BR112013014578B1 - peça feita de material compósito que compreende um reforço fibroso densificado por uma matriz - Google Patents

peça feita de material compósito que compreende um reforço fibroso densificado por uma matriz Download PDF

Info

Publication number
BR112013014578B1
BR112013014578B1 BR112013014578-1A BR112013014578A BR112013014578B1 BR 112013014578 B1 BR112013014578 B1 BR 112013014578B1 BR 112013014578 A BR112013014578 A BR 112013014578A BR 112013014578 B1 BR112013014578 B1 BR 112013014578B1
Authority
BR
Brazil
Prior art keywords
arc
warp
shaped portion
fibrous structure
fibrous
Prior art date
Application number
BR112013014578-1A
Other languages
English (en)
Portuguese (pt)
Other versions
BR112013014578A2 (pt
Inventor
Thierry Godon
Bruno Jacques Gérard Dambrine
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 BR112013014578A2 publication Critical patent/BR112013014578A2/pt
Publication of BR112013014578B1 publication Critical patent/BR112013014578B1/pt

Links

Images

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
    • 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
    • B29C70/22—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 two directions forming a two-dimensional [2D] structure
    • B29C70/222—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 two directions forming a two-dimensional [2D] structure the structure being shaped to form a three dimensional configuration
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00—Woven fabrics designed to make specified articles
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D11/00—Double or multi-ply fabrics not otherwise provided for
    • D03D11/02—Fabrics formed with pockets, tubes, loops, folds, tucks or flaps
    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D13/00—Woven fabrics characterised by the special disposition of the warp or weft threads, e.g. with curved weft threads, with discontinuous warp threads, with diagonal warp or weft
    • D03D13/004—Woven fabrics characterised by the special disposition of the warp or weft threads, e.g. with curved weft threads, with discontinuous warp threads, with diagonal warp or weft with weave pattern being non-standard or providing special effects
    • 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
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • D10B2505/02—Reinforcing materials; Prepregs
    • 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
    • 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
    • Y10T428/00—Stock material or miscellaneous articles
    • Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479—Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612—Composite web or sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
BR112013014578-1A 2010-12-13 2011-12-05 peça feita de material compósito que compreende um reforço fibroso densificado por uma matriz BR112013014578B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1060408A FR2968679B1 (fr) 2010-12-13 2010-12-13 Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche
FR1060408 2010-12-13
PCT/FR2011/052868 WO2012080617A1 (fr) 2010-12-13 2011-12-05 Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche

Publications (2)

Publication Number Publication Date
BR112013014578A2 BR112013014578A2 (pt) 2016-09-20
BR112013014578B1 true BR112013014578B1 (pt) 2020-12-01

Family

ID=43821920

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112013014578-1A BR112013014578B1 (pt) 2010-12-13 2011-12-05 peça feita de material compósito que compreende um reforço fibroso densificado por uma matriz

Country Status (9)

Country Link
US (1) US9365956B2 (cg-RX-API-DMAC7.html)
EP (1) EP2652185B1 (cg-RX-API-DMAC7.html)
JP (1) JP6017445B2 (cg-RX-API-DMAC7.html)
CN (1) CN103261499B (cg-RX-API-DMAC7.html)
BR (1) BR112013014578B1 (cg-RX-API-DMAC7.html)
CA (1) CA2820415C (cg-RX-API-DMAC7.html)
FR (1) FR2968679B1 (cg-RX-API-DMAC7.html)
RU (1) RU2578996C2 (cg-RX-API-DMAC7.html)
WO (1) WO2012080617A1 (cg-RX-API-DMAC7.html)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2970715B1 (fr) * 2011-01-21 2014-10-17 Snecma Structure fibreuse tissee multicouches ayant une partie tubulaire creuse, procede de fabrication et piece composite la comportant
US9833930B2 (en) 2012-10-23 2017-12-05 Albany Engineered Composites, Inc. Circumferential stiffeners for composite fancases
FR3002548A1 (fr) * 2013-02-22 2014-08-29 Aircelle Sa Procede de tissage d’un tissu en relief, metier a tisser pour realiser le procede et preforme utilisant un tel tissu en relief
FR3002549B1 (fr) * 2013-02-22 2015-03-27 Aircelle Sa Metier a tisser a avance multiple, procede de tissage utilisant un tel metier a tisser et un tissu creneau ainsi obtenu.
FR3002547B1 (fr) * 2013-02-22 2015-07-17 Aircelle Sa Procede de tissage d’un tissu double creneau dans le sens chaine et preforme utilisant un tel tissu.
WO2014163676A1 (en) * 2013-03-13 2014-10-09 Lazur Andrew J Compliant composite component and method of manufacture
FR3009315B1 (fr) * 2013-07-30 2015-12-18 Aircelle Sa Procede de fabrication d'une preforme tissee pour une poutre en materiaux composites disposant de renforts interieurs transversaux
FR3018286B1 (fr) * 2014-03-10 2016-05-27 Aircelle Sa Preforme tissee pour realiser un renfort circonferentiel ou torique a section en omega
CN104264312B (zh) * 2014-09-10 2016-04-13 淄博银仕来纺织有限公司 宽幅管状织物的织造方法
FR3027549B1 (fr) * 2014-10-23 2017-09-08 Snecma Assemblage par un element d'ancrage mecanique entre deux pieces dont l'une est realisee en materiau composite
CN107002320B (zh) 2014-12-10 2018-11-09 内野株式会社 多层纱的制造方法和多层纱织品
JP6377568B2 (ja) * 2015-04-27 2018-08-22 株式会社オルセン 立体織物
FR3065231B1 (fr) * 2017-04-12 2020-03-27 Chamatex Tissu integrant au moins un element de liage
WO2019027717A1 (en) * 2017-07-31 2019-02-07 Dow Silicones Corporation DOUBLE CURABLE SILICONE COMPOSITIONS
BR112020007073B1 (pt) 2017-10-12 2023-12-19 Albany Engineered Composites, Inc Método para formar um enrijecedor tecido 3d
US20190285028A1 (en) * 2018-03-16 2019-09-19 Mra Systems, Llc. Thrust reverser cascade
JP6564971B2 (ja) * 2018-03-27 2019-08-28 株式会社オルセン 立体織物を用いた留付具およびこの留付具を用いたテント等の設営方法
FR3084088B1 (fr) * 2018-07-23 2020-10-02 Safran Texture fibreuse pour carter en materiau composite a resistance a l'impact amelioree
FR3092034B1 (fr) * 2019-01-30 2022-12-02 Safran Aircraft Engines Carter en matériau composite avec variation locale d’épaisseur
FR3120878B1 (fr) * 2021-03-17 2023-03-31 Safran Procédé de fabrication d’une pièce de turbomachine en matériau composite comportant une zone de rigidification
FR3136189B1 (fr) * 2022-06-02 2025-04-25 Safran Aircraft Engines Pièce en matériau composite à capacité d’absorption des chocs améliorée, et procédé de fabrication d’une telle pièce
US20260168142A1 (en) * 2024-12-18 2026-06-18 General Electric Company Method of manufacturing a woven fabric for a composite component

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6297938A (ja) * 1985-10-23 1987-05-07 敷島カンバス株式会社 立体成形用織物の製織方法
JPH0243893Y2 (cg-RX-API-DMAC7.html) * 1986-07-23 1990-11-21
EP0286004B1 (en) * 1987-03-31 1992-07-22 Asahi Kasei Kogyo Kabushiki Kaisha Woven fabric having multi-layer structure and composite material comprising the woven fabric
US5098756A (en) * 1989-01-25 1992-03-24 Henderson Mark P Elastic self-extinguishing strap material
US5080142A (en) * 1989-04-06 1992-01-14 Hitco Integrally woven multi-apertured multi-layer angle interlock fabrics
EP0481772B1 (en) * 1990-10-18 1996-08-28 Nippon Oil Company, Limited Tubular multilayer woven fabric and method for manufacturing the same
JPH05230735A (ja) * 1992-02-17 1993-09-07 Fukukou Orimono Kk 織物及びその製造方法
RU2117736C1 (ru) * 1997-01-23 1998-08-20 Акционерное общество закрытого типа "Русстек" Волокнистая основа для композиционного изоляционного и/или кровельного материала
FR2759096B1 (fr) * 1997-02-04 1999-02-26 Snecma Texture multicouche liee pour materiaux composites structuraux
CN1053613C (zh) * 1998-09-28 2000-06-21 天津纺织工学院 多层机织物复合材料及成型模具和方法
JP3730874B2 (ja) * 2001-02-13 2006-01-05 日本フイルコン株式会社 車両の走行補助織物
FR2887601B1 (fr) 2005-06-24 2007-10-05 Snecma Moteurs Sa Piece mecanique et procede de fabrication d'une telle piece
FR2902803B1 (fr) * 2006-06-21 2008-11-14 Snecma Propulsion Solide Sa Structure fibreuse de renfort pour piece en materiau composite et piece la comportant
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
FR2904167B1 (fr) * 2006-07-21 2008-10-17 Laudren Electronique Sarl Procede et dispositif de suppression d'echo dans un systeme de communication par digits
FR2939129B1 (fr) * 2008-11-28 2014-08-22 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.
FR2940167B1 (fr) * 2008-12-24 2012-12-21 Messier Dowty Sa Procede de liaison d'un element structurel en materiau composite a un tube.

Also Published As

Publication number Publication date
US9365956B2 (en) 2016-06-14
US20130270389A1 (en) 2013-10-17
EP2652185B1 (fr) 2015-06-24
FR2968679B1 (fr) 2014-02-07
RU2578996C2 (ru) 2016-03-27
JP6017445B2 (ja) 2016-11-02
CA2820415C (fr) 2018-03-20
CN103261499B (zh) 2014-12-31
BR112013014578A2 (pt) 2016-09-20
CA2820415A1 (fr) 2012-06-21
FR2968679A1 (fr) 2012-06-15
EP2652185A1 (fr) 2013-10-23
WO2012080617A1 (fr) 2012-06-21
JP2014506304A (ja) 2014-03-13
RU2013132219A (ru) 2015-01-20
CN103261499A (zh) 2013-08-21

Similar Documents

Publication Publication Date Title
JP6017445B2 (ja) １つ以上の弓形形状部を有する複合材料からなる部品用繊維構造
JP2014506304A5 (cg-RX-API-DMAC7.html)
BR112016000215B1 (pt) Pá de hélice de aeronave, motor aeronáutico, aeronave, e, processo de fabricação de uma pá de hélice de aeronave
JP6038178B2 (ja) 複合材料で作成され、プラットフォームが一体化されたタービンエンジンブレード用の繊維プリフォーム、およびそれを作成する方法
JP6734261B2 (ja) 有機マトリックスを伴う複合材料から成る自己補剛ケーシング
CN103415388B (zh) 包括固定装置的复合材料零件
CN102666277B (zh) 航空器螺旋桨叶片以及叶片的制造方法
JP6254532B2 (ja) 薄肉部を有する複合材料部品のための繊維補強構造
CN114728440B (zh) 用于制造风扇叶片的由复合材料制成的编织的纤维预成型件
BRPI1015161B1 (pt) processo de fabricação de uma pá de turbomáquina de material compósito com plataforma superior ou inferior integrada
BR112017017389B1 (pt) Método para fabricação de uma lâmina de turbo máquina
BR112014014488B1 (pt) Estrutura de fibra para reforçar uma peça de material compósito, peça de material compósito e método de fabricação de uma estrutura de fibra para reforçar uma peça de material compósito
US9382647B2 (en) Fibrous structure for a part made of a composite material and having a complex shape
BR112016019538B1 (pt) Processo de fabricação de peça de material compósito, e peça de estrutura
BR112018009047B1 (pt) Método para fabricação de uma peça de material compósito
BR112012007154B1 (pt) pré-forma tecida tridimensional, compósito reforçado com fibra e métodos de formação de pré-forma tecida tridimensional e de compósito reforçado com fibra
BR112017017462B1 (pt) Estrutura fibrosa, peça de material compósito, e, processo de fabricação de uma estrutura fibrosa.
BR112012006935B1 (pt) pré-forma tecida tridimensional, compósito reforçado de fibra, métodos de formação de pré-forma tecida tridimensional e de compósito reforçado com fibra
BR112015017494B1 (pt) Método de fabricação de uma estrutura alveolar curvada feita de material compósito
BR112016007194B1 (pt) Estrutura de fibra, e, métodos de fabricação de uma estrutura de fibra e de uma pré- forma de reforço de fibra
BR112020003874A2 (pt) estrutura fibrosa, pré-forma fibrosa, caixa de motor de turbina a gás, e, motor de turbina a gás de aeronave.
US20180127088A1 (en) Reinforced blade and spar
JP7678039B2 (ja) オメガ形状補強材の三次元織物プリフォーム
BRPI0919003B1 (pt) Elemento para uma aeronave compreendendo um painel sanduíche compósito

Legal Events

Date Code Title Description
B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B06T Formal requirements before examination [chapter 6.20 patent gazette]
B06A Patent application procedure suspended [chapter 6.1 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 05/12/2011, OBSERVADAS AS CONDICOES LEGAIS.