WO2009083456A3 - Gasturbine - Google Patents
Gasturbine Download PDFInfo
- Publication number
- WO2009083456A3 WO2009083456A3 PCT/EP2008/067739 EP2008067739W WO2009083456A3 WO 2009083456 A3 WO2009083456 A3 WO 2009083456A3 EP 2008067739 W EP2008067739 W EP 2008067739W WO 2009083456 A3 WO2009083456 A3 WO 2009083456A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- cooling ports
- groups
- arrangement
- turbine
- cooling
- Prior art date
Links
- 238000001816 cooling Methods 0.000 abstract 7
- 238000002485 combustion reaction Methods 0.000 abstract 2
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
- F01D9/00—Stators
- F01D9/02—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
- F01D9/023—Transition ducts between combustor cans and first stage of the turbine in gas-turbine engines; their cooling or sealings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2240/00—Components
- F05B2240/80—Platforms for stationary or moving blades
- F05B2240/801—Platforms for stationary or moving blades cooled platforms
-
- 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
- F05D2240/80—Platforms for stationary or moving blades
- F05D2240/81—Cooled platforms
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Bei einer Gasturbine (10) leitet eine erste Mehrzahl von konzentrisch zur Drehachse in einer regulären Anordnung angeordneten Brennern (22a, b, c) jeweils durch einen zugehörigen Brennkammerauslass (11) Heissgas (12) in eine Turbine ein, an deren Eingang eine zweite Mehrzahl von Leitschaufeln (15; 15a, b, c, d) in einem Kranz um die Drehachse herum gleichmässig beabstandet angeordnet sind, wobei über den Umfang verteilt Kühlöffnungen vorgesehen sind, durch welche Kühlluft in den Heissgasstrom am Brennkammerauslass (11) eingedüst wird. Bei einer solchen Gasturbine wird eine Verbesserung der Strömungsverhältnisse im Heissgas, dadurch erreicht, dass die Kühlöffnungen in erste Kühlöffnungsgruppen (20a, b, c, d) und zweite Kühlöffnungsgruppen (21') aufgeteilt sind, dass die Anordnung der ersten Kühlöffnungsgruppen (20a, b, c, d) der Anordnung der Leitschaufeln (15; 15a, b, c, d) entspricht, und dass die Anordnung der zweiten Kühlöffnungsgruppen (21') der regulären Anordnung der Brenner (22a, b, c) entspricht.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP08868596.1A EP2229507B1 (de) | 2007-12-29 | 2008-12-17 | Gasturbine |
US12/824,630 US8783044B2 (en) | 2007-12-29 | 2010-06-28 | Turbine stator nozzle cooling structure |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH232008 | 2007-12-29 | ||
CH23/08 | 2007-12-29 |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US12/824,630 Continuation US8783044B2 (en) | 2007-12-29 | 2010-06-28 | Turbine stator nozzle cooling structure |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2009083456A2 WO2009083456A2 (de) | 2009-07-09 |
WO2009083456A3 true WO2009083456A3 (de) | 2009-09-17 |
Family
ID=39358154
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2008/067739 WO2009083456A2 (de) | 2007-12-29 | 2008-12-17 | Gasturbine |
Country Status (3)
Country | Link |
---|---|
US (1) | US8783044B2 (de) |
EP (1) | EP2229507B1 (de) |
WO (1) | WO2009083456A2 (de) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP2483529B1 (de) * | 2009-09-28 | 2013-08-28 | Siemens Aktiengesellschaft | Gasturbinendüsenanordnung und gasturbine |
CN102667068A (zh) * | 2009-12-30 | 2012-09-12 | 西门子公司 | 用于转换能量的涡轮机及其操作方法 |
EP2341217A1 (de) * | 2009-12-30 | 2011-07-06 | Siemens Aktiengesellschaft | Turbine zur Umwandlung von Energie und Verfahren zu ihrem Betrieb |
US10337404B2 (en) * | 2010-03-08 | 2019-07-02 | General Electric Company | Preferential cooling of gas turbine nozzles |
CH703105A1 (de) | 2010-05-05 | 2011-11-15 | Alstom Technology Ltd | Gasturbine mit einer sekundärbrennkammer. |
EP2754858B1 (de) * | 2013-01-14 | 2015-09-16 | Alstom Technology Ltd | Anordnung zum Abdichten eines offenen Hohlraums gegen Heißgaseinschluss |
JP6263365B2 (ja) | 2013-11-06 | 2018-01-17 | 三菱日立パワーシステムズ株式会社 | ガスタービン翼 |
EP3102808B1 (de) * | 2014-02-03 | 2020-05-06 | United Technologies Corporation | Gasturbine mit verbundrohr für kühlung |
US9752447B2 (en) * | 2014-04-04 | 2017-09-05 | United Technologies Corporation | Angled rail holes |
JP6546481B2 (ja) * | 2015-08-31 | 2019-07-17 | 川崎重工業株式会社 | 排気ディフューザ |
EP3141702A1 (de) * | 2015-09-14 | 2017-03-15 | Siemens Aktiengesellschaft | Gasturbinenleitschaufelsegment und verfahren zur herstellung |
DE102016217320A1 (de) * | 2016-09-12 | 2018-03-15 | Siemens Aktiengesellschaft | Gasturbine mit getrennter Kühlung für Turbine und Abgasgehäuse |
DE102019211418A1 (de) * | 2019-07-31 | 2021-02-04 | Siemens Aktiengesellschaft | Verfahren zur Modernisierung einer Gasturbinenanlage sowie Gasturbinenanlage |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1199541B (de) * | 1961-12-04 | 1965-08-26 | Jan Jerie Dr Ing | Sammler von Treibgasen fuer das Leitrad von Gasturbinen |
US4733538A (en) * | 1978-10-02 | 1988-03-29 | General Electric Company | Combustion selective temperature dilution |
EP0615055A1 (de) * | 1993-03-11 | 1994-09-14 | ROLLS-ROYCE plc | Leitschaufelkühlung |
EP0902164A1 (de) * | 1997-09-15 | 1999-03-17 | Asea Brown Boveri AG | Plattformkühlung für Gasturbinen |
DE19813779A1 (de) * | 1998-03-27 | 1999-09-30 | Bmw Rolls Royce Gmbh | Anordnung zur Kühlung der Plattformen von Leitschaufeln einer Gasturbine |
Family Cites Families (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1252470B (de) * | 1964-08-14 | 1967-10-19 | Bordes Joseph Szydlowski (Frankreich) | Ringförmige Brennkammer, insbesondere für Gasturbinentriebwerke |
US3608310A (en) * | 1966-06-27 | 1971-09-28 | Gen Motors Corp | Turbine stator-combustor structure |
GB1488481A (en) * | 1973-10-05 | 1977-10-12 | Rolls Royce | Gas turbine engines |
US3965066A (en) * | 1974-03-15 | 1976-06-22 | General Electric Company | Combustor-turbine nozzle interconnection |
GB1492049A (en) * | 1974-12-07 | 1977-11-16 | Rolls Royce | Combustion equipment for gas turbine engines |
US4012167A (en) * | 1975-10-14 | 1977-03-15 | United Technologies Corporation | Turbomachinery vane or blade with cooled platforms |
US4026659A (en) * | 1975-10-16 | 1977-05-31 | Avco Corporation | Cooled composite vanes for turbine nozzles |
US4126405A (en) * | 1976-12-16 | 1978-11-21 | General Electric Company | Turbine nozzle |
US4739621A (en) * | 1984-10-11 | 1988-04-26 | United Technologies Corporation | Cooling scheme for combustor vane interface |
US4821522A (en) * | 1987-07-02 | 1989-04-18 | United Technologies Corporation | Sealing and cooling arrangement for combustor vane interface |
CH674561A5 (de) | 1987-12-21 | 1990-06-15 | Bbc Brown Boveri & Cie | |
JPH03213602A (ja) * | 1990-01-08 | 1991-09-19 | General Electric Co <Ge> | ガスタービンエンジンの当接セグメントを連結する自己冷却式ジョイント連結構造 |
GB9305012D0 (en) * | 1993-03-11 | 1993-04-28 | Rolls Royce Plc | Sealing structures for gas turbine engines |
DE4435266A1 (de) | 1994-10-01 | 1996-04-04 | Abb Management Ag | Brenner |
JP4031590B2 (ja) | 1999-03-08 | 2008-01-09 | 三菱重工業株式会社 | 燃焼器の尾筒シール構造及びその構造を用いたガスタービン |
DE50109870D1 (de) * | 2001-03-26 | 2006-06-29 | Siemens Ag | Gasturbine |
FR2833035B1 (fr) * | 2001-12-05 | 2004-08-06 | Snecma Moteurs | Plate-forme d'aube de distributeur pour moteur a turbine a gaz |
US6758651B2 (en) * | 2002-10-16 | 2004-07-06 | Mitsubishi Heavy Industries, Ltd. | Gas turbine |
US7234304B2 (en) * | 2002-10-23 | 2007-06-26 | Pratt & Whitney Canada Corp | Aerodynamic trip to improve acoustic transmission loss and reduce noise level for gas turbine engine |
DE10336432A1 (de) | 2003-08-08 | 2005-03-10 | Alstom Technology Ltd Baden | Gasturbine und zugehöriges Kühlverfahren |
US7004720B2 (en) * | 2003-12-17 | 2006-02-28 | Pratt & Whitney Canada Corp. | Cooled turbine vane platform |
DE102004029696A1 (de) * | 2004-06-15 | 2006-01-05 | Rolls-Royce Deutschland Ltd & Co Kg | Plattformkühlanordnung für den Leitschaufelkranz einer Gasturbine |
US20060032233A1 (en) * | 2004-08-10 | 2006-02-16 | Zhang Luzeng J | Inlet film cooling of turbine end wall of a gas turbine engine |
US7806650B2 (en) * | 2006-08-29 | 2010-10-05 | General Electric Company | Method and apparatus for fabricating a nozzle segment for use with turbine engines |
US7857580B1 (en) * | 2006-09-15 | 2010-12-28 | Florida Turbine Technologies, Inc. | Turbine vane with end-wall leading edge cooling |
US8171634B2 (en) * | 2007-07-09 | 2012-05-08 | Pratt & Whitney Canada Corp. | Method of producing effusion holes |
-
2008
- 2008-12-17 WO PCT/EP2008/067739 patent/WO2009083456A2/de active Application Filing
- 2008-12-17 EP EP08868596.1A patent/EP2229507B1/de not_active Not-in-force
-
2010
- 2010-06-28 US US12/824,630 patent/US8783044B2/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1199541B (de) * | 1961-12-04 | 1965-08-26 | Jan Jerie Dr Ing | Sammler von Treibgasen fuer das Leitrad von Gasturbinen |
US4733538A (en) * | 1978-10-02 | 1988-03-29 | General Electric Company | Combustion selective temperature dilution |
EP0615055A1 (de) * | 1993-03-11 | 1994-09-14 | ROLLS-ROYCE plc | Leitschaufelkühlung |
EP0902164A1 (de) * | 1997-09-15 | 1999-03-17 | Asea Brown Boveri AG | Plattformkühlung für Gasturbinen |
DE19813779A1 (de) * | 1998-03-27 | 1999-09-30 | Bmw Rolls Royce Gmbh | Anordnung zur Kühlung der Plattformen von Leitschaufeln einer Gasturbine |
Also Published As
Publication number | Publication date |
---|---|
US8783044B2 (en) | 2014-07-22 |
US20100313571A1 (en) | 2010-12-16 |
WO2009083456A2 (de) | 2009-07-09 |
EP2229507A2 (de) | 2010-09-22 |
EP2229507B1 (de) | 2017-02-08 |
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