WO2009083456A3 - Gasturbine - Google Patents

Gasturbine Download PDF

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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
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.)
Ceased
Application number
PCT/EP2008/067739
Other languages
English (en)
French (fr)
Other versions
WO2009083456A2 (de
Inventor
Ulrich Steiger
Jonas Hurter
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.)
GE Vernova GmbH
Original Assignee
Alstom Technology AG
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 Alstom Technology AG filed Critical Alstom Technology AG
Priority to EP08868596.1A priority Critical patent/EP2229507B1/de
Publication of WO2009083456A2 publication Critical patent/WO2009083456A2/de
Publication of WO2009083456A3 publication Critical patent/WO2009083456A3/de
Priority to US12/824,630 priority patent/US8783044B2/en
Anticipated expiration legal-status Critical
Ceased 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
    • F01D5/186—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.
PCT/EP2008/067739 2007-12-29 2008-12-17 Gasturbine Ceased WO2009083456A2 (de)

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 Ceased 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)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9790799B2 (en) 2013-11-06 2017-10-17 Mitsubishi Hitachi Power Systems, Ltd. Gas turbine airfoil

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2483529B1 (de) * 2009-09-28 2013-08-28 Siemens Aktiengesellschaft Gasturbinendüsenanordnung und gasturbine
US20120263572A1 (en) * 2009-12-30 2012-10-18 Andrew Shepherd Turbine for converting energy and method for operating the same
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
US10662792B2 (en) * 2014-02-03 2020-05-26 Raytheon Technologies Corporation Gas turbine engine cooling fluid composite tube
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)

* Cited by examiner, † Cited by third party
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

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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
EP1245804B1 (de) * 2001-03-26 2006-05-24 Siemens Aktiengesellschaft Gasturbine
FR2833035B1 (fr) * 2001-12-05 2004-08-06 Snecma Moteurs Plate-forme d'aube de distributeur pour moteur a turbine a gaz
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DE10336432A1 (de) * 2003-08-08 2005-03-10 Alstom Technology Ltd Baden Gasturbine und zugehöriges Kühlverfahren
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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
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Patent Citations (5)

* Cited by examiner, † Cited by third party
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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9790799B2 (en) 2013-11-06 2017-10-17 Mitsubishi Hitachi Power Systems, Ltd. Gas turbine airfoil

Also Published As

Publication number Publication date
US20100313571A1 (en) 2010-12-16
EP2229507A2 (de) 2010-09-22
EP2229507B1 (de) 2017-02-08
US8783044B2 (en) 2014-07-22
WO2009083456A2 (de) 2009-07-09

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