ES2085020T3 - Metodo para la produccion de una estructura composite con un textil tridimensional intermedio, y una estructura hecha mediante el metodo. - Google Patents

Metodo para la produccion de una estructura composite con un textil tridimensional intermedio, y una estructura hecha mediante el metodo.

Info

Publication number
ES2085020T3
ES2085020T3 ES92913245T ES92913245T ES2085020T3 ES 2085020 T3 ES2085020 T3 ES 2085020T3 ES 92913245 T ES92913245 T ES 92913245T ES 92913245 T ES92913245 T ES 92913245T ES 2085020 T3 ES2085020 T3 ES 2085020T3
Authority
ES
Spain
Prior art keywords
dies
fibers
textile material
resin
dimensional textile
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.)
Expired - Lifetime
Application number
ES92913245T
Other languages
English (en)
Inventor
Marco Fantino
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.)
Metalleido Srl
Original Assignee
Metalleido Srl
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 Metalleido Srl filed Critical Metalleido Srl
Application granted granted Critical
Publication of ES2085020T3 publication Critical patent/ES2085020T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/08Impregnating
    • 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
    • B29C70/08Fibrous reinforcements only comprising combinations of different forms of fibrous reinforcements incorporated in matrix material, forming one or more layers, and with or without non-reinforced layers
    • 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
    • B29C70/24Fibrous 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
    • 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
    • B29C70/42Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles
    • B29C70/46Shaping 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
    • B29C70/467Shaping 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 during mould closing
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29DPRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
    • B29D24/00Producing articles with hollow walls
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B37/00Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the pressing technique, e.g. using action of vacuum or fluid pressure
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B32LAYERED PRODUCTS
    • B32BLAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B38/00Ancillary operations in connection with laminating processes
    • B32B38/18Handling of layers or the laminate
    • B32B38/1858Handling of layers or the laminate using vacuum

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Textile Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Reinforced Plastic Materials (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Woven Fabrics (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Laser Beam Processing (AREA)
  • Nitrogen And Oxygen Or Sulfur-Condensed Heterocyclic Ring Systems (AREA)
  • Peptides Or Proteins (AREA)
  • Preparation Of Compounds By Using Micro-Organisms (AREA)
  • Chemical Or Physical Treatment Of Fibers (AREA)
  • Measuring Or Testing Involving Enzymes Or Micro-Organisms (AREA)
  • Blow-Moulding Or Thermoforming Of Plastics Or The Like (AREA)

Abstract

UN MATERIAL TEXTIL TRIDIMENSIONAL (3) FORMADO A PARTIR DE DOS HOJAS DE UN MATERIAL TEXTIL (5, 6) COLOCADAS CARA A CARA Y CONECTADAS ENTRE SI MEDIANTE UNA PLURALIDAD DE FIBRAS EXTENSIBLES (10), SE IMPREGNA CON RESINA Y SE COLOCA ENTRE DOS CAPAS (16, 17) PARA ASI FORMAR UNA ESTRUCTURA ESTRATIFICADA (19). ESTA ESTRUCTURA ESTRATIFICADA (1) SE INSERTA ENTRE DOS TROQUELES (25, 26) DE UNA PRENSA CALENTADA QUE DESPUES SE CIERRA PERMITIR QUE LA RESINA QUE IMPREGNA LA ESTRUCTURA SE DISTRIBUYA UNIFORMEMENTE. A CONTINUACION SE UNEN LAS CAPAS (16, 17) MEDIANTE VACIO A LAS CARAS DE LOS TROQUELES (25, 26) QUE SE ABREN AHORA UNA PRIMERA DISTANCIA CONTROLADA DENTRO DEL LIMITE DE RECUPERACION ELASTICA DEL MATERIAL TEXTIL TRIDIMENSIONAL (3). A CONTINUACION SE POLIMERIZAN LAS CARAS EXTERIORES DE LA ESTRUCTURA (1) A BASE DE CALENTAR LOS TROQUELES (25, 26) MIENTRAS QUE LA RESINA QUE IMPREGNA LAS FIBRAS (10) PERMANECE EN UN ESTADO PLASTICO. ENTONCES SE LIBERA EL TROQUEL INFERIOR (25) AL PLANO EN QUE QUEDA TENDIDOY LOS TROQUELES (25, 26) SE SEPARAN A UNA SEGUNDA DISTANCIA TAL QUE SE ESTIREN LAS FIBRAS DEL MATERIAL TEXTIL TRIDIMENSIONAL Y QUEDEN ALINEADAS SUSTANCIALMENTE EN VERTICAL; ENTONCES SE BLOQUEA EL TROQUEL FLOTANTE (25, 26). A CONTINUACION SE SEPARAN LOS TROQUELES (25, 26) A UNA DISTANCIA PREDETERMINADA UNO DE OTRO PARA EXTENDER LAS FIBRAS (10) COMPLETAMENTE Y SE MANTIENE A LA PRENSA (28) EN ESTA POSICION HASTA QUE TODA LA RESINA SE HAYA POLIMERIZADO COMPLETAMENTE, ENDURECIENDOSE LA ESTRUCTURA EN LA POSICION ASUMIDA.
ES92913245T 1991-05-29 1992-05-28 Metodo para la produccion de una estructura composite con un textil tridimensional intermedio, y una estructura hecha mediante el metodo. Expired - Lifetime ES2085020T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITTO910397A IT1245753B (it) 1991-05-29 1991-05-29 Procedimento per la realizzazione di una struttura composita con tessuto intermedio tridimensionale ,e struttura realizzata mediante il procedimento stesso

Publications (1)

Publication Number Publication Date
ES2085020T3 true ES2085020T3 (es) 1996-05-16

Family

ID=11409378

Family Applications (1)

Application Number Title Priority Date Filing Date
ES92913245T Expired - Lifetime ES2085020T3 (es) 1991-05-29 1992-05-28 Metodo para la produccion de una estructura composite con un textil tridimensional intermedio, y una estructura hecha mediante el metodo.

Country Status (22)

Country Link
US (1) US5580412A (es)
EP (1) EP0591324B1 (es)
JP (1) JP3421789B2 (es)
KR (1) KR100220543B1 (es)
AT (1) ATE133371T1 (es)
AU (1) AU658653B2 (es)
BR (1) BR9206058A (es)
CA (1) CA2110051C (es)
CZ (1) CZ285702B6 (es)
DE (1) DE69207906T2 (es)
DK (1) DK0591324T3 (es)
ES (1) ES2085020T3 (es)
FI (1) FI103025B1 (es)
GR (1) GR3019072T3 (es)
HU (1) HU215370B (es)
IT (1) IT1245753B (es)
NO (1) NO303165B1 (es)
PL (1) PL168866B1 (es)
RU (1) RU2093362C1 (es)
SK (1) SK279043B6 (es)
UA (1) UA26323C2 (es)
WO (1) WO1992021511A1 (es)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1245753B (it) * 1991-05-29 1994-10-14 Metalleido Srl Procedimento per la realizzazione di una struttura composita con tessuto intermedio tridimensionale ,e struttura realizzata mediante il procedimento stesso
US5508096A (en) * 1994-03-16 1996-04-16 Aerotrans Integral composite structure incorporating multiple resin-based systems and method of manufacture
WO1995035201A1 (en) * 1994-06-21 1995-12-28 Metalleido S.R.L. Continuous forming method and device for a composite structure, in particular a composite structure featuring tree-dimensional fabric
DE19821840C1 (de) * 1998-05-15 2000-02-17 Von Roll Isola Gmbh Verfahren zur Herstellung einer Sandwichplatte
DE19825402C1 (de) * 1998-05-27 2000-02-10 Abb Daimler Benz Transp Selbsttragendes Formteil für mechanisch und korrosiv hochbeanspruchte, gekrümmt ausgebildete Bauteile eines Schienenfahrzeuges
US7048985B2 (en) * 2001-07-23 2006-05-23 Vrac, Llc Three-dimensional spacer fabric resin infusion media and reinforcing composite lamina
US7060156B2 (en) * 2001-07-23 2006-06-13 Vrac, Llc Three-dimensional spacer fabric resin interlaminar infusion media process and vacuum-induced reinforcing composite laminate structures
NZ532360A (en) * 2001-09-17 2005-12-23 Verdant Technologies Inc Three-dimensional knit spacer fabric sandwich composite
AUPR821401A0 (en) * 2001-10-11 2001-11-01 Cooperative Research Centre For Advanced Composite Structures Ltd Method of manufacturing composite sandwich structures
DE102005024408A1 (de) 2005-05-27 2006-11-30 Airbus Deutschland Gmbh Verstärkung von Schaumwerkstoffen
KR101332539B1 (ko) * 2006-03-08 2013-11-22 도레이 카부시키가이샤 섬유 강화 수지의 제조 방법
DE102007055684A1 (de) 2007-11-21 2009-06-10 Airbus Deutschland Gmbh Vorrichtung zur Herstellung eines verstärkten Schaumwerkstoffes
ITMI20080971A1 (it) * 2008-05-26 2009-11-27 Nat Style Ltd Dispositivo e procedimento di produzione in continuo di un tessuto tridimensionale per la produzione di pannelli.
CN201357532Y (zh) * 2009-03-13 2009-12-09 苏州红枫风电模具有限公司 模具电加热和空气冷却系统
GB0913171D0 (en) * 2009-07-29 2009-09-02 Airbus Operations Ltd Adjustable shim
FR2958875B1 (fr) * 2010-04-20 2017-07-07 Snecma Dispositif de fabrication d'un carter en materiau composite et procede de fabrication mettant en oeuvre un tel dispositif
FR2981000B1 (fr) * 2011-10-06 2013-11-29 Snecma Dispositif pour la fabrication d'une piece en materiau composite
FR3024959B1 (fr) * 2014-08-21 2016-09-09 Snecma Procede et ensemble de fabrication d'aube composite
CA2942625C (en) * 2014-03-13 2022-12-13 Abet Laminati S.P.A. Method for making a composite board
CN105134849B (zh) * 2015-08-13 2018-03-13 北京勤达远致新材料科技股份有限公司 一种三维编织复合材料汽车板簧及其制备方法
CN113696509B (zh) * 2021-08-06 2022-10-04 南京航空航天大学 一种超混杂面板/三维编织中空夹层复合材料的一体化成型方法

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3045319A (en) * 1961-01-25 1962-07-24 Wimpfheimer & Bro Inc A Resin molded fabric
AT296622B (de) * 1967-07-04 1972-02-25 Bayer Ag Hochbeanspruchbarer Schaumstoffkörper
US3592435A (en) * 1968-09-09 1971-07-13 Mattingly Inc Form structure
US4318682A (en) * 1980-09-05 1982-03-09 Ex-Cell-O Corporation Press locking apparatus
DE3101022A1 (de) * 1981-01-15 1982-08-05 Hoechst Ag, 6000 Frankfurt "formstabiles verbundmaterial und verfahren zu seiner herstellung"
US4420359A (en) * 1981-08-05 1983-12-13 Goldsworthy Engineering, Inc. Apparatus for producing fiber-reinforced plastic sheet structures
US4551085A (en) * 1983-04-25 1985-11-05 The Budd Company Compression molding apparatus having vacuum chamber
US4786351A (en) * 1985-12-31 1988-11-22 Astechnologies, Inc. Process and apparatus for simultaneously shaping foam and laminating fabric thereto
IT1208428B (it) * 1987-05-05 1989-06-12 Alusuisse Italia S P A Ferrari Elemento strutturale portante composito e procedimento per la sua fabbricazione in particolare per la realizzazione di carrozzerie di veicoli
JPH0239927A (ja) * 1988-07-29 1990-02-08 Mitsubishi Rayon Co Ltd 積層体の製造方法
US4879152A (en) * 1989-02-15 1989-11-07 Green Patrick H Composite panel structure
IT1245753B (it) * 1991-05-29 1994-10-14 Metalleido Srl Procedimento per la realizzazione di una struttura composita con tessuto intermedio tridimensionale ,e struttura realizzata mediante il procedimento stesso

Also Published As

Publication number Publication date
FI935283A0 (fi) 1993-11-26
BR9206058A (pt) 1994-11-15
GR3019072T3 (en) 1996-05-31
JP3421789B2 (ja) 2003-06-30
HU9303336D0 (en) 1994-03-28
CZ256593A3 (en) 1994-03-16
SK132093A3 (en) 1994-05-11
KR100220543B1 (ko) 1999-09-15
DK0591324T3 (da) 1996-03-25
HU215370B (hu) 1998-12-28
AU658653B2 (en) 1995-04-27
FI103025B (fi) 1999-04-15
JPH06507856A (ja) 1994-09-08
CA2110051C (en) 2004-02-17
IT1245753B (it) 1994-10-14
RU2093362C1 (ru) 1997-10-20
NO934305L (no) 1994-01-28
CZ285702B6 (cs) 1999-10-13
EP0591324A1 (en) 1994-04-13
ITTO910397A1 (it) 1992-11-29
DE69207906T2 (de) 1996-08-01
PL168866B1 (pl) 1996-04-30
NO303165B1 (no) 1998-06-08
ITTO910397A0 (it) 1991-05-29
EP0591324B1 (en) 1996-01-24
UA26323C2 (uk) 1999-08-30
CA2110051A1 (en) 1992-12-10
NO934305D0 (no) 1993-11-26
HUT67318A (en) 1995-03-28
ATE133371T1 (de) 1996-02-15
AU2150892A (en) 1993-01-08
DE69207906D1 (de) 1996-03-07
WO1992021511A1 (en) 1992-12-10
FI935283A (fi) 1993-11-26
SK279043B6 (sk) 1998-06-03
FI103025B1 (fi) 1999-04-15
US5580412A (en) 1996-12-03

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