FR3028448B1 - Procede et installation pour fabriquer automatiquement un assemblage de mise sous vide - Google Patents

Procede et installation pour fabriquer automatiquement un assemblage de mise sous vide Download PDF

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Publication number
FR3028448B1
FR3028448B1 FR1561090A FR1561090A FR3028448B1 FR 3028448 B1 FR3028448 B1 FR 3028448B1 FR 1561090 A FR1561090 A FR 1561090A FR 1561090 A FR1561090 A FR 1561090A FR 3028448 B1 FR3028448 B1 FR 3028448B1
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FR
France
Prior art keywords
vacuum assembly
facility
vacuum
automatically manufacturing
assembly
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.)
Active
Application number
FR1561090A
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English (en)
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FR3028448A1 (fr
Inventor
Jens Ramon Bolke
Christian Krombholz
Andreas Kolbe
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
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Deutsches Zentrum fuer Luft und Raumfahrt eV
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Publication of FR3028448A1 publication Critical patent/FR3028448A1/fr
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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
    • 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
    • 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
    • B32B37/14—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

L'invention concerne un procédé et une installation pour fabriquer de manière automatisée un assemblage de mise sous vide destiné à la fabrication d'une pièce composite renforcée de fibres ; plusieurs couches de matériau (M1-M5) non confectionnées sont d'abord préparées et fournies pour l'assemblage de mise sous vide, puis assemblées de manière automatisée, couche par couche, par un dispositif de montage (120) pour former un assemblage de mise sous vide pré-confectionné, les couches de matériau étant confectionnées automatiquement par un dispositif de coupe (140), en fonction de données géométriques prescrites.
FR1561090A 2014-11-18 2015-11-18 Procede et installation pour fabriquer automatiquement un assemblage de mise sous vide Active FR3028448B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE102014116848.8A DE102014116848B4 (de) 2014-11-18 2014-11-18 Verfahren und Anlage zum automatisierten Herstellen eines Vakuumaufbaus

Publications (2)

Publication Number Publication Date
FR3028448A1 FR3028448A1 (fr) 2016-05-20
FR3028448B1 true FR3028448B1 (fr) 2022-01-07

Family

ID=55855014

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1561090A Active FR3028448B1 (fr) 2014-11-18 2015-11-18 Procede et installation pour fabriquer automatiquement un assemblage de mise sous vide

Country Status (3)

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

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102016102056A1 (de) 2016-02-05 2017-08-10 Deutsches Zentrum für Luft- und Raumfahrt e.V. Deckanordnung und Verfahren zum Herstellen eines Faserverbundwerkstoff-Bauteils
DE102016111073A1 (de) 2016-06-16 2017-12-21 Deutsches Zentrum für Luft- und Raumfahrt e.V. Formelement und Verfahren zum unterdruckunterstützten Verarbeiten eines Faserhalbzeugs
DE102016111074A1 (de) 2016-06-16 2017-12-21 Deutsches Zentrum für Luft- und Raumfahrt e.V. Gasführungsanordnung und Verfahren zum unterdruckunterstützten Verarbeiten eines Faserhalbzeugs
DE102017100740B3 (de) 2017-01-16 2018-07-05 Eleftherios Gerolymos Fließhilfe für eine Infusionsanordnung zum Infiltrieren eines Harzes in ein Fasermaterial
PL437425A1 (pl) * 2021-03-26 2022-10-03 Marbet Spółka Z Ograniczoną Odpowiedzialnością Sposób wytwarzania monomateriałowych paneli z włóknin termoformowalnych

Family Cites Families (11)

* 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
DK0684130T3 (da) 1994-05-27 1999-12-06 David John Instance Etiketter og fremstilling af disse
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
ES2205961B2 (es) 2001-02-13 2005-03-01 Eads Construcciones Aeronauticas, S.A. Procedimiento de fabricacion de elementos de material compuesto mediante la tecnoclogia del coencolado.
SE0301319L (sv) 2003-05-07 2004-11-08 Hssa Sweden Ab Metod för tillverkning av kompositstrukturer
ES2246675B1 (es) 2003-12-30 2007-05-01 Airbus España S.L. Metodo y aparato para la formacion de una bolsa de vacio en la fabricacion de estructuras de material compuesto de gran superficie.
KR101170659B1 (ko) 2004-04-30 2012-08-07 로베르트 보쉬 게엠베하 백 패키지 제조 방법
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 (de) 2008-01-25 2009-01-08 Eads Deutschland Gmbh Mehrlagiges, flexibles Flächenmaterial
DE102008058345B4 (de) 2008-11-20 2022-09-29 Fritz Egger Gmbh & Co. Og Verfahren zur Herstellung einer Platte

Also Published As

Publication number Publication date
ES2570584A1 (es) 2016-05-19
DE102014116848B4 (de) 2023-06-15
FR3028448A1 (fr) 2016-05-20
DE102014116848A1 (de) 2016-05-19

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