ES2039116T3 - Distribuidor de turbina para turbo-reactor y su procedimiento de fabricacion. - Google Patents

Distribuidor de turbina para turbo-reactor y su procedimiento de fabricacion.

Info

Publication number
ES2039116T3
ES2039116T3 ES199090401321T ES90401321T ES2039116T3 ES 2039116 T3 ES2039116 T3 ES 2039116T3 ES 199090401321 T ES199090401321 T ES 199090401321T ES 90401321 T ES90401321 T ES 90401321T ES 2039116 T3 ES2039116 T3 ES 2039116T3
Authority
ES
Spain
Prior art keywords
rings
turbo
reactor
distributor
manufacturing procedure
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 - Lifetime
Application number
ES199090401321T
Other languages
English (en)
Inventor
Jacques G. Fouillot
Gerard Letanter
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.)
Societe Europeenne de Propulsion SEP SA
Original Assignee
Societe Europeenne de Propulsion SEP SA
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 Europeenne de Propulsion SEP SA filed Critical Societe Europeenne de Propulsion SEP SA
Application granted granted Critical
Publication of ES2039116T3 publication Critical patent/ES2039116T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3069—Fixing blades to rotors; Blade roots ; Blade spacers between two discs or 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3084—Fixing blades to rotors; Blade roots ; Blade spacers the blades being made of ceramics
    • 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
    • F05D2300/00—Materials; Properties thereof
    • F05D2300/20—Oxide or non-oxide ceramics
    • F05D2300/21—Oxide ceramics
    • 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
    • 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
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49316—Impeller making
    • Y10T29/4932—Turbomachine making
    • Y10T29/49323—Assembling fluid flow directing devices, e.g., stators, diaphragms, nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Ceramic Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Physical Or Chemical Processes And Apparatus (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

EL DISTRIBUIDOR ESTA REALIZADO EN MATERIAL COMPUESTO DE MATRIZ CERAMICA Y CONSTA DE: UN CUBO QUE LLEVA UNAS PALETAS (12) CON UN DEDO (14) QUE SOBRESALE RADIALMENTE POR EL EXTREMO DE CADA PALETA; Y DOS ANILLOS DENTADOS (20,30) QUE TIENEN UNOS DENTADOS, UNO FRENTE A OTRO, Y APLICADOS UNO CONTRA OTRO PARA INMOVILIZAR CADA ESPIGA DE LA PALETA AXIAL Y CIRCUNFERENCIALMENTE ENTRE UN PLANTO (22) DE UN DIENTE (21) Y UN ANILLO Y UN FLANCO (32) DE UN DIENTE (31) DEL OTRO ANILLO. LOS ANILLOS (20,30) ESTAN APLICADOS UNO HACIA EL OTRO MEDIANTE UNOS ELEMENTOS ELASTICOS, LO QUE PROPORCIONA UNA SEPARACION MUTUA, CON ROTACION RELATIVA ENTRE LOS DOS ANILLOS, BAJO EL EFECTO DE LA DILATACION DE LAS ESPIGAS DE LAS PALETAS, REALIZANDOSE LA FIJACION DEL DISTRIBUIDOR AL CARTER DEL TURBO-REACTOR POR ENLACE MECANICO ENTRE EL CARTER Y UNO DE LOS ANILLOS.
ES199090401321T 1989-05-23 1990-05-18 Distribuidor de turbina para turbo-reactor y su procedimiento de fabricacion. Expired - Lifetime ES2039116T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8906748A FR2647502B1 (fr) 1989-05-23 1989-05-23 Distributeur de turbine pour turbo-reacteur et son procede de fabrication

Publications (1)

Publication Number Publication Date
ES2039116T3 true ES2039116T3 (es) 1993-08-16

Family

ID=9381931

Family Applications (1)

Application Number Title Priority Date Filing Date
ES199090401321T Expired - Lifetime ES2039116T3 (es) 1989-05-23 1990-05-18 Distribuidor de turbina para turbo-reactor y su procedimiento de fabricacion.

Country Status (6)

Country Link
US (1) US5074749A (es)
EP (1) EP0399879B1 (es)
CA (1) CA2017263C (es)
DE (1) DE69000854T2 (es)
ES (1) ES2039116T3 (es)
FR (1) FR2647502B1 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5411368A (en) * 1993-11-08 1995-05-02 Allied-Signal Inc. Ceramic-to-metal stator vane assembly with braze
US5704762A (en) * 1993-11-08 1998-01-06 Alliedsignal Inc. Ceramic-to-metal stator vane assembly
US5788456A (en) * 1997-02-21 1998-08-04 Dresser-Rand Company Turbine diaphragm assembly and method thereof
US6000906A (en) * 1997-09-12 1999-12-14 Alliedsignal Inc. Ceramic airfoil
JP3722188B2 (ja) 1999-01-28 2005-11-30 石川島播磨重工業株式会社 セラミックス基複合部材及びその製造方法
US6200092B1 (en) * 1999-09-24 2001-03-13 General Electric Company Ceramic turbine nozzle
JP5091615B2 (ja) * 2007-10-15 2012-12-05 三菱重工業株式会社 静翼環セグメントの組立方法、静翼環セグメント、結合部材、溶接方法
FR2946999B1 (fr) 2009-06-18 2019-08-09 Safran Aircraft Engines Element de distributeur de turbine en cmc, procede pour sa fabrication, et distributeur et turbine a gaz l'incorporant.
EP2431571B1 (fr) * 2010-09-16 2013-06-05 Techspace Aero S.A. Assemblage d'un aube et d'un support composite par scellage
US8696311B2 (en) 2011-03-29 2014-04-15 Pratt & Whitney Canada Corp. Apparatus and method for gas turbine engine vane retention
US8770931B2 (en) * 2011-05-26 2014-07-08 United Technologies Corporation Hybrid Ceramic Matrix Composite vane structures for a gas turbine engine
EP2971578B1 (en) * 2013-03-15 2020-05-06 United Technologies Corporation Method of assembling a gas turbine engine front architecture and corresponding gas turbine engine front architecture
DE102013213834A1 (de) * 2013-07-15 2015-02-19 MTU Aero Engines AG Verfahren zum Herstellen eines Isolationselements und Isolationselement für ein Gehäuse eines Flugtriebwerks
US10746035B2 (en) 2017-08-30 2020-08-18 General Electric Company Flow path assemblies for gas turbine engines and assembly methods therefore

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR389268A (fr) * 1907-04-20 1908-09-04 Carl Roth Système de fixation des aubes de turbines à vapeur et autres machines analogues
US2221684A (en) * 1938-08-27 1940-11-12 Gen Electric Elastic fluid turbine bucket wheel
FR896203A (fr) * 1942-07-09 1945-02-15 Wagner Hochdruck Dampfturbinen Supports d'aubes directrices pour turbines à vapeur ou à gaz
GB828248A (en) * 1956-04-16 1960-02-17 Gen Electric Improvements in turbine and compressor blade cover assembly
US3042366A (en) * 1958-05-05 1962-07-03 Holmquist Ernst Rudolf Magnus Axial flow gas turbine
US3357082A (en) * 1963-02-13 1967-12-12 Whiton Machine Company Method of making a turbine wheel
FR1339521A (fr) * 1966-06-10 1963-10-11 Rolls Royce Machine à circulation de fluide
US3367630A (en) * 1967-01-16 1968-02-06 Westinghouse Electric Corp Continuous shroud structure
US3677663A (en) * 1970-10-01 1972-07-18 Avco Corp Damped turbomachine rotor assembly
US3905723A (en) * 1972-10-27 1975-09-16 Norton Co Composite ceramic turbine rotor
US3900626A (en) * 1973-09-04 1975-08-19 United Aircraft Corp Tantalum wire reinforced silicon nitride articles and method for making the same
US4066384A (en) * 1975-07-18 1978-01-03 Westinghouse Electric Corporation Turbine rotor blade having integral tenon thereon and split shroud ring associated therewith
JPS5311201A (en) * 1976-07-20 1978-02-01 Mitsubishi Heavy Ind Ltd Infinite cascade structure for rotary machines
DE2635830A1 (de) * 1976-08-09 1978-02-16 Siemens Ag Anordnung zur befestigung eines deckbandes an turbinenschaufeln
FR2567874B1 (fr) * 1984-07-20 1987-01-02 Europ Propulsion Procede de fabrication d'un materiau composite a renfort fibreux refractaire et matrice ceramique, et structure telle qu'obtenue par ce procede
US4643636A (en) * 1985-07-22 1987-02-17 Avco Corporation Ceramic nozzle assembly for gas turbine engine

Also Published As

Publication number Publication date
CA2017263A1 (en) 1990-11-23
EP0399879A1 (fr) 1990-11-28
DE69000854D1 (de) 1993-03-18
EP0399879B1 (fr) 1993-02-03
DE69000854T2 (de) 1993-08-19
US5074749A (en) 1991-12-24
CA2017263C (en) 1999-12-28
FR2647502A1 (fr) 1990-11-30
FR2647502B1 (fr) 1991-09-13

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