BR112014005409B8 - método de fabricação de um setor a partir de um material compósito para um bocal de turbina ou um difusor de compressor de um motor de turbina, turbina e compressor para um motor de turbina, e, motor de turbina - Google Patents
método de fabricação de um setor a partir de um material compósito para um bocal de turbina ou um difusor de compressor de um motor de turbina, turbina e compressor para um motor de turbina, e, motor de turbinaInfo
- Publication number
- BR112014005409B8 BR112014005409B8 BR112014005409A BR112014005409A BR112014005409B8 BR 112014005409 B8 BR112014005409 B8 BR 112014005409B8 BR 112014005409 A BR112014005409 A BR 112014005409A BR 112014005409 A BR112014005409 A BR 112014005409A BR 112014005409 B8 BR112014005409 B8 BR 112014005409B8
- Authority
- BR
- Brazil
- Prior art keywords
- turbine
- turbine engine
- composite material
- compressor
- sector
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
- B29C70/04—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
- B29C70/06—Fibrous reinforcements only
- B29C70/10—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
- B29C70/16—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
- B29C70/24—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in at least three directions forming a three dimensional structure
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/52—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbon, e.g. graphite
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/563—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on boron carbide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/515—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics
- C04B35/56—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides
- C04B35/565—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products based on non-oxide ceramics based on carbides or oxycarbides based on silicon carbide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/628—Coating the powders or the macroscopic reinforcing agents
- C04B35/62844—Coating fibres
- C04B35/62857—Coating fibres with non-oxide ceramics
- C04B35/62865—Nitrides
- C04B35/62868—Boron nitride
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/628—Coating the powders or the macroscopic reinforcing agents
- C04B35/62844—Coating fibres
- C04B35/62857—Coating fibres with non-oxide ceramics
- C04B35/62873—Carbon
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/622—Forming processes; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/626—Preparing or treating the powders individually or as batches ; preparing or treating macroscopic reinforcing agents for ceramic products, e.g. fibres; mechanical aspects section B
- C04B35/628—Coating the powders or the macroscopic reinforcing agents
- C04B35/62897—Coatings characterised by their thickness
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B35/00—Shaped ceramic products characterised by their composition; Ceramics compositions; Processing powders of inorganic compounds preparatory to the manufacturing of ceramic products
- C04B35/71—Ceramic products containing macroscopic reinforcing agents
- C04B35/78—Ceramic products containing macroscopic reinforcing agents containing non-metallic materials
- C04B35/80—Fibres, filaments, whiskers, platelets, or the like
-
- 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
- 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
- F01D5/284—Selection of ceramic materials
-
- 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
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/02—Selection of particular materials
- F04D29/023—Selection of particular materials especially adapted for elastic fluid pumps
-
- 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
-
- 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
-
- 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
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/52—Constituents or additives characterised by their shapes
- C04B2235/5208—Fibers
- C04B2235/5216—Inorganic
- C04B2235/522—Oxidic
- C04B2235/5224—Alumina or aluminates
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/52—Constituents or additives characterised by their shapes
- C04B2235/5208—Fibers
- C04B2235/5216—Inorganic
- C04B2235/524—Non-oxidic, e.g. borides, carbides, silicides or nitrides
- C04B2235/5244—Silicon carbide
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/02—Composition of constituents of the starting material or of secondary phases of the final product
- C04B2235/50—Constituents or additives of the starting mixture chosen for their shape or used because of their shape or their physical appearance
- C04B2235/52—Constituents or additives characterised by their shapes
- C04B2235/5208—Fibers
- C04B2235/5252—Fibers having a specific pre-form
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
- C04B2235/612—Machining
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
- C04B2235/614—Gas infiltration of green bodies or pre-forms
-
- C—CHEMISTRY; METALLURGY
- C04—CEMENTS; CONCRETE; ARTIFICIAL STONE; CERAMICS; REFRACTORIES
- C04B—LIME, MAGNESIA; SLAG; CEMENTS; COMPOSITIONS THEREOF, e.g. MORTARS, CONCRETE OR LIKE BUILDING MATERIALS; ARTIFICIAL STONE; CERAMICS; REFRACTORIES; TREATMENT OF NATURAL STONE
- C04B2235/00—Aspects relating to ceramic starting mixtures or sintered ceramic products
- C04B2235/60—Aspects relating to the preparation, properties or mechanical treatment of green bodies or pre-forms
- C04B2235/616—Liquid infiltration of green bodies or pre-forms
-
- 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
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
-
- 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
- F05D2240/12—Fluid guiding means, e.g. vanes
-
- 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
- F05D2300/6033—Ceramic matrix composites [CMC]
-
- 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)
- Chemical & Material Sciences (AREA)
- Ceramic Engineering (AREA)
- Materials Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Mechanical Engineering (AREA)
- Organic Chemistry (AREA)
- Structural Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Textile Engineering (AREA)
- Inorganic Chemistry (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Woven Fabrics (AREA)
Abstract
método para produção de um setor de uma pá de hélice de estator de compressor ou bocal de turbina feito de um material compósito para um motor de turbina e turbina ou com pressor que inclui uma pá de hélice de estator ou bocal que consiste nos ditos setores trata-se de pás de hélice com aerofólio único que têm, cada uma, uma plataforma interna (114), uma plataforma externa (116) e um aerofólio (118) são obtidos ao: usar tecelagem tridimensional para produzir um bloco bruto de fibra como uma peça única; conformar o bloco bruto de fibra para obter uma pré-forma de fibra inteiriça; e densificar a pré-forma com uma matriz para obter uma pá de hélice de material compósito que forma uma peça única com plataformas interna e externa incorporadas na mesma. uma pluralidade de pás de hélice são montadas e ligadas para formar um setor com múltiplos aerofólios feitos de material compósito para um bocal de turbina ou um difusor de compressor, sendo que a ligação é realizada por um processo que compreende pelo menos uma etapa selecionada de: uma etapa de ligação por brasagem; e uma etapa de ligação por codensificação com pás de hélice de matriz em comum que já foram montadas enquanto em um estágio intermediário de densificação.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1157925A FR2979573B1 (fr) | 2011-09-07 | 2011-09-07 | Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine et turbine ou compresseur incorporant un distributeur ou un redresseur forme de tels secteurs |
FR1157925 | 2011-09-07 | ||
PCT/FR2012/051994 WO2013034857A2 (fr) | 2011-09-07 | 2012-09-06 | Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine et turbine ou compresseur incorporant un distributeur ou un redresseur forme de tels secteurs |
Publications (3)
Publication Number | Publication Date |
---|---|
BR112014005409A2 BR112014005409A2 (pt) | 2017-06-13 |
BR112014005409B1 BR112014005409B1 (pt) | 2020-08-25 |
BR112014005409B8 true BR112014005409B8 (pt) | 2020-12-08 |
Family
ID=46968264
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014005409A BR112014005409B8 (pt) | 2011-09-07 | 2012-09-06 | método de fabricação de um setor a partir de um material compósito para um bocal de turbina ou um difusor de compressor de um motor de turbina, turbina e compressor para um motor de turbina, e, motor de turbina |
Country Status (8)
Country | Link |
---|---|
EP (1) | EP2753466B1 (pt) |
JP (1) | JP6038153B2 (pt) |
CN (1) | CN103796818B (pt) |
BR (1) | BR112014005409B8 (pt) |
CA (1) | CA2848018C (pt) |
FR (1) | FR2979573B1 (pt) |
RU (1) | RU2608405C2 (pt) |
WO (1) | WO2013034857A2 (pt) |
Families Citing this family (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10309235B2 (en) * | 2012-08-27 | 2019-06-04 | United Technologies Corporation | Shiplap cantilevered stator |
US20140193270A1 (en) * | 2013-01-08 | 2014-07-10 | Coi Ceramics, Inc. | Ceramic composite matrix material bonded assembly and processes thereof |
WO2015009392A2 (en) * | 2013-07-19 | 2015-01-22 | General Electric Comapny | Turbine nozzle with impingement baffle |
US10180073B2 (en) * | 2013-08-06 | 2019-01-15 | General Electric Company | Mounting apparatus for low-ductility turbine nozzle |
FR3018308B1 (fr) * | 2014-03-06 | 2016-04-08 | Herakles | Secteur de stator pour turbomachine et son procede de fabrication |
FR3021349B1 (fr) * | 2014-05-22 | 2021-07-02 | Herakles | Procede de fabrication d'une aube de turbomachine en materiau composite, aube ainsi obtenue et turbomachine l'incorporant |
FR3037097B1 (fr) * | 2015-06-03 | 2017-06-23 | Snecma | Aube composite comprenant une plateforme munie d'un raidisseur |
US9850772B2 (en) * | 2015-04-24 | 2017-12-26 | General Electric Company | Seals with a thermal barrier for turbomachinery |
US10563524B2 (en) | 2017-06-14 | 2020-02-18 | General Electric Company | Ceramic matrix composite (CMC) turbine blades and methods of forming CMC turbine blades |
CN109139262A (zh) * | 2017-06-28 | 2019-01-04 | 中国航发贵阳发动机设计研究所 | 一种航空发动机燃烧室扩压器 |
CN111102017B (zh) * | 2019-12-13 | 2022-07-12 | 西安鑫垚陶瓷复合材料有限公司 | 航空发动机陶瓷基复合材料固定导向器叶片结构及其成型 |
FR3112142B1 (fr) * | 2020-07-03 | 2022-09-09 | Safran Ceram | Procédé de fabrication d’une aube de distributeur en matériau composite à matrice céramique |
RU206651U1 (ru) * | 2021-04-16 | 2021-09-21 | Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК") | Направляющий аппарат статора компрессора газотурбинного двигателя |
FR3122208A1 (fr) * | 2021-04-21 | 2022-10-28 | Safran Aircraft Engines | Procede de finition d’une aube composite pour turbomachine d’aeronef |
FR3127019A1 (fr) | 2021-09-14 | 2023-03-17 | Safran Aircraft Engines | Distributeur en CMC dont l’étanchéité est améliorée et Turbine de turbomachine associée |
CN114483207B (zh) * | 2021-12-29 | 2024-03-08 | 西安鑫垚陶瓷复合材料股份有限公司 | 陶瓷基复合材料涡轮外环预制体、定型模具及其使用方法 |
Family Cites Families (21)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2640258B1 (fr) | 1988-05-10 | 1991-06-07 | Europ Propulsion | Procede de fabrication de materiaux composites a renfort en fibres de carbure de silicium et a matrice ceramique |
FR2664518B1 (fr) * | 1990-07-12 | 1995-02-17 | Europ Propulsion | Composition de brasage pour materiaux ceramiques et materiaux composites thermostructuraux et procede pour sa mise en óoeuvre. |
US5246756A (en) | 1992-01-29 | 1993-09-21 | Mobil Oil Corporation | Release sheet |
JPH05288001A (ja) * | 1992-04-06 | 1993-11-02 | Ngk Insulators Ltd | 冷却孔付セラミックスガスタービン静翼及びその製造方法 |
FR2732338B1 (fr) | 1995-03-28 | 1997-06-13 | Europ Propulsion | Materiau composite protege contre l'oxydation par matrice auto-cicatrisante et son procede de fabrication |
JPH09125905A (ja) * | 1995-11-02 | 1997-05-13 | Ngk Insulators Ltd | 多連式セラミック静翼及びその製造方法 |
FR2745808B1 (fr) * | 1996-03-07 | 1998-04-10 | Snecma | Procede de brasage de pieces en materiaux composites a matrice ceramique ou vitroceramique |
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 |
US6227798B1 (en) * | 1999-11-30 | 2001-05-08 | General Electric Company | Turbine nozzle segment band cooling |
JP3831265B2 (ja) * | 2002-01-21 | 2006-10-11 | 本田技研工業株式会社 | 静翼構造体の製造方法 |
FR2844510B1 (fr) * | 2002-09-12 | 2006-06-16 | Snecma Propulsion Solide | Structure fibreuse tridimensionnelle en fibres refractaires, procede pour sa realisation et application aux materiaux composites thermostructuraux |
DE10334342A1 (de) * | 2003-07-29 | 2005-02-24 | Mtu Aero Engines Gmbh | Fasergelege und Verfahren zur Herstellung desselben |
US7334306B2 (en) * | 2004-06-02 | 2008-02-26 | General Electric Company | Methods and apparatus for fabricating a turbine nozzle assembly |
FR2887601B1 (fr) | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | Piece mecanique et procede de fabrication d'une telle piece |
WO2007085912A2 (en) * | 2005-12-29 | 2007-08-02 | Rolls-Royce Power Engineering Plc | Airfoil for a first stage nozzle guide vane |
FR2933970B1 (fr) | 2008-07-21 | 2012-05-11 | Snecma Propulsion Solide | Procede de fabrication d'une piece en materiau composite thermostructural et piece ainsi obtenue |
FR2939129B1 (fr) * | 2008-11-28 | 2014-08-22 | Snecma Propulsion Solide | Aube de turbomachine en materiau composite et procede pour sa fabrication. |
FR2943942B1 (fr) * | 2009-04-06 | 2016-01-29 | Snecma | Procede de fabrication d'une aube de turbomachine en materiau composite |
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 |
US8499450B2 (en) * | 2010-01-26 | 2013-08-06 | United Technologies Corporation | Three-dimensionally woven composite blade with spanwise weft yarns |
-
2011
- 2011-09-07 FR FR1157925A patent/FR2979573B1/fr active Active
-
2012
- 2012-09-06 CN CN201280043538.XA patent/CN103796818B/zh active Active
- 2012-09-06 RU RU2014113419A patent/RU2608405C2/ru active
- 2012-09-06 JP JP2014529053A patent/JP6038153B2/ja active Active
- 2012-09-06 WO PCT/FR2012/051994 patent/WO2013034857A2/fr active Application Filing
- 2012-09-06 BR BR112014005409A patent/BR112014005409B8/pt active IP Right Grant
- 2012-09-06 CA CA2848018A patent/CA2848018C/fr active Active
- 2012-09-06 EP EP12767035.4A patent/EP2753466B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
BR112014005409A2 (pt) | 2017-06-13 |
FR2979573A1 (fr) | 2013-03-08 |
FR2979573B1 (fr) | 2017-04-21 |
EP2753466A2 (fr) | 2014-07-16 |
CA2848018C (fr) | 2019-12-31 |
BR112014005409B1 (pt) | 2020-08-25 |
JP2014529708A (ja) | 2014-11-13 |
JP6038153B2 (ja) | 2016-12-07 |
RU2014113419A (ru) | 2015-10-20 |
WO2013034857A2 (fr) | 2013-03-14 |
CN103796818A (zh) | 2014-05-14 |
WO2013034857A3 (fr) | 2013-10-24 |
CN103796818B (zh) | 2016-12-28 |
RU2608405C2 (ru) | 2017-01-18 |
CA2848018A1 (fr) | 2013-03-14 |
EP2753466B1 (fr) | 2017-11-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BR112014005409B8 (pt) | método de fabricação de um setor a partir de um material compósito para um bocal de turbina ou um difusor de compressor de um motor de turbina, turbina e compressor para um motor de turbina, e, motor de turbina | |
WO2013060977A3 (fr) | Procede de fabrication d'un secteur de distributeur de turbine ou redresseur de compresseur en materiau composite pour turbomachine | |
CN103030416B (zh) | Cmc构件、功率发生***和形成cmc构件的方法 | |
RU2013104448A (ru) | Лопасть со встроенным композитным лонжероном | |
GB2478673A (en) | Ceramic matrix composite blade having integral platform structures and methods of fabrication | |
RU2016119631A (ru) | Волокнистая заготовка для полой лопатки газотурбинного двигателя | |
BR112017020233A2 (pt) | núcleo cerâmico, uso de um núcleo cerâmico, método de fabricação para fabricar uma pá de turbina oca para um motor de turbina, e, motor de turbina | |
ATE397512T1 (de) | Hälfte einer hohlen gebläseschaufel, hohle gebläseschaufel für gasturbinentriebwerk, sowie entsprechendes herstellungsverfahren | |
DE602005007274D1 (de) | Hälfte einer hohlen Gebläseschaufel, hohle Gebläseschaufel für Gasturbinentriebwerk, sowie entsprechendes Herstellungsverfahren | |
ATE517725T1 (de) | Helikopterblattdorn, verfahren zur herstellung des helikopterblattdorns und verfahren zur formung eines helikopterrotorblattes | |
BRPI0909405A2 (pt) | processo de fabricação de um disco com pás monobloco | |
ATE381976T1 (de) | Herstellungsverfahren für eine hohle gebläseschaufel einer strömungsmaschine | |
ATE478251T1 (de) | Verfahren zur herstellung einer mit einem cmc- flussmischer ausgestatteten struktur für einen turbinen-luftmotor | |
BR112016012234A2 (pt) | Método para formar uma construção em um leito de pó e aparelho para formar uma construção em um leito de pó | |
EP2105579A3 (en) | An article formed from a composite material | |
RU2014121516A (ru) | Способ изготовления композитных лопаток турбинного двигателя со встроенными полками | |
EP1557532A3 (en) | Hollow fan blade for gas turbine engine, gas turbine engine and method for making such a hollow fan blade | |
EP2540486A3 (en) | Method of making composite fan blade | |
RU2016139110A (ru) | Сектор статора для газотурбинного двигателя и способ его изготовления | |
CN104812950B (zh) | 用于制造复合材料的涡轮发动机叶片根部的方法以及通过这种方法获得的叶片根部 | |
EP2706241A3 (en) | Fan blade | |
DK1603736T3 (da) | Forbindelse imellem elementer | |
RU2010144484A (ru) | Способ изготовления моноблочного лопаточного диска с кольцом для временного удержания лопаток | |
US20130224035A1 (en) | Composite airfoil with local tailoring of material properties | |
ATE537060T1 (de) | Rotorblatt als faserverbundprofilkörper und verfahren zu seiner herstellung mittels harzinjektionstechnik |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
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 06/09/2012, OBSERVADAS AS CONDICOES LEGAIS. |
|
B16C | Correction of notification of the grant [chapter 16.3 patent gazette] |
Free format text: REF. RPI 2590 DE 25/08/2020 QUANTO AO TITULO. |