ATE526486T1 - Leitschaufel für eine gasturbine - Google Patents

Leitschaufel für eine gasturbine

Info

Publication number
ATE526486T1
ATE526486T1 AT09723174T AT09723174T ATE526486T1 AT E526486 T1 ATE526486 T1 AT E526486T1 AT 09723174 T AT09723174 T AT 09723174T AT 09723174 T AT09723174 T AT 09723174T AT E526486 T1 ATE526486 T1 AT E526486T1
Authority
AT
Austria
Prior art keywords
gas turbine
shroud
trailing edge
blade
stator blade
Prior art date
Application number
AT09723174T
Other languages
English (en)
Inventor
Erich Kreiselmaier
Jose Anguisola Mcfeat
Christoph Nagler
Sergei Riazantsev
Brian Kenneth Wardle
Original Assignee
Alstom Technology Ltd
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 Ltd filed Critical Alstom Technology Ltd
Application granted granted Critical
Publication of ATE526486T1 publication Critical patent/ATE526486T1/de

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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246Fastening of diaphragms or stator-rings
    • 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
    • F01D11/00Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/005Sealing means between non relatively rotating elements
    • 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
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/08Cooling; Heating; Heat-insulation
    • 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
    • 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
    • F05D2240/11Shroud seal segments
    • 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
    • F05D2240/80Platforms for stationary or moving blades
    • F05D2240/81Cooled platforms
    • 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
    • F05D2270/00Control
    • F05D2270/01Purpose of the control system
    • F05D2270/11Purpose of the control system to prolong engine life
    • F05D2270/114Purpose of the control system to prolong engine life by limiting mechanical stresses

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
AT09723174T 2008-03-19 2009-02-19 Leitschaufel für eine gasturbine ATE526486T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
CH4172008 2008-03-19
PCT/EP2009/051969 WO2009115390A1 (de) 2008-03-19 2009-02-19 Leitschaufel für eine gasturbine

Publications (1)

Publication Number Publication Date
ATE526486T1 true ATE526486T1 (de) 2011-10-15

Family

ID=39699716

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09723174T ATE526486T1 (de) 2008-03-19 2009-02-19 Leitschaufel für eine gasturbine

Country Status (5)

Country Link
US (1) US8142143B2 (de)
EP (1) EP2265799B1 (de)
AT (1) ATE526486T1 (de)
ES (1) ES2374148T3 (de)
WO (1) WO2009115390A1 (de)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8096757B2 (en) * 2009-01-02 2012-01-17 General Electric Company Methods and apparatus for reducing nozzle stress
FR3048015B1 (fr) 2016-02-19 2020-03-06 Safran Aircraft Engines Aube de turbomachine, comprenant un pied aux concentrations de contrainte reduites
CN112302729B (zh) * 2019-07-31 2022-10-11 中国航发商用航空发动机有限责任公司 航空发动机涡轮静子组件及航空发动机

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE755567A (fr) * 1969-12-01 1971-02-15 Gen Electric Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe
US4573865A (en) * 1981-08-31 1986-03-04 General Electric Company Multiple-impingement cooled structure
US4687413A (en) * 1985-07-31 1987-08-18 United Technologies Corporation Gas turbine engine assembly
US4820116A (en) * 1987-09-18 1989-04-11 United Technologies Corporation Turbine cooling for gas turbine engine
US5201846A (en) * 1991-11-29 1993-04-13 General Electric Company Low-pressure turbine heat shield
CH687269A5 (de) 1993-04-08 1996-10-31 Abb Management Ag Gasturbogruppe.
EP0844369B1 (de) 1996-11-23 2002-01-30 ROLLS-ROYCE plc Zusammenbau eines Schaufelrotors und dessen Gehäuses
JPH1150806A (ja) 1997-08-04 1999-02-23 Ishikawajima Harima Heavy Ind Co Ltd ガスタービンのノズル部材
US6761529B2 (en) 2002-07-25 2004-07-13 Mitshubishi Heavy Industries, Ltd. Cooling structure of stationary blade, and gas turbine
US7094029B2 (en) 2003-05-06 2006-08-22 General Electric Company Methods and apparatus for controlling gas turbine engine rotor tip clearances
US6951447B2 (en) * 2003-12-17 2005-10-04 United Technologies Corporation Turbine blade with trailing edge platform undercut
DE102004004014A1 (de) 2004-01-27 2005-08-18 Mtu Aero Engines Gmbh Leitschaufel für eine Turbomaschine
US7862300B2 (en) * 2006-05-18 2011-01-04 Wood Group Heavy Industrial Turbines Ag Turbomachinery blade having a platform relief hole

Also Published As

Publication number Publication date
WO2009115390A1 (de) 2009-09-24
US8142143B2 (en) 2012-03-27
ES2374148T3 (es) 2012-02-14
EP2265799B1 (de) 2011-09-28
US20110070089A1 (en) 2011-03-24
EP2265799A1 (de) 2010-12-29

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