FR2654463B1 - - Google Patents

Info

Publication number
FR2654463B1
FR2654463B1 FR8914963A FR8914963A FR2654463B1 FR 2654463 B1 FR2654463 B1 FR 2654463B1 FR 8914963 A FR8914963 A FR 8914963A FR 8914963 A FR8914963 A FR 8914963A FR 2654463 B1 FR2654463 B1 FR 2654463B1
Authority
FR
France
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.)
Expired - Fee Related
Application number
FR8914963A
Other languages
French (fr)
Other versions
FR2654463A1 (fr
Inventor
Ollivier Carletti
Elie Armand Jean Marie Thomas Michel
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
Priority to FR8914963A priority Critical patent/FR2654463A1/fr
Priority to US07/607,696 priority patent/US5083900A/en
Priority to EP90403218A priority patent/EP0433111B1/fr
Priority to DE90403218T priority patent/DE69002313T2/de
Publication of FR2654463A1 publication Critical patent/FR2654463A1/fr
Application granted granted Critical
Publication of FR2654463B1 publication Critical patent/FR2654463B1/fr
Granted 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
    • 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
    • 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)
FR8914963A 1989-11-15 1989-11-15 Element de stator de turbomachine. Granted FR2654463A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR8914963A FR2654463A1 (fr) 1989-11-15 1989-11-15 Element de stator de turbomachine.
US07/607,696 US5083900A (en) 1989-11-15 1990-11-01 Turbomachine stator element
EP90403218A EP0433111B1 (fr) 1989-11-15 1990-11-14 Elément de stator de turbomachine
DE90403218T DE69002313T2 (de) 1989-11-15 1990-11-14 Statorelement einer Turbomaschine.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8914963A FR2654463A1 (fr) 1989-11-15 1989-11-15 Element de stator de turbomachine.

Publications (2)

Publication Number Publication Date
FR2654463A1 FR2654463A1 (fr) 1991-05-17
FR2654463B1 true FR2654463B1 (enExample) 1994-04-22

Family

ID=9387411

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8914963A Granted FR2654463A1 (fr) 1989-11-15 1989-11-15 Element de stator de turbomachine.

Country Status (4)

Country Link
US (1) US5083900A (enExample)
EP (1) EP0433111B1 (enExample)
DE (1) DE69002313T2 (enExample)
FR (1) FR2654463A1 (enExample)

Families Citing this family (44)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5226789A (en) * 1991-05-13 1993-07-13 General Electric Company Composite fan stator assembly
US5290143A (en) * 1992-11-02 1994-03-01 Allied Signal Bicast vane and shroud rings
FR2702242B1 (fr) * 1993-03-03 1995-04-07 Snecma Etage d'aubes libres à une extrémité.
US5421703A (en) * 1994-05-25 1995-06-06 General Electric Company Positively retained vane bushing for an axial flow compressor
US5690469A (en) * 1996-06-06 1997-11-25 United Technologies Corporation Method and apparatus for replacing a vane assembly in a turbine engine
US6450766B1 (en) * 1999-08-09 2002-09-17 United Technologies Corporation Stator vane blank and method of forming the vane blank
US6619917B2 (en) 2000-12-19 2003-09-16 United Technologies Corporation Machined fan exit guide vane attachment pockets for use in a gas turbine
FR2819026B1 (fr) * 2001-01-04 2003-02-28 Snecma Moteurs Stator de compresseur axial de turbine a gaz
FR2856749B1 (fr) * 2003-06-30 2005-09-23 Snecma Moteurs Redresseur de compresseur de moteur aeronautique a aubes collees
US7530782B2 (en) * 2005-09-12 2009-05-12 Pratt & Whitney Canada Corp. Foreign object damage resistant vane assembly
US7413400B2 (en) 2005-09-12 2008-08-19 Pratt & Whitney Canada Corp. Vane assembly with grommet
US7510372B2 (en) * 2006-04-19 2009-03-31 United Technologies Corporation Wedge repair of mechanically retained vanes
AT503840B1 (de) * 2006-06-30 2010-09-15 Facc Ag Leitschaufelanordnung für ein triebwerk
CN100552235C (zh) * 2006-07-01 2009-10-21 五龙控股有限公司 导流环加强型环型冷却风扇
US7665963B2 (en) * 2006-09-06 2010-02-23 United Technologies Corporation Curved variable pitch wedge retention in vane outer base
US7614848B2 (en) * 2006-10-10 2009-11-10 United Technologies Corporation Fan exit guide vane repair method and apparatus
US7980813B2 (en) * 2007-08-13 2011-07-19 United Technologies Corporation Fan outlet guide vane shroud insert repair
EP2075415B1 (fr) * 2007-12-27 2016-10-19 Techspace Aero Structure annulaire de stator allégée pour turbomoteur d'aéronef
EP2199544B1 (fr) * 2008-12-22 2016-03-30 Techspace Aero S.A. Architecture de redresseur
US8206100B2 (en) * 2008-12-31 2012-06-26 General Electric Company Stator assembly for a gas turbine engine
GB0905729D0 (en) * 2009-04-03 2009-05-20 Rolls Royce Plc Stator vane assembly
EP2339120B1 (fr) * 2009-12-22 2015-07-08 Techspace Aero S.A. Étage redresseur de turbomachine et compresseur associé
US8454303B2 (en) * 2010-01-14 2013-06-04 General Electric Company Turbine nozzle assembly
EP2431571B1 (fr) * 2010-09-16 2013-06-05 Techspace Aero S.A. Assemblage d'un aube et d'un support composite par scellage
US8920117B2 (en) * 2011-10-07 2014-12-30 Pratt & Whitney Canada Corp. Fabricated gas turbine duct
EP2805022B1 (en) * 2011-12-30 2018-11-07 Rolls-Royce Corporation Gas turbine bypass vane system, gas turbine engine and method for manufacturing a bypass vane stage
EP2644828A1 (de) * 2012-03-29 2013-10-02 Siemens Aktiengesellschaft Modulare Turbinenschaufel mit Plattform
EP2644834A1 (de) * 2012-03-29 2013-10-02 Siemens Aktiengesellschaft Turbinenschaufel sowie zugehöriges Verfahren zum Herstellen einer Turbinenschaufel
FR2989130B1 (fr) * 2012-04-05 2014-03-28 Snecma Etage redresseur de compresseur pour une turbomachine
US11035238B2 (en) 2012-06-19 2021-06-15 Raytheon Technologies Corporation Airfoil including adhesively bonded shroud
US20130333350A1 (en) 2012-06-19 2013-12-19 Nicholas D. Stilin Airfoil including adhesively bonded shroud
US9341194B2 (en) 2012-11-01 2016-05-17 Solar Turbines Incorporated Gas turbine engine compressor with a biased inner ring
US20140212284A1 (en) * 2012-12-21 2014-07-31 General Electric Company Hybrid turbine nozzle
CA2903738A1 (en) * 2013-03-07 2014-09-12 Rolls-Royce Canada, Ltd. Gas turbine engine comprising an outboard insertion system of vanes and corresponding assembling method
GB201306123D0 (en) * 2013-04-05 2013-05-22 Rolls Royce Plc Vane assembly and method of making the same
US9840929B2 (en) * 2013-05-28 2017-12-12 Pratt & Whitney Canada Corp. Gas turbine engine vane assembly and method of mounting same
EP2966264B1 (fr) * 2014-07-07 2021-09-22 Safran Aero Boosters SA Caisson à aubes de redresseur de compresseur de turbomachine axiale
GB201412960D0 (en) * 2014-07-22 2014-09-03 Rolls Royce Plc Vane assembly
GB201414587D0 (en) * 2014-08-18 2014-10-01 Rolls Royce Plc Mounting Arrangement For Aerofoil Body
US10294807B2 (en) 2016-05-19 2019-05-21 Honeywell International Inc. Inter-turbine ducts
US10815804B2 (en) * 2017-04-04 2020-10-27 General Electric Company Turbine engine containment assembly and method for manufacturing the same
FR3073561B1 (fr) * 2017-11-10 2020-11-20 Safran Aircraft Engines Anneau d'aubes fixes d'un turboreacteur comprenant une structure de traitement acoustique
US11060411B2 (en) * 2019-03-22 2021-07-13 Pratt & Whitney Canada Corp. Inner shroud assembly for stator vanes
US11286798B2 (en) * 2019-08-20 2022-03-29 Rolls-Royce Corporation Airfoil assembly with ceramic matrix composite parts and load-transfer features

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE498667A (enExample) * 1949-08-27
GB722458A (en) * 1952-07-14 1955-01-26 Bristol Aeroplane Co Ltd Improvements in or relating to the manufacture of blades for use in axial flow compressors or the like
US2857093A (en) * 1954-12-02 1958-10-21 Cincinnati Testing & Res Lab Stator casing and blade assembly
US2914300A (en) * 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
US3339833A (en) * 1963-12-04 1967-09-05 Rolls Royce Axial fluid flow machine such as a compressor or turbine
GB995228A (en) * 1964-05-08 1965-06-16 Rolls Royce Bladed structure, for example, for a gas turbine engine compressor
US3442442A (en) * 1966-12-02 1969-05-06 Gen Electric Mounting of blades in an axial flow compressor
FR2073239A1 (enExample) * 1969-12-01 1971-10-01 Snecma
US3778185A (en) * 1972-08-28 1973-12-11 United Aircraft Corp Composite strut joint construction
US4378961A (en) * 1979-01-10 1983-04-05 United Technologies Corporation Case assembly for supporting stator vanes
US4594761A (en) * 1984-02-13 1986-06-17 General Electric Company Method of fabricating hollow composite airfoils
FR2568953B1 (fr) * 1984-08-08 1989-02-10 Ratier Figeac Soc Aube fixe pour reacteurs
FR2599081B1 (fr) * 1986-05-23 1988-07-29 Snecma Redresseur de soufflante de turboreacteur multiflux
FR2610673B1 (fr) * 1987-02-05 1991-03-15 Snecma Turboreacteur multiflux a couronne externe de redresseur de soufflante frettee sur le carter

Also Published As

Publication number Publication date
EP0433111A1 (fr) 1991-06-19
FR2654463A1 (fr) 1991-05-17
US5083900A (en) 1992-01-28
DE69002313T2 (de) 1993-12-02
EP0433111B1 (fr) 1993-07-21
DE69002313D1 (de) 1993-08-26

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Legal Events

Date Code Title Description
ST Notification of lapse