ES8707891A1 - Procedimiento para fabricar una pieza hueca con una forma cualquiera - Google Patents

Procedimiento para fabricar una pieza hueca con una forma cualquiera

Info

Publication number
ES8707891A1
ES8707891A1 ES557438A ES557438A ES8707891A1 ES 8707891 A1 ES8707891 A1 ES 8707891A1 ES 557438 A ES557438 A ES 557438A ES 557438 A ES557438 A ES 557438A ES 8707891 A1 ES8707891 A1 ES 8707891A1
Authority
ES
Spain
Prior art keywords
contact
product
generatrix
tape
point
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
Application number
ES557438A
Other languages
English (en)
Other versions
ES557438A0 (es
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.)
Airbus Group SAS
Original Assignee
Airbus Group 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 Airbus Group SAS filed Critical Airbus Group SAS
Publication of ES557438A0 publication Critical patent/ES557438A0/es
Publication of ES8707891A1 publication Critical patent/ES8707891A1/es
Expired legal-status Critical Current

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
    • B29C70/30—Shaping 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
    • B29C70/32—Shaping 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 on a rotating mould, former or core
    • 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
    • B29C53/00—Shaping by bending, folding, twisting, straightening or flattening; Apparatus therefor
    • B29C53/56—Winding and joining, e.g. winding spirally
    • B29C53/58—Winding and joining, e.g. winding spirally helically
    • B29C53/60—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels
    • B29C53/62—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis
    • B29C53/66—Winding and joining, e.g. winding spirally helically using internal forming surfaces, e.g. mandrels rotatable about the winding axis with axially movable winding feed member, e.g. lathe type winding
    • B29C53/665—Coordinating the movements of the winding feed member and the mandrel
    • 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
    • B29C70/30—Shaping 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
    • B29C70/32—Shaping 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 on a rotating mould, former or core
    • B29C70/323—Shaping 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 on a rotating mould, former or core on the inner surface of a rotating mould
    • 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
    • B29C70/30—Shaping 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
    • B29C70/38—Automated lay-up, e.g. using robots, laying filaments according to predetermined patterns
    • B29C70/382—Automated fiber placement [AFP]
    • 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
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/04—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using liquids, gas or steam
    • B29C35/045—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using liquids, gas or steam using gas or flames
    • 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
    • B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
    • B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
    • B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
    • B29C35/0805—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Composite Materials (AREA)
  • Robotics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Separation Using Semi-Permeable Membranes (AREA)
  • Laminated Bodies (AREA)
  • Inorganic Fibers (AREA)
  • Artificial Filaments (AREA)
  • Spinning Methods And Devices For Manufacturing Artificial Fibers (AREA)

Abstract

PROCEDIMIENTO PARA LA FORMACION DE UNA PIEZA HUECA DE FORMA CUALQUIERA. COMPRENDE LAS OPERACIONES DE ENROLLAR UN PRODUCTO COMPUESTO A BASE DE FIBRAS CONTINUAS IMPREGNADAS DE UNA RESINA, QUE SE PRESENTA BAJO LA FORMA DE UNA CINTA SOBRE UNA SUPERFICIE LLEVADA POR UNA PIEZA DE FORMA POR MEDIO DE UN ORGANO APLICADOR, QUE INCLUYE UNA GENERATRIZ DE CONTACTO, ENTRE LA CUAL Y DICHA SUPERFICIE PASA EL PRODUCTO; DE DOTAR A LA SUPERFICIE RESPECTO AL ORGANO APLICADOR, DE UN MOVIMIENTO RELATIVO DE ROTACION ALREDEDOR DE UN EJE FIJO Y DE TRASLACION PARALELA A ESTE EJE; Y DE MANTENER EL ORGANO APLICADOR EN UNA ORIENTACION TAL, QUE LA FUERZA DE APLICACION DE DICHO ORGANO SOBRE LA SUPERFICIE SEA SENSIBLEMENTE NORMAL DE MODO CONSTANTE A LA SUPERFICIE EN EL PUNTO DE CONTACTO.
ES557438A 1985-03-25 1987-03-12 Procedimiento para fabricar una pieza hueca con una forma cualquiera Expired ES8707891A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8504379A FR2579130B1 (fr) 1985-03-25 1985-03-25 Procede et dispositif pour realiser une piece creuse de forme complexe par enroulement filamentaire au contact

Publications (2)

Publication Number Publication Date
ES557438A0 ES557438A0 (es) 1987-09-01
ES8707891A1 true ES8707891A1 (es) 1987-09-01

Family

ID=9317528

Family Applications (2)

Application Number Title Priority Date Filing Date
ES553309A Expired ES8705795A1 (es) 1985-03-25 1986-03-24 Procedimiento para fabricar una pieza hueca con una forma cualquiera
ES557438A Expired ES8707891A1 (es) 1985-03-25 1987-03-12 Procedimiento para fabricar una pieza hueca con una forma cualquiera

Family Applications Before (1)

Application Number Title Priority Date Filing Date
ES553309A Expired ES8705795A1 (es) 1985-03-25 1986-03-24 Procedimiento para fabricar una pieza hueca con una forma cualquiera

Country Status (9)

Country Link
EP (1) EP0198744B1 (es)
JP (1) JPS61267666A (es)
AT (1) ATE41353T1 (es)
CA (1) CA1299475C (es)
DE (1) DE3662348D1 (es)
DK (1) DK160238C (es)
ES (2) ES8705795A1 (es)
FR (1) FR2579130B1 (es)
IN (1) IN166733B (es)

Families Citing this family (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0355308B1 (en) * 1988-08-25 1993-09-22 Cincinnati Milacron Inc. Fibre placement machine
US5200018A (en) * 1990-12-19 1993-04-06 Hercules Incorporated Ribbonizing apparatus for individually heating a plurality of laterally adjacent tows in a fiber placement device
CA2057160A1 (en) * 1990-12-19 1992-06-20 John A. Johnson Fiber placement compaction preheat system
CA2057222C (en) * 1990-12-19 1998-05-19 Keith G. Shupe Fiber placement delivery system
CA2057225C (en) * 1990-12-19 1994-09-27 John A. Johnson Band fiber forming and placement delivery head
US5273602A (en) * 1990-12-19 1993-12-28 Hercules Incorporated Ribbonizing method for selectively heating a respective one of a plurality of fiber tows
CA2057201C (en) * 1990-12-19 1998-05-19 Vernon M. Benson Multiple axes fiber placement machine
EP0534092B1 (en) 1991-07-31 1996-09-18 Hercules Incorporated Cure-on-the-fly system
JP3194765B2 (ja) * 1991-11-13 2001-08-06 株式会社ブリヂストン 細幅帯状体の巻き付け装置
FR2686080B1 (fr) * 1992-01-14 1994-11-10 Aerospatiale Procede de depose au contact a chaud de materiau composite fibre a matrice vitreuse et dispositif pour la mise en óoeuvre du procede.
US5954917A (en) * 1997-06-02 1999-09-21 Boeing North American, Inc. Automated material delivery system
FR2784930B1 (fr) * 1998-10-23 2007-09-28 Vetrotex France Sa Corps de revolution creux en materiau composite et son procede de fabrication
EP1211052A1 (de) * 2000-10-26 2002-06-05 Abb Research Ltd. Verfahren und Vorrichtung zum Bandagieren von Körpern mit faserverstärkten Kunststoffbändern
US6989067B2 (en) 2003-04-14 2006-01-24 Roller Equipment Manufacturing Co., Inc. Method and apparatus for application of material to core
US7080441B2 (en) * 2003-07-28 2006-07-25 The Boeing Company Composite fuselage machine and method of automated composite lay up
US7282107B2 (en) * 2003-08-22 2007-10-16 The Boeing Company Multiple head automated composite laminating machine for the fabrication of large barrel section components
US7083698B2 (en) * 2003-08-22 2006-08-01 The Boeing Company Automated composite lay-up to an internal fuselage mandrel
US7048024B2 (en) * 2003-08-22 2006-05-23 The Boeing Company Unidirectional, multi-head fiber placement
EP1533107B1 (fr) * 2003-11-21 2007-01-03 Société de Technologie Michelin Appareil et procédé de pose d'une bandelette en continu sur une surface toroidale
US7134629B2 (en) 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7527222B2 (en) 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7325771B2 (en) 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US7503368B2 (en) 2004-11-24 2009-03-17 The Boeing Company Composite sections for aircraft fuselages and other structures, and methods and systems for manufacturing such sections
US7278198B2 (en) 2005-02-01 2007-10-09 The Boeing Company Mandrel segment loader
US7472736B2 (en) 2005-02-14 2009-01-06 The Boeing Company Modular head lamination device and method
NL1028697C2 (nl) * 2005-04-05 2006-10-09 Airborne Dev B V Inrichting en werkwijze voor het vervaardigen van vezelversterkte buis.
US8388795B2 (en) 2007-05-17 2013-03-05 The Boeing Company Nanotube-enhanced interlayers for composite structures
US8042767B2 (en) 2007-09-04 2011-10-25 The Boeing Company Composite fabric with rigid member structure
US8296923B2 (en) * 2007-11-29 2012-10-30 Spirit Aerosystems, Inc. Modular numerically controlled system
US20100200168A1 (en) * 2009-02-06 2010-08-12 Ingersoll Machine Tools, Inc. Fiber delivery apparatus and system having a creel and fiber placement head sans fiber redirect
US8758538B2 (en) * 2010-05-12 2014-06-24 Fives Machining Systems, Inc. Robotic based fiber placement cell with stationary dispensing head and creel
NL2004854C2 (en) 2010-06-08 2011-12-12 Airborne Dev B V Method and device for manufacturing composite products comprising a planar portion.
US8954180B2 (en) 2010-08-06 2015-02-10 Ingersoll Machine Tools, Inc. Manufacturing process and apparatus having an interchangeable machine tool head with integrated control
US8534338B2 (en) 2010-10-15 2013-09-17 Ingersoll Machine Tools, Inc. Fiber delivery apparatus and system having a creel and fiber placement head with polar axis of rotation
DE102010043415B4 (de) * 2010-11-04 2015-04-09 Airbus Operations Gmbh Verfahren zum Herstellen eines hohlen Bauteils sowie Vorrichtung
NL2006335C2 (en) 2011-03-03 2012-09-04 Airborne Composites Tubulars B V Method for manufacturing continuous composite tube, apparatus for manufacturing continuous composite tube.
DE102015206858A1 (de) * 2015-04-16 2016-10-20 Bayerische Motoren Werke Aktiengesellschaft Verfahren und Vorrichtung zur Herstellung flächiger Bauteile mit faserverstärktem Kunststoff
US10589463B2 (en) * 2017-06-29 2020-03-17 Continuous Composites Inc. Print head for additive manufacturing system
FR3070023B1 (fr) * 2017-08-10 2021-07-16 Safran Nacelles Procédé de fabrication d’une structure fibreuse tubulaire
CA3084429A1 (fr) * 2017-12-06 2019-06-13 Safran Aircraft Engines Procede de fabrication additive in situ d'un revetement sur un carter de turbomachine
CN110143483A (zh) * 2019-05-15 2019-08-20 合肥黑孚电热工业技术有限公司 一种用于自限温伴热带的快速放线复饶机
EP3871861B1 (en) * 2020-02-28 2024-08-07 Tsudakoma Kogyo Kabushiki Kaisha Automated fiber bundle placement apparatus

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Publication number Priority date Publication date Assignee Title
JPS5075264A (es) * 1973-11-05 1975-06-20
DE3226290C2 (de) * 1982-07-14 1985-09-12 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung zum gesteuerten Ablegen von Fasern auf eine Form
US4790898A (en) * 1982-07-19 1988-12-13 The Boeing Company Method and apparatus for fiber lamination
US4461669A (en) * 1983-09-30 1984-07-24 The Boeing Company Pivotal mount for laminating head

Also Published As

Publication number Publication date
EP0198744B1 (fr) 1989-03-15
ES553309A0 (es) 1987-05-16
ES8705795A1 (es) 1987-05-16
JPH0542337B2 (es) 1993-06-28
ES557438A0 (es) 1987-09-01
FR2579130A1 (fr) 1986-09-26
FR2579130B1 (fr) 1987-10-09
EP0198744A1 (fr) 1986-10-22
DK160238C (da) 1991-07-22
JPS61267666A (ja) 1986-11-27
DE3662348D1 (en) 1989-04-20
CA1299475C (fr) 1992-04-28
ATE41353T1 (de) 1989-04-15
DK126786D0 (da) 1986-03-19
IN166733B (es) 1990-07-14
DK126786A (da) 1986-09-26
DK160238B (da) 1991-02-18

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Legal Events

Date Code Title Description
FD1A Patent lapsed

Effective date: 20040628