DE602005000290D1 - Hochdruckturbinenstator einer Strömungsmaschine und deren Zusammenbauverfahren - Google Patents

Hochdruckturbinenstator einer Strömungsmaschine und deren Zusammenbauverfahren

Info

Publication number
DE602005000290D1
DE602005000290D1 DE602005000290T DE602005000290T DE602005000290D1 DE 602005000290 D1 DE602005000290 D1 DE 602005000290D1 DE 602005000290 T DE602005000290 T DE 602005000290T DE 602005000290 T DE602005000290 T DE 602005000290T DE 602005000290 D1 DE602005000290 D1 DE 602005000290D1
Authority
DE
Germany
Prior art keywords
turbomachine
pressure turbine
assembly method
turbine stator
stator
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.)
Active
Application number
DE602005000290T
Other languages
English (en)
Other versions
DE602005000290T2 (de
Inventor
Anne-Marie Arraitz
Thierry Fachat
Jerome Friedel
Alain Gendraud
Delphine Roussin
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Publication of DE602005000290D1 publication Critical patent/DE602005000290D1/de
Application granted granted Critical
Publication of DE602005000290T2 publication Critical patent/DE602005000290T2/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • F01D9/042—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector fixing blades to stators
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/246—Fastening of diaphragms or stator-rings
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F01D25/26—Double casings; Measures against temperature strain in casings
    • 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
    • F05D2260/209—Heat transfer, e.g. cooling using vortex tubes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
DE602005000290T 2004-03-18 2005-02-14 Hochdruckturbinenstator einer Strömungsmaschine und deren Zusammenbauverfahren Active DE602005000290T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0402825 2004-03-18
FR0402825A FR2867805A1 (fr) 2004-03-18 2004-03-18 Stator de turbine haute-pression de turbomachine et procede d'assemblage

Publications (2)

Publication Number Publication Date
DE602005000290D1 true DE602005000290D1 (de) 2007-01-11
DE602005000290T2 DE602005000290T2 (de) 2007-06-21

Family

ID=34834195

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005000290T Active DE602005000290T2 (de) 2004-03-18 2005-02-14 Hochdruckturbinenstator einer Strömungsmaschine und deren Zusammenbauverfahren

Country Status (9)

Country Link
US (1) US7360987B2 (de)
EP (1) EP1577501B1 (de)
JP (1) JP4526420B2 (de)
CA (1) CA2500493C (de)
DE (1) DE602005000290T2 (de)
ES (1) ES2273318T3 (de)
FR (1) FR2867805A1 (de)
RU (1) RU2374459C2 (de)
UA (1) UA87968C2 (de)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8047763B2 (en) * 2008-10-30 2011-11-01 General Electric Company Asymmetrical gas turbine cooling port locations
DE102009031009A1 (de) * 2009-06-29 2010-12-30 Osram Opto Semiconductors Gmbh Strahlungsemittierendes Bauelement
DE102015215144B4 (de) 2015-08-07 2017-11-09 MTU Aero Engines AG Vorrichtung und Verfahren zum Beeinflussen der Temperaturen in Innenringsegmenten einer Gasturbine
US10443616B2 (en) * 2016-03-16 2019-10-15 United Technologies Corporation Blade outer air seal with centrally mounted seal arc segments

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3146992A (en) * 1962-12-10 1964-09-01 Gen Electric Turbine shroud support structure
US5100291A (en) * 1990-03-28 1992-03-31 General Electric Company Impingement manifold
US5281085A (en) * 1990-12-21 1994-01-25 General Electric Company Clearance control system for separately expanding or contracting individual portions of an annular shroud
US5205115A (en) * 1991-11-04 1993-04-27 General Electric Company Gas turbine engine case counterflow thermal control
US5219268A (en) * 1992-03-06 1993-06-15 General Electric Company Gas turbine engine case thermal control flange
FR2766232B1 (fr) * 1997-07-18 1999-08-20 Snecma Dispositif de refroidissement ou d'echauffement d'un carter circulaire
FR2766231B1 (fr) * 1997-07-18 1999-08-20 Snecma Dispositif d'echauffement ou de refroidissement d'un carter circulaire
FR2816352B1 (fr) * 2000-11-09 2003-01-31 Snecma Moteurs Ensemble de ventilation d'un anneau de stator
US6454529B1 (en) * 2001-03-23 2002-09-24 General Electric Company Methods and apparatus for maintaining rotor assembly tip clearances
GB2388407B (en) * 2002-05-10 2005-10-26 Rolls Royce Plc Gas turbine blade tip clearance control structure

Also Published As

Publication number Publication date
CA2500493A1 (fr) 2005-09-18
JP2005264935A (ja) 2005-09-29
EP1577501B1 (de) 2006-11-29
ES2273318T3 (es) 2007-05-01
UA87968C2 (ru) 2009-09-10
DE602005000290T2 (de) 2007-06-21
JP4526420B2 (ja) 2010-08-18
CA2500493C (fr) 2012-01-10
RU2374459C2 (ru) 2009-11-27
RU2005106888A (ru) 2006-08-20
US20050238477A1 (en) 2005-10-27
FR2867805A1 (fr) 2005-09-23
EP1577501A1 (de) 2005-09-21
US7360987B2 (en) 2008-04-22

Similar Documents

Publication Publication Date Title
DE602006011409D1 (de) Gasturbinentriebwerksanordnung und Verfahren zu deren Zusammenbau
DE602005004353D1 (de) Gasturbine und Verfahren zu deren Montage
DE602004002049D1 (de) Niederdruck-Turbine einer Turbomaschine
DE60314032D1 (de) Mantelringsegment, Herstellungsverfahren eines Mantelringsegments, sowie Mantelringanordnung für ein Turbinentriebwerk
DE602005000026D1 (de) Dichtungsanordnung für die Hochdruckturbine einer Turbomaschine
DE602005026619D1 (de) Verfahren zur Herstellung einer reparierten Leitschaufelanordnung einer Turbomaschine und reparierte Anordnung
DE60221628D1 (de) Turbinenleitschaufel einer Gasturbine und deren Herstellungsmethode
ITMI20061784A1 (it) Guarnizioni per turbine e macchinario di turbine
DE60302990D1 (de) Diagnostisches Verfahren der Leistung einer Gasturbine
DE602005025427D1 (de) Verstellbare Leitschaufelanordnung einer Gasturbine
DE602005021428D1 (de) Turbinentriebwerk und Montageverfahren für ein Turbinentriebwerk
NO20051741D0 (no) Stator med hoy virkningsgrad for den forste fase i en gassturbin
DK1979612T3 (da) Vindturbinesamling og relateret fremgangsmåde
DE60332196D1 (de) Kühlstruktur einer Turbinenleitschaufel und Gasturbine
DE602004031424D1 (de) Segment eines mantelrings einer turbine
DK1779997T4 (da) Fremgangsmåde til fremstilling af en vindmøllerotorvinge
DE602005027512D1 (de) Betriebsverfahren für ein Gasturbinenkraftwerk und zugehöriges Gasturbinenkraftwerk
NO20054322D0 (no) Rotorblad for forste trinn i en gassturbin
ATE291172T1 (de) Windenergieanlage und verfahren zum betreiben einer windenergieanlage
DE602005007297D1 (de) Turbine eines Gasturbinentriebwerks
DE602005011977D1 (de) Mehrbereichsrohranordnung und montageverfahren für ein übergangsteil einer gasturbine
SG123728A1 (en) Turbine nozzle segment and method of repairing same
DE112005002547A5 (de) Optimierte Turbinenstufe einer Turbinenanlage sowie Auslegungsverfahren
DE602006020567D1 (de) Rotor für dampfturbine und verfahren zu dessen herstellung
DE602004025887D1 (de) Rotorschaufel und Gasturbinentriebwerk mit einer entsprechenden Rotoranordnung

Legal Events

Date Code Title Description
8364 No opposition during term of opposition