BR112015003567A2 - Método para fabricar partes de material compósito com pré-formas obtidas por tecelagem de contorno e instalação para fabricar as mesmas - Google Patents

Método para fabricar partes de material compósito com pré-formas obtidas por tecelagem de contorno e instalação para fabricar as mesmas

Info

Publication number
BR112015003567A2
BR112015003567A2 BR112015003567A BR112015003567A BR112015003567A2 BR 112015003567 A2 BR112015003567 A2 BR 112015003567A2 BR 112015003567 A BR112015003567 A BR 112015003567A BR 112015003567 A BR112015003567 A BR 112015003567A BR 112015003567 A2 BR112015003567 A2 BR 112015003567A2
Authority
BR
Brazil
Prior art keywords
preform
composite material
mandrel
phase
carried out
Prior art date
Application number
BR112015003567A
Other languages
English (en)
Inventor
Desjoyeaux Bertrand
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
Application filed by Aircelle Sa filed Critical Aircelle Sa
Publication of BR112015003567A2 publication Critical patent/BR112015003567A2/pt

Links

Classifications

    • 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
    • B29C70/28Shaping operations therefor
    • B29C70/30Shaping by lay-up, i.e. applying fibres, tape or broadsheet on a mould, former or core; Shaping by spray-up, i.e. spraying of fibres on a mould, former or core
    • 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
    • B29C70/02Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts comprising combinations of reinforcements, e.g. non-specified reinforcements, fibrous reinforcing inserts and fillers, e.g. particulate fillers, incorporated in matrix material, forming one or more layers and with or without non-reinforced or non-filled layers
    • B29C70/021Combinations of fibrous reinforcement and non-fibrous material
    • 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
    • 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
    • B29C70/28Shaping operations therefor
    • B29C70/40Shaping or impregnating by compression not applied
    • 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
    • B29C67/00Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00
    • B29C67/0014Shaping techniques not covered by groups B29C39/00 - B29C65/00, B29C70/00 or B29C73/00 for shaping tubes or blown tubular films
    • B29C67/0018Turning tubes inside out
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29KINDEXING 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
    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/25Solid
    • B29K2105/253Preform
    • B29K2105/258Tubular
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2023/00Tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29LINDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
    • B29L2031/00Other particular articles
    • B29L2031/772Articles characterised by their shape and not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Moulding By Coating Moulds (AREA)
  • Woven Fabrics (AREA)
  • Braiding, Manufacturing Of Bobbin-Net Or Lace, And Manufacturing Of Nets By Knotting (AREA)

Abstract

MÉTODO PARA FABRICAR PARTES DE MATERIAL COMPÓSITO COM PRÉ-FORMAS OBTIDAS POR TECELAGEM DE CONTORNO E INSTALAÇÃO PARA FABRICAR AS MESMAS. A presente invenção diz respeito a um método para fabricar partes compósitas. Também diz respeito a uma instalação de fabricação implementando tal método e para partes compósitas fabricadas desse modo. Ela encontra aplicação no campo da construção aeronáutica. Durante uma primeira fase, o projeto da parte, o cálculo da geometria e o layout de drapeado da pré-forma feita de tela e o cálculo de um mandril para formar um primeiro estado da pré-forma são realizados. Durante uma segunda fase, a produção de uma tela (21) da pré-forma e o mandril (20) calculado durante a primeira fase é realizada. Durante uma terceira fase, o enrolamento do mandril com a tela fabricada, a extração da pré-forma de seu mandril a fim de dobrar (R) uma porção (29b) da pré-forma, são realizados e, finalmente, a impregnação da pré-forma é realizada a fim de obter a parte de material compósito desejada.
BR112015003567A 2012-09-18 2013-09-17 Método para fabricar partes de material compósito com pré-formas obtidas por tecelagem de contorno e instalação para fabricar as mesmas BR112015003567A2 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1258720A FR2995557A1 (fr) 2012-09-18 2012-09-18 Procede de fabrication de pieces composites, installation de fabrication mettant en oeuvre un tel procede, et pieces composites ainsi fabriquees
PCT/FR2013/052133 WO2014044963A2 (fr) 2012-09-18 2013-09-17 Procédé de fabrication de pièces composites, installation de fabrication mettant en oeuvre un tel procédé, et pièces composites ainsi fabriquées

Publications (1)

Publication Number Publication Date
BR112015003567A2 true BR112015003567A2 (pt) 2017-08-15

Family

ID=47295003

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112015003567A BR112015003567A2 (pt) 2012-09-18 2013-09-17 Método para fabricar partes de material compósito com pré-formas obtidas por tecelagem de contorno e instalação para fabricar as mesmas

Country Status (8)

Country Link
US (1) US20150174833A1 (pt)
EP (1) EP2897784A2 (pt)
CN (1) CN104837608A (pt)
BR (1) BR112015003567A2 (pt)
CA (1) CA2881118A1 (pt)
FR (1) FR2995557A1 (pt)
RU (1) RU2015113957A (pt)
WO (1) WO2014044963A2 (pt)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3018286B1 (fr) * 2014-03-10 2016-05-27 Aircelle Sa Preforme tissee pour realiser un renfort circonferentiel ou torique a section en omega
DE102015205934B3 (de) * 2015-04-01 2016-09-22 Airbus Operations Gmbh Druckschott und Verfahren zur Herstellung eines Druckschotts
FR3048435B1 (fr) * 2016-03-02 2018-04-06 Safran Aircraft Engines Installation et procede pour la fabrication d'une texture fibreuse en forme de bande presentant en section transversale un profil evolutif
FR3053623B1 (fr) * 2016-07-06 2018-08-17 Safran Nacelles Procede de fabrication d’une preforme pour materiaux composites
FR3062659B1 (fr) * 2017-02-03 2019-03-22 Safran Aircraft Engines Appel de preforme dans un metier a tisser du type jacquard
DE102017208182A1 (de) * 2017-05-16 2018-11-22 Bayerische Motoren Werke Aktiengesellschaft Verfahren zum Festlegen einer geometrischen Form eines Kernbauteils für ein faserverstärktes Flechtbauteil, Kernbauteil für ein faserverstärktes Flechtbauteil sowie faserverstärktes Flechtbauteil
FR3071765B1 (fr) 2017-10-03 2020-11-20 Safran Ceram Realisation en materiau composite d'une structure a lobes de melangeur de flux
FR3085126B1 (fr) * 2018-08-27 2020-09-11 Safran Nacelles Procede de fabrication d'une preforme composite pour la fabrication d'un panneau composite a geometrie a double courbure
FR3098225B1 (fr) * 2019-07-03 2021-07-16 3Ditex Dispositif de realisation d'une preforme en 3d, procede de realisation en 3d avec ledit dispositif, preforme en 3d ainsi obtenue
CN114248463B (zh) * 2020-09-21 2024-07-23 江苏金风科技有限公司 纤维织物及其治具和制造方法
FR3116466B1 (fr) * 2020-11-25 2022-11-25 Safran Ceram Préforme fibreuse d'un profil aérodynamique d'aube de turbomachine
CN113085222B (zh) * 2021-04-01 2023-03-21 湖北航泰科技有限公司 一种复合材料增强件及成型工艺方法
DE102021109699A1 (de) * 2021-04-16 2022-10-20 Airbus Operations Gmbh Verfahren zum Herstellen von Verbundbauteilen mit einer nicht-abwickelbaren Oberfläche
FR3126640A1 (fr) * 2021-09-03 2023-03-10 Safran Outillage pour l’enroulement d’une texture fibreuse et procédé d’enroulement associé
FR3129392B1 (fr) * 2021-11-22 2023-11-17 Safran Ceram Procédé d’obtention d’une pièce en matériau composite à matrice céramique.

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4534813A (en) * 1982-07-26 1985-08-13 Mcdonnell Douglas Corporation Compound curve-flat pattern process
CN1056800C (zh) * 1994-12-20 2000-09-27 波音公司 手动辅助操作层压系统
DE102004017418A1 (de) * 2004-04-08 2005-11-03 Grundfos A/S Verfahren zum Herstellen eines formstabilen, hohlkörperförmigen Elementes mit einem Bodenbereich und Verwendung eines solchen Elementes
DE102005041940B4 (de) * 2005-08-30 2013-01-31 ThyssenKrupp Carbon Components GmbH Rad aus Faserverbundwerkstoff sowie Verfahren zu dessen Herstellung
NZ561410A (en) * 2007-09-11 2010-04-30 Parker Hannifin Gmbh End-fittings for composite tubes, method for joining fittings to the ends of composite tubes and composite tubes incorporating end-fittings
US9017814B2 (en) * 2007-10-16 2015-04-28 General Electric Company Substantially cylindrical composite articles and fan casings
FR2935990B1 (fr) * 2008-09-17 2011-05-13 Aircelle Sa Procede de fabrication d'une piece en materiau composite a matrice metallique
US20130269159A1 (en) * 2010-11-03 2013-10-17 University Of Ottawa Novel composite parts, methods and apparatus for manufacturing the same
DE102010053635B4 (de) * 2010-12-07 2017-05-11 Hero Gmbh Verfahren zur Herstellung eines Faserverbundprodukts

Also Published As

Publication number Publication date
EP2897784A2 (fr) 2015-07-29
US20150174833A1 (en) 2015-06-25
CA2881118A1 (fr) 2014-03-27
WO2014044963A2 (fr) 2014-03-27
FR2995557A1 (fr) 2014-03-21
RU2015113957A (ru) 2016-11-10
CN104837608A (zh) 2015-08-12
WO2014044963A3 (fr) 2014-05-08

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]
B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2433 DE 22-08-2017 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.

B350 Update of information on the portal [chapter 15.35 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]