DE602008004863D1 - Verriegelungsorgan von Ringsektoren an einem Turbinengehäuse, das Greifmitteln umfasst - Google Patents

Verriegelungsorgan von Ringsektoren an einem Turbinengehäuse, das Greifmitteln umfasst

Info

Publication number
DE602008004863D1
DE602008004863D1 DE602008004863T DE602008004863T DE602008004863D1 DE 602008004863 D1 DE602008004863 D1 DE 602008004863D1 DE 602008004863 T DE602008004863 T DE 602008004863T DE 602008004863 T DE602008004863 T DE 602008004863T DE 602008004863 D1 DE602008004863 D1 DE 602008004863D1
Authority
DE
Germany
Prior art keywords
locking member
gripping means
turbine housing
ring sectors
sectors
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
DE602008004863T
Other languages
English (en)
Inventor
David Audeon
Kamel Benderradji
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 DE602008004863D1 publication Critical patent/DE602008004863D1/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
    • F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
    • F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
    • 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
    • F05D2240/10—Stators
    • F05D2240/11—Shroud seal segments
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Clamps And Clips (AREA)
DE602008004863T 2007-09-24 2008-09-22 Verriegelungsorgan von Ringsektoren an einem Turbinengehäuse, das Greifmitteln umfasst Active DE602008004863D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0757801A FR2921410B1 (fr) 2007-09-24 2007-09-24 Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des moyens permettant sa prehension

Publications (1)

Publication Number Publication Date
DE602008004863D1 true DE602008004863D1 (de) 2011-03-24

Family

ID=39427592

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602008004863T Active DE602008004863D1 (de) 2007-09-24 2008-09-22 Verriegelungsorgan von Ringsektoren an einem Turbinengehäuse, das Greifmitteln umfasst

Country Status (7)

Country Link
US (1) US8038393B2 (de)
EP (1) EP2039885B1 (de)
CA (1) CA2639762C (de)
DE (1) DE602008004863D1 (de)
ES (1) ES2359951T3 (de)
FR (1) FR2921410B1 (de)
RU (1) RU2511821C2 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0807137D0 (en) * 2008-04-21 2008-05-21 Rolls Royce Plc Rear fan case for a gas turbine engine
FR2931196B1 (fr) * 2008-05-16 2010-06-18 Snecma Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages radiaux permettant sa prehension
FR2931197B1 (fr) * 2008-05-16 2010-06-18 Snecma Organe de verrouillage de secteurs d'anneau sur un carter de turbomachine, comprenant des passages axiaux pour sa prehension
GB2467747B (en) * 2009-02-12 2012-05-02 Vector Int Ltd Clamp
WO2014200571A2 (en) 2013-02-19 2014-12-18 United Technologies Corporation Composite attachment structure with 3d weave
FR3009740B1 (fr) 2013-08-13 2017-12-15 Snecma Amelioration pour le verrouillage de pieces de support d'aubage
EP2846001B1 (de) * 2013-09-06 2023-01-11 MTU Aero Engines AG Montage- und Demontageverfahren eines Gasturbinenrotors und zugehörige Werkzeug
FR3019210B1 (fr) 2014-04-01 2016-05-13 Snecma Partie de turbomachine comportant une bride avec un dispositif de drainage

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5197853A (en) * 1991-08-28 1993-03-30 General Electric Company Airtight shroud support rail and method for assembling in turbine engine
FR2780443B1 (fr) * 1998-06-25 2000-08-04 Snecma Anneau de stator de turbine haute pression d'une turbomachine
FR2800797B1 (fr) * 1999-11-10 2001-12-07 Snecma Assemblage d'un anneau bordant une turbine a la structure de turbine
FR2819010B1 (fr) * 2001-01-04 2004-05-28 Snecma Moteurs Secteur d'entretoise de support d'anneau de stator de la turbine haute pression d'une turbomachine avec rattrapage de jeux
FR2865237B1 (fr) * 2004-01-16 2006-03-10 Snecma Moteurs Perfectionnements apportes aux dispositifs de controle de jeu dans une turbine a gaz
FR2867224B1 (fr) * 2004-03-04 2006-05-19 Snecma Moteurs Dispositif de maintien axial de secteur d'entretoise pour anneau d'une turbine haute-pression de turbomachine
FR2887920B1 (fr) * 2005-06-29 2010-09-10 Snecma Dispositif de fixation de secteurs d'anneau sur un carter de turbine
FR2899275A1 (fr) * 2006-03-30 2007-10-05 Snecma Sa Dispositif de fixation de secteurs d'anneau sur un carter de turbine d'une turbomachine
FR2913050B1 (fr) * 2007-02-28 2011-06-17 Snecma Turbine haute-pression d'une turbomachine
FR2931872B1 (fr) * 2008-05-28 2010-08-20 Snecma Turbine haute pression d'une turbomachine avec montage ameliore du boitier de pilotage des jeux radiaux d'aubes mobiles.
FR2935777B1 (fr) * 2008-09-09 2013-03-08 Snecma Chambre de combustion de turbomachine

Also Published As

Publication number Publication date
RU2511821C2 (ru) 2014-04-10
FR2921410A1 (fr) 2009-03-27
US8038393B2 (en) 2011-10-18
US20090081037A1 (en) 2009-03-26
EP2039885B1 (de) 2011-02-09
FR2921410B1 (fr) 2010-03-12
CA2639762A1 (en) 2009-03-24
RU2008138054A (ru) 2010-03-27
EP2039885A1 (de) 2009-03-25
CA2639762C (en) 2015-11-24
ES2359951T3 (es) 2011-05-30

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