FR2993492B1 - Procede de fabrication d'une piece composite en t par moulage par transfert de resine - Google Patents

Procede de fabrication d'une piece composite en t par moulage par transfert de resine

Info

Publication number
FR2993492B1
FR2993492B1 FR1257069A FR1257069A FR2993492B1 FR 2993492 B1 FR2993492 B1 FR 2993492B1 FR 1257069 A FR1257069 A FR 1257069A FR 1257069 A FR1257069 A FR 1257069A FR 2993492 B1 FR2993492 B1 FR 2993492B1
Authority
FR
France
Prior art keywords
piece
transfer molding
resin transfer
manufacturing composite
composite
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
FR1257069A
Other languages
English (en)
Other versions
FR2993492A1 (fr
Inventor
Didier Leretour
Sebastien Louchard
Laurent Dubois
Claire Dupuis
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 Nacelles SAS
Original Assignee
Aircelle SA
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
Priority to FR1257069A priority Critical patent/FR2993492B1/fr
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to EP13744738.9A priority patent/EP2874799A1/fr
Priority to CN201380038575.6A priority patent/CN104470707A/zh
Priority to CA2879135A priority patent/CA2879135A1/fr
Priority to RU2015105002A priority patent/RU2015105002A/ru
Priority to BR112015001202A priority patent/BR112015001202A2/pt
Priority to PCT/FR2013/051673 priority patent/WO2014013167A1/fr
Publication of FR2993492A1 publication Critical patent/FR2993492A1/fr
Application granted granted Critical
Publication of FR2993492B1 publication Critical patent/FR2993492B1/fr
Priority to US14/598,546 priority patent/US20150125654A1/en
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
    • 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
    • B29C70/28—Shaping operations therefor
    • B29C70/40—Shaping or impregnating by compression not applied
    • B29C70/42—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs
    • B29C70/48—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using matched moulds, e.g. for deforming sheet moulding compounds [SMC] or prepregs and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM], e.g. by vacuum
    • 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
    • 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
    • B29C70/28—Shaping operations therefor
    • B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
    • B29C70/543—Fixing the position or configuration of fibrous reinforcements before or during moulding
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D99/00—Subject matter not provided for in other groups of this subclass
    • B29D99/0003—Producing profiled members, e.g. beams
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/02—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions
    • B32B3/08—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by features of form at particular places, e.g. in edge regions characterised by added members at particular parts
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/26—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
    • B32B3/263—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by a layer having non-uniform thickness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/06—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts
    • B29K2105/08—Condition, form or state of moulded material or of the material to be shaped containing reinforcements, fillers or inserts of continuous length, e.g. cords, rovings, mats, fabrics, strands or yarns
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2307/00—Use of elements other than metals as reinforcement
    • B29K2307/04—Carbon
    • 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
    • B29L2031/001—Profiled members, e.g. beams, sections
    • B29L2031/003—Profiled members, e.g. beams, sections having a profiled transverse cross-section
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
    • 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.]
    • Y10T428/24174—Structurally defined web or sheet [e.g., overall dimension, etc.] including sheet or component perpendicular to plane of web or sheet
    • Y10T428/24182—Inward from edge of web or sheet

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Injection Moulding Of Plastics Or The Like (AREA)
FR1257069A 2012-07-20 2012-07-20 Procede de fabrication d'une piece composite en t par moulage par transfert de resine Active FR2993492B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR1257069A FR2993492B1 (fr) 2012-07-20 2012-07-20 Procede de fabrication d'une piece composite en t par moulage par transfert de resine
CN201380038575.6A CN104470707A (zh) 2012-07-20 2013-07-12 通过树脂传递模塑制造t形复合部件的方法
CA2879135A CA2879135A1 (fr) 2012-07-20 2013-07-12 Procede de fabrication d'une piece composite en t par moulage par transfert de resine
RU2015105002A RU2015105002A (ru) 2012-07-20 2013-07-12 Способ изготовления т-образной композитной детали путем инжекции смолы в закрытую форму
EP13744738.9A EP2874799A1 (fr) 2012-07-20 2013-07-12 Procédé de fabrication d'une pièce composite en t par moulage par transfert de résine
BR112015001202A BR112015001202A2 (pt) 2012-07-20 2013-07-12 método para a fabricação de uma parte de compósito em formato de t por moldagem de transferência de resina e parte de compósito em formato de t.
PCT/FR2013/051673 WO2014013167A1 (fr) 2012-07-20 2013-07-12 Procédé de fabrication d'une pièce composite en t par moulage par transfert de résine
US14/598,546 US20150125654A1 (en) 2012-07-20 2015-01-16 Method for manufacturing a t-shaped composite part by resin-transfer molding

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1257069A FR2993492B1 (fr) 2012-07-20 2012-07-20 Procede de fabrication d'une piece composite en t par moulage par transfert de resine

Publications (2)

Publication Number Publication Date
FR2993492A1 FR2993492A1 (fr) 2014-01-24
FR2993492B1 true FR2993492B1 (fr) 2014-07-18

Family

ID=47049267

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1257069A Active FR2993492B1 (fr) 2012-07-20 2012-07-20 Procede de fabrication d'une piece composite en t par moulage par transfert de resine

Country Status (8)

Country Link
US (1) US20150125654A1 (fr)
EP (1) EP2874799A1 (fr)
CN (1) CN104470707A (fr)
BR (1) BR112015001202A2 (fr)
CA (1) CA2879135A1 (fr)
FR (1) FR2993492B1 (fr)
RU (1) RU2015105002A (fr)
WO (1) WO2014013167A1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102015201348A1 (de) * 2015-01-27 2016-07-28 Bayerische Motoren Werke Aktiengesellschaft Verfahren zum Ausbilden eines Funktionsabschnitts an einem Faserverbundbauteil
FR3036060B1 (fr) 2015-05-12 2017-04-28 Aircelle Sa Piece en materiau composite comportant un raidisseur en t et procede de fabrication d'une telle piece
FR3043356B1 (fr) 2015-11-09 2018-08-31 Safran Nacelles Piece en materiau composite comportant un renfort contre le delaminage et son procede de fabrication

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2687174B1 (fr) * 1992-02-11 1995-09-22 Aerospatiale Procede pour la realisation d'une armature de fibres pour piece de matiere composite a parois non coplanaires, et piece composite comportant une telle armature.
FR2687173B1 (fr) * 1992-02-11 1995-09-08 Aerospatiale Procede pour la realisation d'une armature de fibres pour piece de matiere composite, et piece composite comportant une telle armature.
US5789061A (en) * 1996-02-13 1998-08-04 Foster-Miller, Inc. Stiffener reinforced assembly and method of manufacturing same
FR2929167B1 (fr) * 2008-03-27 2010-04-23 Airbus France Procede de fabrication d'un flan en materiau composite thermoplastique, outillage de fabrication associe et application du procede a la realisation de pieces de structure d'aeronef
FR2945847B1 (fr) * 2009-05-20 2011-12-02 Messier Dowty Sa Procede de fabrication d'une bielle en materiau composite et bielle obtenue par la mise en oeuvre dudit procede.
EP2384884A1 (fr) * 2010-05-07 2011-11-09 Eurocopter Deutschland GmbH Procédé de fabrication d'une pièce composite renforcée et pièce composite renforcée obtenue selon ledit procédé

Also Published As

Publication number Publication date
WO2014013167A1 (fr) 2014-01-23
EP2874799A1 (fr) 2015-05-27
CN104470707A (zh) 2015-03-25
RU2015105002A (ru) 2016-09-10
CA2879135A1 (fr) 2014-01-23
BR112015001202A2 (pt) 2017-08-01
US20150125654A1 (en) 2015-05-07
FR2993492A1 (fr) 2014-01-24

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