EP2075408A3 - Pale de stator de dernier étage d'une section basse pression de turbine à vapeur - Google Patents

Pale de stator de dernier étage d'une section basse pression de turbine à vapeur Download PDF

Info

Publication number
EP2075408A3
EP2075408A3 EP08173020A EP08173020A EP2075408A3 EP 2075408 A3 EP2075408 A3 EP 2075408A3 EP 08173020 A EP08173020 A EP 08173020A EP 08173020 A EP08173020 A EP 08173020A EP 2075408 A3 EP2075408 A3 EP 2075408A3
Authority
EP
European Patent Office
Prior art keywords
steam turbine
last stage
pressure section
stator blade
turbine low
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Withdrawn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
EP08173020A
Other languages
German (de)
English (en)
Other versions
EP2075408A2 (fr
Inventor
Nicola Camerlenghi
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.)
Ansaldo Energia SpA
Original Assignee
Ansaldo Energia SpA
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 Ansaldo Energia SpA filed Critical Ansaldo Energia SpA
Publication of EP2075408A2 publication Critical patent/EP2075408A2/fr
Publication of EP2075408A3 publication Critical patent/EP2075408A3/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/14Form or construction
    • F01D5/141Shape, i.e. outer, aerodynamic form
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D9/00Stators
    • F01D9/02Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles
    • F01D9/04Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector
    • F01D9/041Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2200/00Mathematical features
    • F05D2200/20Special functions
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/31Application in turbines in steam turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00Components
    • F05D2240/10Stators
    • F05D2240/12Fluid guiding means, e.g. vanes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
EP08173020A 2007-12-28 2008-12-29 Pale de stator de dernier étage d'une section basse pression de turbine à vapeur Withdrawn EP2075408A3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITMI20072441 ITMI20072441A1 (it) 2007-12-28 2007-12-28 Pala statorica di ultimo stadio di sezione di bassa pressione di una turbina a vapore

Publications (2)

Publication Number Publication Date
EP2075408A2 EP2075408A2 (fr) 2009-07-01
EP2075408A3 true EP2075408A3 (fr) 2013-03-06

Family

ID=40315667

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08173020A Withdrawn EP2075408A3 (fr) 2007-12-28 2008-12-29 Pale de stator de dernier étage d'une section basse pression de turbine à vapeur

Country Status (2)

Country Link
EP (1) EP2075408A3 (fr)
IT (1) ITMI20072441A1 (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12135007B2 (en) 2018-06-08 2024-11-05 Global Energy Co., Ltd. Horizontal shaft rotor

Families Citing this family (32)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8137062B2 (en) 2010-05-11 2012-03-20 General Electric Company Turbomachine nozzle
ITMI20101447A1 (it) * 2010-07-30 2012-01-30 Alstom Technology Ltd "turbina a vapore a bassa pressione e metodo per il funzionamento della stessa"
EP2434094A3 (fr) 2010-09-28 2018-02-21 Mitsubishi Hitachi Power Systems, Ltd. Aube statorique de turbine à vapeur et turbine à vapeur
KR101322554B1 (ko) * 2012-03-27 2013-10-28 가부시키가이샤 히타치세이사쿠쇼 증기 터빈의 고정익 및 그것을 사용한 증기 터빈
ITCO20120061A1 (it) * 2012-12-13 2014-06-14 Nuovo Pignone Srl Metodi per produrre pale di turbomacchina con canali sagomati mediante produzione additiva, pale di turbomacchina e turbomacchine
CN103541774B (zh) * 2013-11-14 2015-06-17 上海汽轮机厂有限公司 涡轮叶片设计方法
WO2015175052A2 (fr) 2014-02-19 2015-11-19 United Technologies Corporation Profil aérodynamique de turbine à gaz
EP3108112B1 (fr) * 2014-02-19 2023-10-11 Raytheon Technologies Corporation Moteur à double flux à engrenage avec aubes de compresseur basse pression
US9567858B2 (en) 2014-02-19 2017-02-14 United Technologies Corporation Gas turbine engine airfoil
US9140127B2 (en) 2014-02-19 2015-09-22 United Technologies Corporation Gas turbine engine airfoil
WO2015175044A2 (fr) 2014-02-19 2015-11-19 United Technologies Corporation Profil aérodynamique de moteur à turbine à gaz
EP3108120B1 (fr) 2014-02-19 2021-03-31 Raytheon Technologies Corporation Moteur à turbine à gaz ayant une architecture à engrenages et une structure à aube fixe spécifique
WO2015175043A2 (fr) 2014-02-19 2015-11-19 United Technologies Corporation Profil aérodynamique de moteur à turbine à gaz
US10465702B2 (en) 2014-02-19 2019-11-05 United Technologies Corporation Gas turbine engine airfoil
US10570916B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
WO2015175073A2 (fr) 2014-02-19 2015-11-19 United Technologies Corporation Surface portante de moteur à turbine à gaz
EP3108100B1 (fr) 2014-02-19 2021-04-14 Raytheon Technologies Corporation Pale de soufflante de moteur à turbine à gaz
EP3575551B1 (fr) 2014-02-19 2021-10-27 Raytheon Technologies Corporation Surface portante de moteur à turbine à gaz
EP3108103B1 (fr) 2014-02-19 2023-09-27 Raytheon Technologies Corporation Aube de soufflante pour moteur à turbine à gaz
US10570915B2 (en) 2014-02-19 2020-02-25 United Technologies Corporation Gas turbine engine airfoil
WO2015126941A1 (fr) 2014-02-19 2015-08-27 United Technologies Corporation Profil aérodynamique de moteur à turbine à gaz
US10584715B2 (en) 2014-02-19 2020-03-10 United Technologies Corporation Gas turbine engine airfoil
EP3108106B1 (fr) 2014-02-19 2022-05-04 Raytheon Technologies Corporation Pale de moteur à turbine à gaz
EP3985226B1 (fr) 2014-02-19 2024-12-25 RTX Corporation Profil d'aube pour moteur à turbine à gaz
EP3108105B1 (fr) 2014-02-19 2021-05-12 Raytheon Technologies Corporation Surface portante pour turbine à gaz
US10495106B2 (en) 2014-02-19 2019-12-03 United Technologies Corporation Gas turbine engine airfoil
WO2015126454A1 (fr) 2014-02-19 2015-08-27 United Technologies Corporation Surface portante de moteur à turbine à gaz
EP3108101B1 (fr) 2014-02-19 2022-04-20 Raytheon Technologies Corporation Profil aérodynamique de moteur à turbine à gaz
EP3108123B1 (fr) 2014-02-19 2023-10-04 Raytheon Technologies Corporation Moteur à double flux à engrenage avec aubes de compresseur basse pression
GB201707811D0 (en) * 2017-05-16 2017-06-28 Rolls Royce Plc Compressor aerofoil member
CN113250755B (zh) * 2021-04-15 2022-06-07 西北工业大学 基于非均匀有理b样条曲线的叶型的设计方法及叶片
DE102022103319A1 (de) 2022-02-11 2023-08-17 MTU Aero Engines AG Leitschaufel für eine Strömungsmaschine

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0916812A1 (fr) * 1997-11-17 1999-05-19 Asea Brown Boveri AG Etage final pour turbine axial
US20030086788A1 (en) * 2001-06-27 2003-05-08 Chandraker A. L. Three dimensional blade
WO2007011355A1 (fr) * 2005-07-19 2007-01-25 Honeywell International Inc. Turbocompresseur a buse variable
WO2007113149A1 (fr) * 2006-03-31 2007-10-11 Alstom Technology Ltd Aube directrice de turbomachine, notamment de turbine à vapeur

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0916812A1 (fr) * 1997-11-17 1999-05-19 Asea Brown Boveri AG Etage final pour turbine axial
US20030086788A1 (en) * 2001-06-27 2003-05-08 Chandraker A. L. Three dimensional blade
WO2007011355A1 (fr) * 2005-07-19 2007-01-25 Honeywell International Inc. Turbocompresseur a buse variable
WO2007113149A1 (fr) * 2006-03-31 2007-10-11 Alstom Technology Ltd Aube directrice de turbomachine, notamment de turbine à vapeur

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12135007B2 (en) 2018-06-08 2024-11-05 Global Energy Co., Ltd. Horizontal shaft rotor

Also Published As

Publication number Publication date
ITMI20072441A1 (it) 2009-06-29
EP2075408A2 (fr) 2009-07-01

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