BR112015010841A2 - preforma e módulo de pá monobloco para um invólucro intermediário de turbomáquina - Google Patents

preforma e módulo de pá monobloco para um invólucro intermediário de turbomáquina

Info

Publication number
BR112015010841A2
BR112015010841A2 BR112015010841A BR112015010841A BR112015010841A2 BR 112015010841 A2 BR112015010841 A2 BR 112015010841A2 BR 112015010841 A BR112015010841 A BR 112015010841A BR 112015010841 A BR112015010841 A BR 112015010841A BR 112015010841 A2 BR112015010841 A2 BR 112015010841A2
Authority
BR
Brazil
Prior art keywords
preform
blade
module
turbomachine housing
shovel module
Prior art date
Application number
BR112015010841A
Other languages
English (en)
Other versions
BR112015010841B1 (pt
Inventor
Marie Christian Coupe Dominique
Gimat Matthieu
Georges Paul Papin Thierry
Marchal Yann
Original Assignee
Snecma
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 filed Critical Snecma
Publication of BR112015010841A2 publication Critical patent/BR112015010841A2/pt
Publication of BR112015010841B1 publication Critical patent/BR112015010841B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00—Making preforms
    • B29B11/14—Making preforms characterised by structure or composition
    • B29B11/16—Making preforms characterised by structure or composition comprising fillers or reinforcement
    • 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
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • F01D5/146—Shape, i.e. outer, aerodynamic form of blades with tandem configuration, split blades or slotted 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
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/28—Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • F01D5/282—Selecting composite materials, e.g. blades with reinforcing filaments
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00—Other particular articles
    • B29L2031/08—Blades for rotors, stators, fans, turbines or the like, e.g. screw propellers
    • B29L2031/087—Propellers
    • 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
    • F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603—Composites; e.g. fibre-reinforced
    • 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)
  • Chemical & Material Sciences (AREA)
  • Materials Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Composite Materials (AREA)
  • Fluid Mechanics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Woven Fabrics (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

1/1 resumo “preforma e módulo de pá monobloco para um invólucro intermediário de turbomáquina” uma preforma de fibra para um módulo de pá de um invólucro intermediário de turbomáquina, a preforma sendo obtida por tecelagem tridimensional. de acordo com a invenção, a preforma compreende primeiro segmento longitudinal, apresentando primeira e segunda extremidades opostas e adequadas para formar uma primeira pá (21); um segundo segmento longitudinal apresentando primeira e segunda extremidades opostas e adequado para formar uma segunda pá (21); e um primeiro segmento transversal conectando juntos o primeiro e segundo segmentos longitudinais por suas primeiras extremidades, e adequado para formar uma primeira parte de pá transversal (26), tal como um flange ou uma plataforma.
BR112015010841-5A 2012-11-13 2013-11-12 pré-forma de fibra para módulo de pá de um cárter intermediário de uma turbomáquina, módulo para produzir cárter intermediário, carter intermediário e turbomáquina BR112015010841B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US201261725622P 2012-11-13 2012-11-13
US61/725,622 2012-11-13
PCT/FR2013/052713 WO2014076407A1 (fr) 2012-11-13 2013-11-12 Preforme et module d'aubes monobloc pour un carter intermediaire de turbomachine

Publications (2)

Publication Number Publication Date
BR112015010841A2 true BR112015010841A2 (pt) 2017-07-11
BR112015010841B1 BR112015010841B1 (pt) 2021-04-20

Family

ID=49780074

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015010841-5A BR112015010841B1 (pt) 2012-11-13 2013-11-12 pré-forma de fibra para módulo de pá de um cárter intermediário de uma turbomáquina, módulo para produzir cárter intermediário, carter intermediário e turbomáquina

Country Status (8)

Country Link
US (1) US10131073B2 (pt)
EP (1) EP2919954B1 (pt)
JP (2) JP6382829B2 (pt)
CN (1) CN104870153B (pt)
BR (1) BR112015010841B1 (pt)
CA (1) CA2891289C (pt)
RU (1) RU2645510C2 (pt)
WO (1) WO2014076407A1 (pt)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2977550B1 (fr) * 2014-07-22 2017-05-31 Safran Aero Boosters SA Aube de turbomachine axiale et turbomachine associée
JP6616402B2 (ja) * 2014-08-26 2019-12-04 サフラン エアークラフト エンジンズ ガスタービンエンジン用の千鳥状取付フランジを具備する複合材料製案内翼
US10018064B2 (en) 2015-03-02 2018-07-10 United Technologies Corporation Floating panel for a gas powered turbine
US10436036B2 (en) * 2016-07-05 2019-10-08 Safran Aircraft Engines Fitted platform for a turbine engine fan, and a method of fabricating it
US10443625B2 (en) * 2016-09-21 2019-10-15 General Electric Company Airfoil singlets
US10428658B2 (en) * 2016-11-17 2019-10-01 United Technologies Corporation Airfoil with panel fastened to core structure
FR3074839B1 (fr) 2017-12-13 2019-11-08 Safran Aircraft Engines Aube multipale de rotor de turbomachine et rotor la comprenant
WO2022235149A1 (en) * 2021-05-03 2022-11-10 InfraCore IP B.V. Structure composed of a plurality of sheets
FR3134598B1 (fr) * 2022-04-15 2024-04-05 Safran Aircraft Engines Aube fixe en matériaux composites fixée radialement sur une structure fixe d’une turbomachine

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3501090A (en) * 1968-01-29 1970-03-17 Gen Electric Composite bladed rotors
US4958663A (en) * 1988-08-15 1990-09-25 Hitco Woven multi-layer angle interlock fabrics having fill weaver yarns interwoven with relatively straight extending warp yarns
GB9007162D0 (en) * 1990-03-30 1990-05-30 Courtaulds Plc Preform and composite structure
KR20000064395A (ko) * 1995-12-15 2000-11-06 드폴 루이스 에이 고온환경장치용세라믹산화물복합재,방법및시스템
US5921754A (en) * 1996-08-26 1999-07-13 Foster-Miller, Inc. Composite turbine rotor
JP4060981B2 (ja) * 1998-04-08 2008-03-12 本田技研工業株式会社 ガスタービンの静翼構造体及びそのユニット
FR2817192B1 (fr) * 2000-11-28 2003-08-08 Snecma Moteurs Ensemble forme par au moins une pale et une plate-forme de fixation de la pale, pour une turbomachine, et procede pour sa fabrication
US6821087B2 (en) * 2002-01-21 2004-11-23 Honda Giken Kogyo Kabushiki Kaisha Flow-rectifying member and its unit and method for producing flow-rectifying member
RU2280767C2 (ru) * 2004-10-14 2006-07-27 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения им. П.И. Баранова" Способ изготовления рабочего колеса турбины из композиционных материалов
US7371046B2 (en) * 2005-06-06 2008-05-13 General Electric Company Turbine airfoil with variable and compound fillet
US7341427B2 (en) * 2005-12-20 2008-03-11 General Electric Company Gas turbine nozzle segment and process therefor
US7726937B2 (en) * 2006-09-12 2010-06-01 United Technologies Corporation Turbine engine compressor vanes
FR2939129B1 (fr) * 2008-11-28 2014-08-22 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.
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.
FR2953885B1 (fr) 2009-12-14 2012-02-10 Snecma Aube de turbomachine en materiau composite et procede pour sa fabrication
FR2956876B1 (fr) 2010-02-26 2012-10-19 Snecma Module structural et aerodynamique d'un carter de turbomachine et structure de carter comportant une pluralite d'un tel module
FR2976968B1 (fr) 2011-06-21 2015-06-05 Snecma Piece de turbomachine formant redresseur de compresseur ou distributeur de turbine et procede pour sa fabrication
US8905719B2 (en) * 2011-12-20 2014-12-09 General Electric Co. Composite rotor and vane assemblies with integral airfoils

Also Published As

Publication number Publication date
US10131073B2 (en) 2018-11-20
CN104870153A (zh) 2015-08-26
EP2919954B1 (fr) 2018-07-18
BR112015010841B1 (pt) 2021-04-20
CA2891289A1 (fr) 2014-05-22
CA2891289C (fr) 2021-09-28
RU2015122646A (ru) 2017-01-10
WO2014076407A1 (fr) 2014-05-22
JP2018173083A (ja) 2018-11-08
JP6382829B2 (ja) 2018-08-29
EP2919954A1 (fr) 2015-09-23
JP6616454B2 (ja) 2019-12-04
RU2645510C2 (ru) 2018-02-21
JP2016505747A (ja) 2016-02-25
CN104870153B (zh) 2018-03-13
US20150354377A1 (en) 2015-12-10

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Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06I Publication of requirement cancelled [chapter 6.9 patent gazette]

Free format text: ANULADA A PUBLICACAO CODIGO 6.6.1 NA RPI NO 2462 DE 13/03/2018 POR TER SIDO INDEVIDA.

B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 12/11/2013, OBSERVADAS AS CONDICOES LEGAIS.