DE3880167D1 - In das gehaeuse eingepresster aussenring eines stators fuer den blaeser eines turbotriebwerks. - Google Patents

In das gehaeuse eingepresster aussenring eines stators fuer den blaeser eines turbotriebwerks.

Info

Publication number
DE3880167D1
DE3880167D1 DE8888400249T DE3880167T DE3880167D1 DE 3880167 D1 DE3880167 D1 DE 3880167D1 DE 8888400249 T DE8888400249 T DE 8888400249T DE 3880167 T DE3880167 T DE 3880167T DE 3880167 D1 DE3880167 D1 DE 3880167D1
Authority
DE
Germany
Prior art keywords
stator
blower
external ring
turbo engine
turbo
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.)
Expired - Fee Related
Application number
DE8888400249T
Other languages
English (en)
Other versions
DE3880167T2 (de
Inventor
Thierry Feuvrier
Alexandre Forestier
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
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Publication of DE3880167D1 publication Critical patent/DE3880167D1/de
Application granted granted Critical
Publication of DE3880167T2 publication Critical patent/DE3880167T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • F01D9/041—Nozzles; Nozzle boxes; Stator blades; Guide conduits, e.g. individual nozzles forming ring or sector using blades
    • 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
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/40—Casings; Connections of working fluid
    • F04D29/52—Casings; Connections of working fluid for axial pumps
    • F04D29/54—Fluid-guiding means, e.g. diffusers
    • F04D29/541—Specially adapted for elastic fluid pumps
    • F04D29/542—Bladed diffusers
    • 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)
DE8888400249T 1987-02-05 1988-02-03 In das gehaeuse eingepresster aussenring eines stators fuer den blaeser eines turbotriebwerks. Expired - Fee Related DE3880167T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8701394A FR2610673B1 (fr) 1987-02-05 1987-02-05 Turboreacteur multiflux a couronne externe de redresseur de soufflante frettee sur le carter

Publications (2)

Publication Number Publication Date
DE3880167D1 true DE3880167D1 (de) 1993-05-19
DE3880167T2 DE3880167T2 (de) 1993-08-26

Family

ID=9347611

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8888400249T Expired - Fee Related DE3880167T2 (de) 1987-02-05 1988-02-03 In das gehaeuse eingepresster aussenring eines stators fuer den blaeser eines turbotriebwerks.

Country Status (4)

Country Link
US (1) US4940386A (de)
EP (1) EP0277884B1 (de)
DE (1) DE3880167T2 (de)
FR (1) FR2610673B1 (de)

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US5226789A (en) * 1991-05-13 1993-07-13 General Electric Company Composite fan stator assembly
DE4117025A1 (de) * 1991-05-24 1992-11-26 Halberg Maschbau Gmbh & Co Drallregler fuer kreiselpumpen
FR2685383B1 (fr) * 1991-12-18 1994-02-11 Snecma Bras structural du carter d'une turbomachine.
US5474419A (en) * 1992-12-30 1995-12-12 Reluzco; George Flowpath assembly for a turbine diaphragm and methods of manufacture
JP3631271B2 (ja) * 1993-11-19 2005-03-23 ユナイテッド テクノロジーズ コーポレイション インナーシュラウド一体型ステータベーン構造
US5494404A (en) * 1993-12-22 1996-02-27 Alliedsignal Inc. Insertable stator vane assembly
US5411370A (en) * 1994-08-01 1995-05-02 United Technologies Corporation Vibration damping shroud for a turbomachine vane
GB9417406D0 (en) * 1994-08-30 1994-10-19 Gec Alsthom Ltd Turbine blade
US5797725A (en) * 1997-05-23 1998-08-25 Allison Advanced Development Company Gas turbine engine vane and method of manufacture
EP1111246B1 (de) * 1999-12-21 2003-08-13 Techspace Aero S.A. Steifes Ringteil
US6619917B2 (en) * 2000-12-19 2003-09-16 United Technologies Corporation Machined fan exit guide vane attachment pockets for use in a gas turbine
US6969239B2 (en) * 2002-09-30 2005-11-29 General Electric Company Apparatus and method for damping vibrations between a compressor stator vane and a casing of a gas turbine engine
US20070069477A1 (en) * 2003-06-20 2007-03-29 Elliott Company Stepped labyrinth damper seal
US20060267289A1 (en) * 2003-06-20 2006-11-30 Elliott Company Hybrid abradable labyrinth damper seal
FR2869360B1 (fr) * 2004-04-27 2006-07-14 Airbus France Sas Ensemble reducteur de bruit pour turboreacteur d'aeronef
US7052234B2 (en) * 2004-06-23 2006-05-30 General Electric Company Turbine vane collar seal
US8191254B2 (en) * 2004-09-23 2012-06-05 Carlton Forge Works Method and apparatus for improving fan case containment and heat resistance in a gas turbine jet engine
US7530782B2 (en) * 2005-09-12 2009-05-12 Pratt & Whitney Canada Corp. Foreign object damage resistant vane assembly
US7637718B2 (en) * 2005-09-12 2009-12-29 Pratt & Whitney Canada Corp. Vane assembly with outer grommets
US7628578B2 (en) * 2005-09-12 2009-12-08 Pratt & Whitney Canada Corp. Vane assembly with improved vane roots
US7413400B2 (en) * 2005-09-12 2008-08-19 Pratt & Whitney Canada Corp. Vane assembly with grommet
EP1801357B1 (de) * 2005-12-22 2010-10-27 Techspace Aero Schaufelleitring einer Strömungsmaschine, Strömungsmaschine mit einem solchen Leitring und Leitschaufel
US7614848B2 (en) * 2006-10-10 2009-11-10 United Technologies Corporation Fan exit guide vane repair method and apparatus
US8016543B2 (en) * 2007-04-02 2011-09-13 Michael Scott Braley Composite case armor for jet engine fan case containment
WO2009157817A1 (en) * 2008-06-26 2009-12-30 Volvo Aero Corporation Vane assembly and method of fabricating, and a turbo-machine with such vane assembly
EP2196629B1 (de) * 2008-12-11 2018-05-16 Safran Aero Boosters SA Segmentierter Verbundmantelring eines axialen Verdichters
GB0905729D0 (en) * 2009-04-03 2009-05-20 Rolls Royce Plc Stator vane assembly
US8672609B2 (en) 2009-08-31 2014-03-18 United Technologies Corporation Composite fan containment case assembly
US9114882B2 (en) 2010-10-26 2015-08-25 United Technologies Corporation Fan case and mount ring snap fit assembly
FR2952403B1 (fr) * 2009-11-12 2012-01-13 Snecma Structure annulaire metallique de raccord pour turbomachine d'aeronef
US8696311B2 (en) 2011-03-29 2014-04-15 Pratt & Whitney Canada Corp. Apparatus and method for gas turbine engine vane retention
US8998574B2 (en) 2011-09-01 2015-04-07 Pratt & Whitney Canada Corp. Spring-tensioned stator restraining strap
US9951639B2 (en) 2012-02-10 2018-04-24 Pratt & Whitney Canada Corp. Vane assemblies for gas turbine engines
US9169736B2 (en) * 2012-07-16 2015-10-27 United Technologies Corporation Joint between airfoil and shroud
US9546571B2 (en) * 2012-08-22 2017-01-17 United Technologies Corporation Mounting lug for connecting a vane to a turbine engine case
EP2735707B1 (de) * 2012-11-27 2017-04-05 Safran Aero Boosters SA Leitrad einer axialen Turbomaschine mit segmentiertem Innendeckband und zugehöriger Verdichter
US20140169979A1 (en) * 2012-12-14 2014-06-19 United Technologies Corporation Gas turbine engine fan blade platform seal
US9702252B2 (en) 2012-12-19 2017-07-11 Honeywell International Inc. Turbine nozzles with slip joints and methods for the production thereof
WO2014137468A1 (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
US9840929B2 (en) * 2013-05-28 2017-12-12 Pratt & Whitney Canada Corp. Gas turbine engine vane assembly and method of mounting same
FR3010154B1 (fr) * 2013-09-05 2015-10-02 Snecma Panneau d'etancheite de carter intermediaire de turbomachine d'aeronef a double flux
JP6221544B2 (ja) 2013-09-18 2017-11-01 株式会社Ihi ターボファンエンジンのためのシール
US10180145B2 (en) * 2013-11-07 2019-01-15 Asia Vital Components Co., Ltd. Fan salt-fog-resistant structure and fan frame thereof
EP2886802B1 (de) * 2013-12-20 2019-04-10 Safran Aero Boosters SA Innenringdichtung der letzten Kompressorstufe eines axialen Turbotriebwerks
JP2015135061A (ja) * 2014-01-16 2015-07-27 株式会社Ihi 翼の連結部構造及びこれを用いたジェットエンジン
FR3021690B1 (fr) * 2014-05-28 2016-07-29 Snecma Aube directrice de sortie comprenant au moins une plateforme surmoulee
US9290274B2 (en) 2014-06-02 2016-03-22 Mra Systems, Inc. Acoustically attenuating sandwich panel constructions
GB201412960D0 (en) * 2014-07-22 2014-09-03 Rolls Royce Plc Vane assembly
US10450878B2 (en) * 2016-07-06 2019-10-22 United Technologies Corporation Segmented stator assembly
US10801343B2 (en) * 2016-12-16 2020-10-13 Pratt & Whitney Canada Corp. Self retaining face seal design for by-pass stator vanes
US10815804B2 (en) * 2017-04-04 2020-10-27 General Electric Company Turbine engine containment assembly and method for manufacturing the same
FR3068742B1 (fr) * 2017-07-07 2021-09-10 Safran Aircraft Engines Aube de turbomachine comprenant une source electroacoustique a montage ameliore, rangee d'aubes directrices de sortie et turbomachine comprenant une telle aube
KR101919249B1 (ko) * 2017-09-15 2018-11-15 두산중공업 주식회사 가스 터빈
CN107725117B (zh) * 2017-09-15 2019-08-16 中国科学院工程热物理研究所 一种静子叶片安装结构
US10830074B2 (en) * 2018-07-03 2020-11-10 Raytheon Technologies Corporation Potted stator vane with metal fillet
FR3085435B1 (fr) * 2018-09-05 2021-06-18 Safran Aircraft Engines Turbomachine a double flux
US11066944B2 (en) * 2019-02-08 2021-07-20 Pratt & Whitney Canada Corp Compressor shroud with shroud segments
US11060411B2 (en) 2019-03-22 2021-07-13 Pratt & Whitney Canada Corp. Inner shroud assembly for stator vanes

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Publication number Priority date Publication date Assignee Title
DE969599C (de) * 1943-05-27 1958-06-19 Holzwarth Gasturbinen G M B H Gekuehlter Duesenkoerper fuer Kreiselmaschinen, insbesondere Abgasturbinen
US2941300A (en) * 1954-05-21 1960-06-21 Sheffield Corp Gauging device
US2914300A (en) * 1955-12-22 1959-11-24 Gen Electric Nozzle vane support for turbines
GB991357A (en) * 1963-12-04 1965-05-05 Rolls Royce Axial fluid flow machine such as a compressor or turbine
US3442442A (en) * 1966-12-02 1969-05-06 Gen Electric Mounting of blades in an axial flow compressor
FR2073239A1 (de) * 1969-12-01 1971-10-01 Snecma
US3867066A (en) * 1972-03-17 1975-02-18 Ingersoll Rand Co Gas compressor
US3849023A (en) * 1973-06-28 1974-11-19 Gen Electric Stator assembly
CA994246A (en) * 1973-09-27 1976-08-03 Harold Tai Vane damping
FR2321616A1 (fr) * 1975-08-21 1977-03-18 Snecma Perfectionnements a la fixation des aubes statoriques d'une soufflante ou d'un compresseur a flux axial
GB2043798B (en) * 1979-03-14 1983-01-12 Rolls Royce Gas turbine stator vane assembly
GB2115883B (en) * 1982-02-26 1986-04-30 Gen Electric Turbomachine airfoil mounting assembly
FR2600379B1 (fr) * 1986-06-18 1988-09-02 Snecma Redresseur de soufflante de turboreacteur multiflux

Also Published As

Publication number Publication date
FR2610673B1 (fr) 1991-03-15
EP0277884A2 (de) 1988-08-10
FR2610673A1 (fr) 1988-08-12
US4940386A (en) 1990-07-10
EP0277884B1 (de) 1993-04-14
EP0277884A3 (en) 1990-07-11
DE3880167T2 (de) 1993-08-26

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee