ES2032729T3 - Procedimiento y aparato para la fabricacion de una lamina compleja estanca con cualquier forma que incorpora una armadura interna. - Google Patents

Procedimiento y aparato para la fabricacion de una lamina compleja estanca con cualquier forma que incorpora una armadura interna.

Info

Publication number
ES2032729T3
ES2032729T3 ES91403176T ES91403176T ES2032729T3 ES 2032729 T3 ES2032729 T3 ES 2032729T3 ES 91403176 T ES91403176 T ES 91403176T ES 91403176 T ES91403176 T ES 91403176T ES 2032729 T3 ES2032729 T3 ES 2032729T3
Authority
ES
Spain
Prior art keywords
manufacture
reinforcement
composite
procedure
formation
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
ES91403176T
Other languages
English (en)
Other versions
ES2032729T1 (es
Inventor
Marc Henri Montagne
Olivier Regipa
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 ES2032729T1 publication Critical patent/ES2032729T1/es
Application granted granted Critical
Publication of ES2032729T3 publication Critical patent/ES2032729T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B29C70/06—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
    • 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
    • B29C70/20—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres
    • B29C70/202—Fibrous reinforcements only characterised by the structure of fibrous reinforcements, e.g. hollow fibres using fibres of substantial or continuous length oriented in a single direction, e.g. roofing or other parallel fibres arranged in parallel planes or structures of fibres crossing at substantial angles, e.g. cross-moulding compound [XMC]
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/04—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the partial melting of at least one layer
    • 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
    • B32B37/00—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding
    • B32B37/10—Methods 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
    • B32B37/1045—Intermittent pressing, e.g. by oscillating or reciprocating motion of the pressing means
    • 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
    • B32B38/00—Ancillary operations in connection with laminating processes
    • B32B38/0036—Heat treatment
    • 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
    • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
    • B29C70/685—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by laminating inserts between two plastic films or plates
    • B29C70/687—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by laminating inserts between two plastic films or plates the inserts being oriented, e.g. nets or meshes
    • 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
    • B29L2031/30—Vehicles, e.g. ships or aircraft, or body parts thereof
    • B29L2031/3076—Aircrafts
    • B29L2031/3085—Wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H9/00—Marine propulsion provided directly by wind power
    • B63H9/04—Marine propulsion provided directly by wind power using sails or like wind-catching surfaces
    • B63H9/06—Types of sail; Constructional features of sails; Arrangements thereof on vessels
    • B63H9/067—Sails characterised by their construction or manufacturing process
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63H—MARINE PROPULSION OR STEERING
    • B63H9/00—Marine propulsion provided directly by wind power
    • B63H9/04—Marine propulsion provided directly by wind power using sails or like wind-catching surfaces
    • B63H9/06—Types of sail; Constructional features of sails; Arrangements thereof on vessels
    • B63H9/067—Sails characterised by their construction or manufacturing process
    • B63H9/0678—Laminated sails

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Textile Engineering (AREA)
  • Composite Materials (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Fluid Mechanics (AREA)
  • Sustainable Energy (AREA)
  • Sustainable Development (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Ocean & Marine Engineering (AREA)
  • Manufacturing & Machinery (AREA)
  • Laminated Bodies (AREA)
  • Nonwoven Fabrics (AREA)
  • Revetment (AREA)
  • Manufacture Of Macromolecular Shaped Articles (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
  • Reinforced Plastic Materials (AREA)

Abstract

PARA FABRICAR UN COMPLEJO ESTANCO QUE LLEVA UN ARMAZON INTERNA Y DESTINADA , EN PARTICULAR, A LA FABRICACION DE GLOBOS AEROESTATICAS, SE REALIZA UNA ARMAZON (10) NO TEJIDA FORMADA DE HILO DE CADENA Y DE HILOS DE TRAMA DISPUESTOS EN DOS CAPAS SUPERPUESTAS. SE APLICA SOBRE CADA UNA DE LAS CARA DE ESTA ARMAZON, CON UNA FUERZA PREDETERMINADA, UNA PELICULA DE RECUBRIMIENTO (16A, 16B), DESPUES DE HABERLA LLEVADO A SU TEMPERATURA DE FUSION PASTOSA SOBRE UN TAMBOR TERMICO (30A, 30B). EL CARACTER NO TEJIDO DE LA ARMAZON PERMITE PRESERVAR LA ESTANQUEIDAD DE LAS PELICULAS DE RECUBRIMIENTO DURANTE EL COMPLEXADO. ADEMAS, LA FORMACION DE HEBILLITAS EN LOS BORDES DEL COMPLEJO ASI OBTENIDO PERMITE INTRODUCIR CABLES DE ENLACE QUE FACILITAN LA RECUPERACION DE LAS TENSIONES.
ES91403176T 1990-11-26 1991-11-25 Procedimiento y aparato para la fabricacion de una lamina compleja estanca con cualquier forma que incorpora una armadura interna. Expired - Lifetime ES2032729T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR909014745A FR2669574B1 (fr) 1990-11-26 1990-11-26 Procede et machine pour la fabrication d'une feuille complexe etanche, de forme quelconque, comportant une armature interne, et feuille ainsi obtenue.

Publications (2)

Publication Number Publication Date
ES2032729T1 ES2032729T1 (es) 1993-03-01
ES2032729T3 true ES2032729T3 (es) 1997-05-16

Family

ID=9402592

Family Applications (1)

Application Number Title Priority Date Filing Date
ES91403176T Expired - Lifetime ES2032729T3 (es) 1990-11-26 1991-11-25 Procedimiento y aparato para la fabricacion de una lamina compleja estanca con cualquier forma que incorpora una armadura interna.

Country Status (10)

Country Link
US (1) US5380388A (es)
EP (1) EP0488870B1 (es)
JP (1) JPH04299135A (es)
AT (1) ATE148395T1 (es)
CA (1) CA2056146A1 (es)
DE (2) DE69124489T2 (es)
DK (1) DK0488870T3 (es)
ES (1) ES2032729T3 (es)
FR (1) FR2669574B1 (es)
GR (1) GR3023218T3 (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IT1262096B (it) * 1993-03-31 1996-06-19 Tecnomeccanica Srl Dispositivo per la plastificazione bianca e volta
US5531850A (en) * 1994-06-21 1996-07-02 Paragon Trade Brands, Inc. Apparatus and method for applying transverse tensioned elastic
FR2725153A1 (fr) * 1994-09-29 1996-04-05 Sedepro Renforcement d'une matrice en materiau caoutchouteux par des fils
DE4439420A1 (de) * 1994-11-04 1996-05-09 Roehm Gmbh Verfahren zum thermischen Verkleben von Teilen aus Acrylkunststoff und Teilen aus technischen Kunststoffen
IT1295861B1 (it) 1997-11-13 1999-05-28 Marco Savelli Procedimento per realizzare un tessuto di forma convessa ed in generale una vela e/o una tensostruttura utilizzando il tessuto
US6914021B2 (en) * 1998-12-07 2005-07-05 Lockheed Martin Corporation Flexible wall material for use in an inflatable structure
JP2003001732A (ja) * 2001-06-20 2003-01-08 Diatex Co Ltd 合成樹脂製補強シート
WO2005000677A1 (en) * 2003-06-23 2005-01-06 Atair Aerospace, Inc. Construction materials and methods for parafoils and parachutes
US8079945B2 (en) 2004-02-10 2011-12-20 Pactiv Corporation Fiber-reinforced film processes and films
DE102008011517A1 (de) * 2008-03-02 2009-09-03 Schottdorf, Bernd, Dr. Verfahren, Vorrichtung und Stützstruktur sowie deren Verwendung zur Herstellung eines Faserverbundteils
CN113232398B (zh) * 2021-02-09 2022-11-15 广州市雨纯生物科技有限公司 一种阻菌性能的无纺布生产工艺

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3020194A (en) * 1958-01-22 1962-02-06 Toscony Fabrics Inc Two-sided laminator
FR1337011A (fr) * 1961-10-12 1963-09-06 Licentia Gmbh Procédé et dispositif pour la fabrication de laminés en nape, en plastique armé
US3535180A (en) * 1967-02-28 1970-10-20 Johnson & Johnson Methods of making reinforced plastic sheeting
US3687764A (en) * 1967-09-27 1972-08-29 Ethyl Corp Method for producing a multilayer reinforced plastic sheet material
US3627613A (en) * 1969-05-23 1971-12-14 Monsanto Co Continuous process for preparing composites in sheet form
US3791911A (en) * 1972-02-23 1974-02-12 Griffolyn Company Adhesive free fiber reinforced laminate
US4090902A (en) * 1973-05-23 1978-05-23 Industrie Pirelli, S.P.A. Optical fiber cable and manufacture thereof
DE2514105A1 (de) * 1975-03-29 1976-10-07 Hoechst Ag Verstaerkte folien, verfahren und vorrichtung zu deren kontinuierlichen herstellung
US4397703A (en) * 1981-10-01 1983-08-09 Mobil Oil Corporation Method and apparatus for manufacture of laminated reinforced film
EP0118628B1 (en) * 1983-02-09 1988-08-24 Mobil Oil Corporation Laminating method and apparatus for manufacture of reinforced film
NL8400410A (nl) * 1984-02-09 1985-09-02 Inventum Koninklijke Fab Werkwijze en inrichting voor het in een bepaald patroon tussen respectievelijk materiaallagen en materiaalbanen aanbrengen van een draadvormig element, in het bijzonder voor toepassing bij de vervaardiging van electrisch verwarmde voorwerpen, zoals dekens en kussens, waarbij het draadvormig element een verwarmingskabel is.
JPS62216730A (ja) * 1986-03-18 1987-09-24 Gunze Ltd 熱圧着ラミネ−ト方法及び装置
DE3821172A1 (de) * 1987-07-01 1989-01-12 Barmag Barmer Maschf Mehrschicht-kunststoffverbundplatte und verfahren zu ihrer herstellung
DE3726827A1 (de) * 1987-08-12 1988-03-03 Gerhard Fabritz Abdeckbahn fuer bewegliche bedachungen

Also Published As

Publication number Publication date
ES2032729T1 (es) 1993-03-01
EP0488870A1 (fr) 1992-06-03
DE69124489D1 (de) 1997-03-13
FR2669574A1 (fr) 1992-05-29
GR3023218T3 (en) 1997-07-30
DE69124489T2 (de) 1997-07-31
ATE148395T1 (de) 1997-02-15
CA2056146A1 (en) 1992-05-27
DE488870T1 (de) 1992-10-15
EP0488870B1 (fr) 1997-01-29
FR2669574B1 (fr) 1994-11-18
US5380388A (en) 1995-01-10
JPH04299135A (ja) 1992-10-22
DK0488870T3 (da) 1997-07-28

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