CN103261499B - 用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构 - Google Patents

用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构 Download PDF

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Publication number
CN103261499B
CN103261499B CN201180059797.7A CN201180059797A CN103261499B CN 103261499 B CN103261499 B CN 103261499B CN 201180059797 A CN201180059797 A CN 201180059797A CN 103261499 B CN103261499 B CN 103261499B
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CN
China
Prior art keywords
fibre structure
warp thread
arcuate part
composite material
material parts
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CN201180059797.7A
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English (en)
Chinese (zh)
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CN103261499A (zh
Inventor
蒂里·戈登
布鲁诺·杰克斯·杰拉德·达米布瑞恩
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Safran Aircraft Engines SAS
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SNECMA SAS
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Publication of CN103261499A publication Critical patent/CN103261499A/zh
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29BPREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
    • B29B11/00Making preforms
    • B29B11/14Making preforms characterised by structure or composition
    • B29B11/16Making preforms characterised by structure or composition comprising fillers or reinforcement
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C70/00Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
    • B29C70/04Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising reinforcements only, e.g. self-reinforcing plastics
    • B29C70/06Fibrous reinforcements only
    • B29C70/10Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres
    • B29C70/16Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length
    • B29C70/22Fibrous 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 structure
    • B29C70/222Fibrous 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 structure the structure being shaped to form a three dimensional configuration
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/402Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D1/00Woven fabrics designed to make specified articles
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D11/00Double or multi-ply fabrics not otherwise provided for
    • D03D11/02Fabrics formed with pockets, tubes, loops, folds, tucks or flaps
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D13/00Woven 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
    • D03D13/004Woven 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
    • DTEXTILES; PAPER
    • D03WEAVING
    • D03DWOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D25/00Woven fabrics not otherwise provided for
    • D03D25/005Three-dimensional woven fabrics
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24Casings; Casing parts, e.g. diaphragms, casing fastenings
    • DTEXTILES; PAPER
    • D10INDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10BINDEXING SCHEME ASSOCIATED WITH SUBLASSES OF SECTION D, RELATING TO TEXTILES
    • D10B2505/00Industrial
    • D10B2505/02Reinforcing materials; Prepregs
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2300/00Materials; Properties thereof
    • F05D2300/60Properties or characteristics given to material by treatment or manufacturing
    • F05D2300/603Composites; e.g. fibre-reinforced
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient propulsion technologies, e.g. for aircraft
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/24Structurally defined web or sheet [e.g., overall dimension, etc.]
    • Y10T428/24479Structurally defined web or sheet [e.g., overall dimension, etc.] including variation in thickness
    • Y10T428/24612Composite web or sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
CN201180059797.7A 2010-12-13 2011-12-05 用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构 Active CN103261499B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1060408 2010-12-13
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
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
CN103261499A CN103261499A (zh) 2013-08-21
CN103261499B true CN103261499B (zh) 2014-12-31

Family

ID=43821920

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201180059797.7A Active CN103261499B (zh) 2010-12-13 2011-12-05 用于具有一个或多个拱形部分的由复合材料制成的零件的纤维结构

Country Status (9)

Country Link
US (1) US9365956B2 (enExample)
EP (1) EP2652185B1 (enExample)
JP (1) JP6017445B2 (enExample)
CN (1) CN103261499B (enExample)
BR (1) BR112013014578B1 (enExample)
CA (1) CA2820415C (enExample)
FR (1) FR2968679B1 (enExample)
RU (1) RU2578996C2 (enExample)
WO (1) WO2012080617A1 (enExample)

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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
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.
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
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.
EP2971558A1 (en) 2013-03-13 2016-01-20 Rolls-Royce Corporation 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
WO2016092652A1 (ja) 2014-12-10 2016-06-16 内野株式会社 多重ガーゼの製織方法および多重ガーゼ織物
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
JP7231612B2 (ja) * 2017-07-31 2023-03-01 ダウ シリコーンズ コーポレーション 二重硬化性シリコーン組成物
EP4345200B1 (en) 2017-10-12 2025-09-24 Albany Engineered Composites, Inc. Three-dimensional woven preforms for omega stiffeners
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

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EP0391745A1 (en) * 1989-04-06 1990-10-10 Bp Chemicals ( Hitco) Inc. Integrally woven multi-apertured multi-layer angle interlock fabrics
US5098756A (en) * 1989-01-25 1992-03-24 Henderson Mark P Elastic self-extinguishing strap material
CN1216785A (zh) * 1998-09-28 1999-05-19 天津纺织工学院 多层机织物复合材料及成型模具和方法
US6955192B2 (en) * 2001-02-13 2005-10-18 Nippon Filcon Co., Ltd. Vehicle running assisting fabric
FR2904167A1 (fr) * 2006-07-21 2008-01-25 Laudren Electronique Sarl Procede et dispositif de suppression d'echo dans un systeme de communication par digits
CN101473079A (zh) * 2006-06-21 2009-07-01 斯奈克玛动力部件公司 用于制造复合材料部件的纤维增强结构
CN101473078A (zh) * 2006-06-21 2009-07-01 斯奈克玛动力部件公司 用于复合材料部件的具有复缎编织的增强纤维结构
FR2939129A1 (fr) * 2008-11-28 2010-06-04 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.

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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 (enExample) * 1986-07-23 1990-11-21
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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
FR2887601B1 (fr) 2005-06-24 2007-10-05 Snecma Moteurs Sa Piece mecanique et procede de fabrication d'une telle piece
FR2940167B1 (fr) * 2008-12-24 2012-12-21 Messier Dowty Sa Procede de liaison d'un element structurel en materiau composite a un tube.

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5098756A (en) * 1989-01-25 1992-03-24 Henderson Mark P Elastic self-extinguishing strap material
EP0391745A1 (en) * 1989-04-06 1990-10-10 Bp Chemicals ( Hitco) Inc. Integrally woven multi-apertured multi-layer angle interlock fabrics
CN1216785A (zh) * 1998-09-28 1999-05-19 天津纺织工学院 多层机织物复合材料及成型模具和方法
US6955192B2 (en) * 2001-02-13 2005-10-18 Nippon Filcon Co., Ltd. Vehicle running assisting fabric
CN101473079A (zh) * 2006-06-21 2009-07-01 斯奈克玛动力部件公司 用于制造复合材料部件的纤维增强结构
CN101473078A (zh) * 2006-06-21 2009-07-01 斯奈克玛动力部件公司 用于复合材料部件的具有复缎编织的增强纤维结构
FR2904167A1 (fr) * 2006-07-21 2008-01-25 Laudren Electronique Sarl Procede et dispositif de suppression d'echo dans un systeme de communication par digits
FR2939129A1 (fr) * 2008-11-28 2010-06-04 Snecma Propulsion Solide Aube de turbomachine en materiau composite et procede pour sa fabrication.

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Also Published As

Publication number Publication date
BR112013014578B1 (pt) 2020-12-01
FR2968679B1 (fr) 2014-02-07
RU2578996C2 (ru) 2016-03-27
FR2968679A1 (fr) 2012-06-15
RU2013132219A (ru) 2015-01-20
EP2652185B1 (fr) 2015-06-24
CA2820415C (fr) 2018-03-20
JP2014506304A (ja) 2014-03-13
US20130270389A1 (en) 2013-10-17
EP2652185A1 (fr) 2013-10-23
BR112013014578A2 (pt) 2016-09-20
JP6017445B2 (ja) 2016-11-02
CA2820415A1 (fr) 2012-06-21
WO2012080617A1 (fr) 2012-06-21
CN103261499A (zh) 2013-08-21
US9365956B2 (en) 2016-06-14

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