ES2570584A1 - Procedure and installation for the automated manufacture of a vacuum structure (Machine-translation by Google Translate, not legally binding) - Google Patents
Procedure and installation for the automated manufacture of a vacuum structure (Machine-translation by Google Translate, not legally binding)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
- translation
- installation
- machine
- legally binding
- 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
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
The invention relates to a method and an installation for the automated manufacture of a vacuum structure for manufacturing a fiber composite component, wherein a plurality of layers of untamped material are initially provided for the vacuum structure, assembling the they are automated by means of assembly equipment to form a pre-assembled layered vacuum structure, the layers of material being automatically made by a cutting device as a function of prescribed geometry data. (Machine-translation by Google Translate, not legally binding)
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 manufacture of a vacuum structure (Machine-translation by Google Translate, not legally binding) |
Country Status (3)
Country | Link |
---|---|
DE (1) | DE102014116848B4 (en) |
ES (1) | ES2570584A1 (en) |
FR (1) | FR3028448B1 (en) |
Families Citing this family (5)
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 |
DE102016111074A1 (en) | 2016-06-16 | 2017-12-21 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Gas guide arrangement and method for the 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 |
PL437425A1 (en) * | 2021-03-26 | 2022-10-03 | Marbet Spółka Z Ograniczoną Odpowiedzialnością | Method of producing monomaterial panels from thermoformable nonwovens |
Citations (4)
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. | Method for manufacturing elements of composite materials by the cobonding technique |
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)
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 |
-
2014
- 2014-11-18 DE DE102014116848.8A patent/DE102014116848B4/en active Active
-
2015
- 2015-11-18 ES ES201531666A patent/ES2570584A1/en active Pending
- 2015-11-18 FR FR1561090A patent/FR3028448B1/en active Active
Patent Citations (4)
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. | Method for manufacturing elements of composite materials by the cobonding technique |
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 |
---|---|
FR3028448B1 (en) | 2022-01-07 |
DE102014116848A1 (en) | 2016-05-19 |
FR3028448A1 (en) | 2016-05-20 |
DE102014116848B4 (en) | 2023-06-15 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FC2A | Grant refused |
Effective date: 20171006 |