 (en) * | 2001-01-05 | 2002-08-06 | General Electric Company | Truncated rib turbine nozzle |
-
2002
- 2002-02-28 US US10/085,996 patent/US6602047B1/en not_active Expired - Lifetime
-
2003
- 2003-02-26 DE DE60306825T patent/DE60306825T2/de not_active Expired - Lifetime
- 2003-02-26 EP EP03251180A patent/EP1340884B1/de not_active Expired - Fee Related
- 2003-02-28 CN CNB031067514A patent/CN100357567C/zh not_active Expired - Lifetime
- 2003-02-28 JP JP2003052193A patent/JP4416417B2/ja not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN1441148A (zh) | 2003-09-10 |
EP1340884B1 (de) | 2006-07-19 |
CN100357567C (zh) | 2007-12-26 |
US6602047B1 (en) | 2003-08-05 |
JP4416417B2 (ja) | 2010-02-17 |
EP1340884A2 (de) | 2003-09-03 |
JP2003278503A (ja) | 2003-10-02 |
EP1340884A3 (de) | 2004-06-09 |
DE60306825T2 (de) | 2007-02-22 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition |