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ES2570584A1 - Procedure and installation for the automated manufacturing of a vacuum structure - Google Patents

Procedure and installation for the automated manufacturing of a vacuum structure

Info

Publication number
ES2570584A1
ES2570584A1 ES201531666A ES201531666A ES2570584A1 ES 2570584 A1 ES2570584 A1 ES 2570584A1 ES 201531666 A ES201531666 A ES 201531666A ES 201531666 A ES201531666 A ES 201531666A ES 2570584 A1 ES2570584 A1 ES 2570584A1
Authority
ES
Spain
Prior art keywords
vacuum structure
installation
procedure
layers
automated manufacturing
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.)
Pending
Application number
ES201531666A
Other languages
Spanish (es)
Inventor
Andreas Kolbe
Jens Ramon Bölke
Christian Krombholz
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.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsches Zentrum fuer Luft und Raumfahrt eV
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 Deutsches Zentrum fuer Luft und Raumfahrt eV filed Critical Deutsches Zentrum fuer Luft und Raumfahrt eV
Publication of ES2570584A1 publication Critical patent/ES2570584A1/en
Pending legal-status Critical Current

Links

Classifications

    • 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
    • B32B38/0004—Cutting, tearing or severing, e.g. bursting; Cutter details
    • 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
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • 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
    • B29C70/44—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding
    • B29C70/443—Shaping or impregnating by compression not applied for producing articles of definite length, i.e. discrete articles using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding and impregnating by vacuum or injection
    • 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
    • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
    • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary 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
    • B32B2605/00—Vehicles
    • 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
    • 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
    • B32B37/14—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers
    • B32B37/16—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating
    • B32B37/20—Methods or apparatus for laminating, e.g. by curing or by ultrasonic bonding characterised by the properties of the layers with all layers existing as coherent layers before laminating involving the assembly of continuous webs only

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Composite Materials (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Moulding By Coating Moulds (AREA)

Abstract

La invención se refiere a un procedimiento y a una instalación para la fabricación automatizada de una estructura de vacío para fabricar un componente de compuesto de fibras, en el que primeramente se proporciona una pluralidad de capas de material sin confeccionar para la estructura de vacío, ensamblándose las mismas de forma automatizada mediante un equipo de ensamblaje para formar una estructura de vacío por capas preconfeccionada, confeccionándose automáticamente las capas de material mediante un dispositivo de corte en función de datos de geometría prescritos.The invention relates to a method and an installation for the automated manufacturing of a vacuum structure for manufacturing a fiber composite component, in which a plurality of layers of raw material for the vacuum structure are first provided, the layers being assembled. The same in an automated way by means of assembly equipment to form a pre-assembled layered vacuum structure, the layers of material being automatically made by means of a cutting device based on prescribed geometry data.

ES201531666A 2014-11-18 2015-11-18 Procedure and installation for the automated manufacturing of a vacuum structure Pending ES2570584A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102014116848.8A DE102014116848B4 (en) 2014-11-18 2014-11-18 Process and system for the automated production of a vacuum structure

Publications (1)

Publication Number Publication Date
ES2570584A1 true ES2570584A1 (en) 2016-05-19

Family

ID=55855014

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201531666A Pending ES2570584A1 (en) 2014-11-18 2015-11-18 Procedure and installation for the automated manufacturing of a vacuum structure

Country Status (3)

Country Link
DE (1) DE102014116848B4 (en)
ES (1) ES2570584A1 (en)
FR (1) FR3028448B1 (en)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016102056A1 (en) 2016-02-05 2017-08-10 Deutsches Zentrum für Luft- und Raumfahrt e.V. Deck arrangement and method for producing a fiber composite component
DE102016111073A1 (en) 2016-06-16 2017-12-21 Deutsches Zentrum für Luft- und Raumfahrt e.V. Mold element and method for the vacuum-assisted processing of a semi-finished fiber product
DE102016111074B4 (en) 2016-06-16 2025-08-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Gas guide arrangement and method for vacuum-assisted processing of a semi-finished fiber product
DE102017100740B3 (en) 2017-01-16 2018-07-05 Eleftherios Gerolymos Flow aid for an infusion device for infiltrating a resin into a fibrous material
PL248546B1 (en) * 2021-03-26 2025-12-22 Marbet Spółka Z Ograniczoną Odpowiedzialnością Method of producing monomaterial panels from thermoformable nonwovens

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5738741A (en) * 1996-03-26 1998-04-14 The University Of Dayton Pre-fabricated vacuum bag and vacuum bag process to externally reinforce structural members with advanced composites
ES2205961A1 (en) * 2001-02-13 2004-05-01 Eads Construcciones Aeronauticas, S.A. PROCEDURE FOR THE MANUFACTURE OF COMPOSITE MATERIAL ELEMENTS THROUGH THE COENCOLATE TECHNOLOGY.
ES2246675A1 (en) * 2003-12-30 2006-02-16 Airbus España S.L. Formation of a vacuum bag for autoclavable material consists of full surface contacting of sheet with the component prior to autoclaving, via guides protecting the component
ES2329695T3 (en) * 2004-04-30 2009-11-30 Robert Bosch Gmbh PROCEDURE FOR THE MANUFACTURE OF TUBULAR BAGS.

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2124130B (en) 1982-07-24 1985-11-27 Rolls Royce Vacuum moulding fibre reinforced resin
DE69511458T3 (en) 1994-05-27 2007-04-12 Instance, David John, Sellindge Labels and methods for their manufacture
SE0301319L (en) 2003-05-07 2004-11-08 Hssa Sweden Ab Method for manufacturing composite structures
US7344044B2 (en) 2005-01-14 2008-03-18 Bradford Company Partition assembly having floor parent welded to partitions
US7993479B2 (en) 2006-09-27 2011-08-09 Airbus Deutschland Gmbh Method for joining precured or cured stringers to at least one structural component of an aircraft or spacecraft
DE102008006261B3 (en) 2008-01-25 2009-01-08 Eads Deutschland Gmbh Laminate for lining matrix feeders used to impregnate preforms comprises gas-permeable inner sheet and gas-impermeable outer sheet separated by layer of gas-permeable spacers, textile layer being laminated to outer surface of inner sheet
DE102008058345B4 (en) 2008-11-20 2022-09-29 Fritz Egger Gmbh & Co. Og Method of making a plate

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5738741A (en) * 1996-03-26 1998-04-14 The University Of Dayton Pre-fabricated vacuum bag and vacuum bag process to externally reinforce structural members with advanced composites
ES2205961A1 (en) * 2001-02-13 2004-05-01 Eads Construcciones Aeronauticas, S.A. PROCEDURE FOR THE MANUFACTURE OF COMPOSITE MATERIAL ELEMENTS THROUGH THE COENCOLATE TECHNOLOGY.
ES2246675A1 (en) * 2003-12-30 2006-02-16 Airbus España S.L. Formation of a vacuum bag for autoclavable material consists of full surface contacting of sheet with the component prior to autoclaving, via guides protecting the component
ES2329695T3 (en) * 2004-04-30 2009-11-30 Robert Bosch Gmbh PROCEDURE FOR THE MANUFACTURE OF TUBULAR BAGS.

Also Published As

Publication number Publication date
DE102014116848A1 (en) 2016-05-19
FR3028448A1 (en) 2016-05-20
FR3028448B1 (en) 2022-01-07
DE102014116848B4 (en) 2023-06-15

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Legal Events

Date Code Title Description
FC2A Grant refused

Effective date: 20171006