CA2820415C - Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche - Google Patents

Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche Download PDF

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Publication number
CA2820415C
CA2820415C CA2820415A CA2820415A CA2820415C CA 2820415 C CA2820415 C CA 2820415C CA 2820415 A CA2820415 A CA 2820415A CA 2820415 A CA2820415 A CA 2820415A CA 2820415 C CA2820415 C CA 2820415C
Authority
CA
Canada
Prior art keywords
arch
fibrous structure
shaped portion
layers
fibrous
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
CA2820415A
Other languages
English (en)
French (fr)
Other versions
CA2820415A1 (fr
Inventor
Thierry Godon
Bruno Jacques Gerard Dambrine
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SAS filed Critical SNECMA SAS
Publication of CA2820415A1 publication Critical patent/CA2820415A1/fr
Application granted granted Critical
Publication of CA2820415C publication Critical patent/CA2820415C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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 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 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)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • General Engineering & Computer Science (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
CA2820415A 2010-12-13 2011-12-05 Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche Active CA2820415C (fr)

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
CA2820415A1 CA2820415A1 (fr) 2012-06-21
CA2820415C true CA2820415C (fr) 2018-03-20

Family

ID=43821920

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2820415A Active CA2820415C (fr) 2010-12-13 2011-12-05 Structure fibreuse pour piece en materiau composite ayant une ou plusieurs parties en forme d'arche

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)

Families Citing this family (21)

* 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
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

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 (enExample) * 1986-07-23 1990-11-21
CA1286588C (en) * 1987-03-31 1991-07-23 Koji Takenaka 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
DE69121662T2 (de) * 1990-10-18 1997-01-23 Nippon Oil Co Ltd Mehrschichtiges schlauchartiges Gewebe und Verfahren zu dessen Herstellung
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
BR112013014578B1 (pt) 2020-12-01
FR2968679B1 (fr) 2014-02-07
RU2578996C2 (ru) 2016-03-27
CN103261499B (zh) 2014-12-31
FR2968679A1 (fr) 2012-06-15
RU2013132219A (ru) 2015-01-20
EP2652185B1 (fr) 2015-06-24
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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Effective date: 20161121