BR112014014244A2 - estrutura de fibra tecida como uma única peça por tecelagem em 3d, e uma aplicação da mesma para fabricar uma parte de material compósito - Google Patents
estrutura de fibra tecida como uma única peça por tecelagem em 3d, e uma aplicação da mesma para fabricar uma parte de material compósitoInfo
- Publication number
- BR112014014244A2 BR112014014244A2 BR112014014244A BR112014014244A BR112014014244A2 BR 112014014244 A2 BR112014014244 A2 BR 112014014244A2 BR 112014014244 A BR112014014244 A BR 112014014244A BR 112014014244 A BR112014014244 A BR 112014014244A BR 112014014244 A2 BR112014014244 A2 BR 112014014244A2
- Authority
- BR
- Brazil
- Prior art keywords
- fiber structure
- piece
- zone
- weaving
- fabricate
- Prior art date
Links
Classifications
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D25/00—Woven fabrics not otherwise provided for
- D03D25/005—Three-dimensional woven fabrics
-
- 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
- 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
-
- D—TEXTILES; PAPER
- D03—WEAVING
- D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
- D03D1/00—Woven fabrics designed to make specified articles
-
- 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
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- D—TEXTILES; PAPER
- D10—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B—INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
- D10B2505/00—Industrial
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- 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
- F05D2300/601—Fabrics
- F05D2300/6012—Woven fabrics
-
- 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
- F05D2300/6034—Orientation of fibres, weaving, ply angle
-
- 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
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1002—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina
- Y10T156/1051—Methods of surface bonding and/or assembly therefor with permanent bending or reshaping or surface deformation of self sustaining lamina by folding
-
- 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
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/30—Woven fabric [i.e., woven strand or strip material]
- Y10T442/3179—Woven fabric is characterized by a particular or differential weave other than fabric in which the strand denier or warp/weft pick count is specified
- Y10T442/3195—Three-dimensional weave [e.g., x-y-z planes, multi-planar warps and/or wefts, etc.]
- Y10T442/3203—Multi-planar warp layers
Landscapes
- Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- General Engineering & Computer Science (AREA)
- Woven Fabrics (AREA)
- Reinforced Plastic Materials (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
1/1 resumo "estrutura de fibra tecida como uma única peça por tecelagem em 3d, e uma aplicação da mesma para fabricar uma parte de material compósito" em uma estrutura de fibra tecida como uma única peça por tecelagem tridimensional, primeiros fios de trama interligar camadas de fios de urdume em uma primeira porção (12) da estrutura de fibra (10) adjacente a uma zona não interligada (16) e também fios de urdume de uma segunda porção (14) da estrutura de fibra além da zona não interligada, e segundos fios de trama interligar camadas de fios de urdume da segunda porção (14) da estrutura de fibra adjacente à zona não interligada e também camadas de fios de urdume da primeira porção (12) da estrutura de fibra além da zona não interligada, de forma que os trajetos dos primeiros e segundos fios de trama se cruzam em pelo menos uma zona de transição (18) se estendendo dentro da estrutura de fibra a partir da extremidade da zona não interligada, a zona de transição se estendendo na direção de trama sobre uma distância maior do que o passo (p) entre colunas de urdume adjacentes.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201161570432P | 2011-12-14 | 2011-12-14 | |
US61/570,432 | 2011-12-14 | ||
PCT/FR2012/052853 WO2013088040A2 (fr) | 2011-12-14 | 2012-12-10 | Structure fibreuse tissee en une seule piece par tissage 3d et application a la fabrication de piece en materiau composite |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112014014244A2 true BR112014014244A2 (pt) | 2017-06-13 |
BR112014014244B1 BR112014014244B1 (pt) | 2021-01-05 |
Family
ID=47666413
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112014014244-0A BR112014014244B1 (pt) | 2011-12-14 | 2012-12-10 | estrutura de fibra tecida como uma única peça por tecelagem tridimensional |
Country Status (8)
Country | Link |
---|---|
US (2) | US10280537B2 (pt) |
EP (1) | EP2791473B1 (pt) |
JP (1) | JP6254533B2 (pt) |
CN (1) | CN103998721B (pt) |
BR (1) | BR112014014244B1 (pt) |
CA (1) | CA2858320C (pt) |
RU (1) | RU2612927C2 (pt) |
WO (1) | WO2013088040A2 (pt) |
Families Citing this family (36)
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WO2013104852A2 (fr) * | 2012-01-09 | 2013-07-18 | Snecma | Preforme fibreuse d'une aube de turbomachine en materiau composite a plate-forme integree, et son procede de realisation |
FR2989977B1 (fr) | 2012-04-26 | 2014-05-23 | Snecma | Ebauche fibreuse tissee en une seule piece par tissage tridimensionnel pour la realisation d'une plate-forme a caisson ferme pour soufflante de turbomachine en materiau composite |
FR3003668B1 (fr) | 2013-03-25 | 2020-10-30 | Snecma | Procede de conception d'une preforme commune pour la realisation de preformes d'aubes directrices de sortie de turbomachine en materiau composite a profils geometriques differents |
FR3025529B1 (fr) | 2014-09-10 | 2017-07-14 | Aircelle Sa | Preforme pour raidisseur composite courbe pour piece axisymetrique telle qu’une virole |
FR3037097B1 (fr) * | 2015-06-03 | 2017-06-23 | Snecma | Aube composite comprenant une plateforme munie d'un raidisseur |
JP5874802B1 (ja) * | 2014-11-25 | 2016-03-02 | 株式会社豊田自動織機 | 繊維構造体及び繊維強化複合材 |
FR3032726B1 (fr) * | 2015-02-16 | 2017-06-02 | Herakles | Structure fibreuse de renfort de pieces en materiau composite a forte variation d'epaisseur |
JP6524880B2 (ja) * | 2015-10-15 | 2019-06-05 | 株式会社豊田自動織機 | 多層織物 |
CN105442154B (zh) * | 2015-12-15 | 2017-05-10 | 机械科学研究总院先进制造技术研究中心 | 一种具有梯度结构的三维预制体织造方法 |
US9725832B1 (en) * | 2016-02-09 | 2017-08-08 | Albany Engineered Composites, Inc. | Weaving multilayer products using multiple warp columns and heddle columns |
US10207471B2 (en) * | 2016-05-04 | 2019-02-19 | General Electric Company | Perforated ceramic matrix composite ply, ceramic matrix composite article, and method for forming ceramic matrix composite article |
US10436036B2 (en) * | 2016-07-05 | 2019-10-08 | Safran Aircraft Engines | Fitted platform for a turbine engine fan, and a method of fabricating it |
US10443409B2 (en) * | 2016-10-28 | 2019-10-15 | Rolls-Royce North American Technologies Inc. | Turbine blade with ceramic matrix composite material construction |
US10577939B2 (en) * | 2016-11-01 | 2020-03-03 | Rolls-Royce Corporation | Turbine blade with three-dimensional CMC construction elements |
US10352273B2 (en) * | 2016-11-08 | 2019-07-16 | Rohr, Inc. | Track beam with composite lug |
US10392946B2 (en) * | 2016-12-21 | 2019-08-27 | Rolls-Royce North American Technologies Inc. | Turbine blade with reinforced platform for composite material construction |
US10557350B2 (en) | 2017-03-30 | 2020-02-11 | General Electric Company | I beam blade platform |
FR3070402B1 (fr) * | 2017-08-30 | 2020-08-28 | Safran Aircraft Engines | Texture fibreuse tissee pour la formation d'une preforme de carter |
FR3079445B1 (fr) | 2018-03-28 | 2020-04-24 | Safran | Procede de fabrication d'une aube en materiau composite a bord d'attaque metallique rapporte pour turbine a gaz |
US11035239B2 (en) * | 2018-10-25 | 2021-06-15 | General Electric Company | Ceramic matrix composite turbine nozzle shell and method of assembly |
FR3090449B1 (fr) * | 2018-12-21 | 2022-01-14 | Safran | preforme avec un renfort fibreux tisse en une seule piece pour plateforme inter aube |
FR3091724B1 (fr) * | 2019-01-15 | 2021-01-22 | Safran Aircraft Engines | Aube ou Pale d'hélice composite pour aéronef intégrant une mousse de conformation |
FR3097314B1 (fr) | 2019-06-14 | 2021-12-10 | Safran Aircraft Engines | Détermination d’une épaisseur par colorimétrie. |
FR3097904B1 (fr) | 2019-06-26 | 2021-06-11 | Safran Aircraft Engines | Plateforme inter-aube avec caisson sacrificiel |
EP3859066B1 (en) * | 2020-02-03 | 2024-01-24 | STÄUBLI BAYREUTH GmbH | Weaving method and weft selector for implementing such a method |
FR3124251B1 (fr) | 2021-06-18 | 2023-11-03 | Safran Aircraft Engines | Procédé et dispositif de détermination de l’épaisseur d’un revêtement par colorimétrie |
FR3125980B1 (fr) | 2021-08-06 | 2024-04-26 | Safran Aircraft Engines | Procédé de fabrication d’une pièce en matériau composite tissé 3D pour turbomachine |
FR3130192B1 (fr) | 2021-12-09 | 2023-11-03 | Safran | Procede de fabrication d’une piece aubagee pour une turbomachine d’aeronef |
CN114457487A (zh) * | 2022-01-04 | 2022-05-10 | 深圳全棉时代科技有限公司 | 分区提花保暖新型纱布 |
FR3132461A1 (fr) | 2022-02-10 | 2023-08-11 | Safran Aircraft Engines | Procédé de fabrication d’une plateforme inter-aubes avec bords sacrificiels |
FR3132539B1 (fr) | 2022-02-10 | 2024-02-09 | Safran Aircraft Engines | Procédé de fabrication d’une plateforme inter-aubes avec bords sacrificiels |
FR3136783B1 (fr) * | 2022-06-21 | 2024-06-21 | Safran Ceram | Métier à tisser avec peigne inclinable et procédé de tissage |
FR3136782B1 (fr) * | 2022-06-21 | 2024-06-21 | Safran Ceram | Procédé de tissage tridimensionnel d’une structure fibreuse avec orientation des colonnes de trame dans une portion de déploiement et structure fibreuse résultante |
US11873735B1 (en) * | 2022-11-10 | 2024-01-16 | General Electric Company | Composite component for a gas turbine engine |
FR3142201A1 (fr) | 2022-11-21 | 2024-05-24 | Safran Ceramics | Ebauche fibreuse avec au moins une déliaison présentant une alternance de tissage |
CN115949471B (zh) * | 2023-01-04 | 2023-12-22 | 北京航空航天大学 | 一种正交三维机织复合材料出口导向叶片及其制造方法 |
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DE60221236T2 (de) * | 2001-09-12 | 2008-04-10 | Lockheed Martin Corporation | Gewebte vorform für eine konstruktionsverbindung |
FR2861143B1 (fr) * | 2003-10-20 | 2006-01-20 | Snecma Moteurs | Aube de turbomachine, notamment aube de soufflante et son procede de fabrication |
US7713893B2 (en) * | 2004-12-08 | 2010-05-11 | Albany Engineered Composites, Inc. | Three-dimensional woven integrally stiffened panel |
FR2887601B1 (fr) | 2005-06-24 | 2007-10-05 | Snecma Moteurs Sa | Piece mecanique et procede de fabrication d'une telle piece |
US7943535B2 (en) * | 2005-11-17 | 2011-05-17 | Albany Engineered Composites, Inc. | Hybrid three-dimensional woven/laminated struts for composite structural applications |
FR2902802B1 (fr) * | 2006-06-21 | 2008-12-12 | Snecma Propulsion Solide Sa | Structure fibreuse de renfort pour piece en materiau composite et piece la comportant |
US20100119777A1 (en) * | 2006-11-16 | 2010-05-13 | Siemens Power Generation, Inc. | Ceramic matrix composite surfaces with open features for improved bonding to coatings |
US8058191B2 (en) * | 2008-09-04 | 2011-11-15 | Siemens Energy, Inc. | Multilayered ceramic matrix composite structure having increased structural strength |
US8079387B2 (en) * | 2008-10-29 | 2011-12-20 | Albany Engineered Composites, Inc. | Pi-shaped preform |
FR2939130B1 (fr) | 2008-11-28 | 2011-09-16 | Snecma Propulsion Solide | Procede de fabrication de piece de forme de forme complexe en materiau composite. |
FR2939153B1 (fr) * | 2008-11-28 | 2011-12-09 | Snecma Propulsion Solide | Realisation d'une structure fibreuse a epaisseur evolutive par tissage 3d |
US9080463B2 (en) * | 2009-03-09 | 2015-07-14 | Snecma | Turbine ring assembly |
CN201801711U (zh) * | 2010-09-26 | 2011-04-20 | 吴伯明 | 一种在四周边缘预留纱线的整体多层顶部织物 |
-
2012
- 2012-12-10 WO PCT/FR2012/052853 patent/WO2013088040A2/fr active Application Filing
- 2012-12-10 BR BR112014014244-0A patent/BR112014014244B1/pt active IP Right Grant
- 2012-12-10 US US14/365,369 patent/US10280537B2/en active Active
- 2012-12-10 JP JP2014546605A patent/JP6254533B2/ja active Active
- 2012-12-10 CN CN201280062069.6A patent/CN103998721B/zh active Active
- 2012-12-10 CA CA2858320A patent/CA2858320C/fr active Active
- 2012-12-10 RU RU2014128571A patent/RU2612927C2/ru active
- 2012-12-10 EP EP12821289.1A patent/EP2791473B1/fr active Active
-
2017
- 2017-05-25 US US15/605,417 patent/US10519576B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
EP2791473A2 (fr) | 2014-10-22 |
WO2013088040A3 (fr) | 2014-01-23 |
US10519576B2 (en) | 2019-12-31 |
CA2858320C (fr) | 2019-04-16 |
CN103998721A (zh) | 2014-08-20 |
RU2014128571A (ru) | 2016-02-10 |
JP6254533B2 (ja) | 2017-12-27 |
US10280537B2 (en) | 2019-05-07 |
CN103998721B (zh) | 2016-01-20 |
BR112014014244B1 (pt) | 2021-01-05 |
US20140349538A1 (en) | 2014-11-27 |
JP2015505916A (ja) | 2015-02-26 |
EP2791473B1 (fr) | 2019-02-06 |
WO2013088040A2 (fr) | 2013-06-20 |
RU2612927C2 (ru) | 2017-03-13 |
CA2858320A1 (fr) | 2013-06-20 |
US20170260661A1 (en) | 2017-09-14 |
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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 10/12/2012, OBSERVADAS AS CONDICOES LEGAIS. |