WO2008003740A1 - Method for producing a fibre composite component using a moulding core, and said moulding core - Google Patents
Method for producing a fibre composite component using a moulding core, and said moulding core Download PDFInfo
- Publication number
- WO2008003740A1 WO2008003740A1 PCT/EP2007/056799 EP2007056799W WO2008003740A1 WO 2008003740 A1 WO2008003740 A1 WO 2008003740A1 EP 2007056799 W EP2007056799 W EP 2007056799W WO 2008003740 A1 WO2008003740 A1 WO 2008003740A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- core
- moulding
- fibre composite
- composite component
- moulding core
- Prior art date
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
- B29C33/00—Moulds or cores; Details thereof or accessories therefor
- B29C33/44—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles
- B29C33/52—Moulds or cores; Details thereof or accessories therefor with means for, or specially constructed to facilitate, the removal of articles, e.g. of undercut articles soluble or fusible
-
- 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
-
- 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
- B29D—PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCES IN A PLASTIC STATE
- B29D99/00—Subject matter not provided for in other groups of this subclass
- B29D99/001—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings
- B29D99/0014—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/13—Hollow or container type article [e.g., tube, vase, etc.]
- Y10T428/1352—Polymer or resin containing [i.e., natural or synthetic]
- Y10T428/1372—Randomly noninterengaged or randomly contacting fibers, filaments, particles, or flakes
Abstract
Description
Claims
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/308,793 US20100092708A1 (en) | 2006-07-06 | 2007-07-05 | Method For Producing A Fibre Composite Component For Aerospace |
JP2009517271A JP2009542494A (en) | 2006-07-06 | 2007-07-05 | Method for producing composite fiber component using molded core material and molded core material thereof |
CN2007800256590A CN101484291B (en) | 2006-07-06 | 2007-07-05 | Method for producing a fibre composite component using a moulding core, and said moulding core |
CA002655710A CA2655710A1 (en) | 2006-07-06 | 2007-07-05 | Method for producing a fibre composite component using a moulding core, and said moulding core |
BRPI0714004-5A BRPI0714004A2 (en) | 2006-07-06 | 2007-07-05 | process for producing a fiber composite component using a modeling core and said modeling core |
EP07787094A EP2043832B8 (en) | 2006-07-06 | 2007-07-05 | Method for producing a fibre composite component using a moulding core, and said moulding core |
Applications Claiming Priority (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US81893006P | 2006-07-06 | 2006-07-06 | |
DE102006031323A DE102006031323B4 (en) | 2006-07-06 | 2006-07-06 | Method for producing a fiber composite component for aerospace applications |
DE102006031323.2 | 2006-07-06 | ||
US60/818,930 | 2006-07-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2008003740A1 true WO2008003740A1 (en) | 2008-01-10 |
Family
ID=38806031
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2007/056799 WO2008003740A1 (en) | 2006-07-06 | 2007-07-05 | Method for producing a fibre composite component using a moulding core, and said moulding core |
Country Status (9)
Country | Link |
---|---|
US (1) | US20100092708A1 (en) |
EP (1) | EP2043832B8 (en) |
JP (1) | JP2009542494A (en) |
CN (1) | CN101484291B (en) |
BR (1) | BRPI0714004A2 (en) |
CA (1) | CA2655710A1 (en) |
DE (1) | DE102006031323B4 (en) |
RU (1) | RU2445206C2 (en) |
WO (1) | WO2008003740A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8500085B2 (en) | 2006-07-06 | 2013-08-06 | Airbus Operations Gmbh | Method for manufacturing a composite fiber component for aerospace |
US8906489B2 (en) | 2006-07-06 | 2014-12-09 | Airbus Operations Gmbh | Method for producing a fibre composite component for aviation and spaceflight |
US9492974B2 (en) | 2006-07-06 | 2016-11-15 | Airbus Operations Gmbh | Method for producing a fiber composite component for aviation and spaceflight |
US10207463B2 (en) | 2006-07-06 | 2019-02-19 | Airbus Operations Gmbh | Method for producing a fiber composite component for aerospace |
Families Citing this family (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE102006031326B4 (en) * | 2006-07-06 | 2010-09-23 | Airbus Deutschland Gmbh | Mold core and method for producing a fiber composite component for the aerospace industry |
DE102008049359B4 (en) * | 2008-09-29 | 2015-10-08 | Airbus Helicopters Deutschland GmbH | Manufacturing process for hollow components made of fiber composite materials in hose construction, film tube and manufacturing process for a film tube |
DE102009027049B4 (en) | 2009-06-19 | 2011-09-15 | Cotesa Gmbh | Method for integrating cavity-forming structures in fiber composite shells |
EP2327526B1 (en) * | 2009-11-27 | 2015-10-14 | AIRBUS HELICOPTERS DEUTSCHLAND GmbH | Mold core comprising a decomposable and a non-decomposable portion |
DE102010010876A1 (en) * | 2010-02-09 | 2011-08-11 | Universität Bremen, 28359 | Loose mold core for manufacturing of components of polymer fiber-reinforced composites, is provided partly, particularly locally or in layer, with fiber reinforcement or textile reinforcement |
DE102011113200B4 (en) * | 2011-09-10 | 2017-10-12 | Volkswagen Aktiengesellschaft | A method for producing a hollow profile node of a fiber-plastic composite for the connection of hollow profile components of a frame member |
DE102012004942B4 (en) | 2012-03-12 | 2014-02-20 | Munich Composites Gmbh | Process for producing a preform and a fiber composite prefabricated component produced therefrom |
DE102013002012A1 (en) * | 2013-02-06 | 2014-08-07 | Jürgen Stumpf | Method of making custom shoe inserts |
US9358703B2 (en) * | 2013-07-09 | 2016-06-07 | The Boeing Company | Thermoplastic sandwich structures |
DE102013111776B8 (en) * | 2013-10-25 | 2016-11-17 | Benteler Sgl Gmbh & Co. Kg | Process for producing a hollow fiber composite component |
DE102014215965A1 (en) | 2014-08-12 | 2016-02-18 | Bayerische Motoren Werke Aktiengesellschaft | Process for producing a fiber-reinforced plastic component |
EP3034263A1 (en) | 2014-12-19 | 2016-06-22 | Sadair Spear AB | Method for manufacturing a fibre-reinforced structure, mandrel, molding system and fibre-reinforced structure |
JP6553903B2 (en) | 2015-03-19 | 2019-07-31 | 住友理工株式会社 | Manufacturing method of resin molded article |
DE102015225656A1 (en) * | 2015-12-17 | 2017-06-22 | Bayerische Motoren Werke Aktiengesellschaft | Method for producing a fiber-reinforced hollow profile component |
EP3533580B1 (en) * | 2016-10-31 | 2021-07-07 | Mitsubishi Chemical Corporation | Method for manufacturing fiber reinforced plastic molded body |
DE102020134901A1 (en) * | 2020-12-23 | 2022-06-23 | Airbus Operations Gmbh | Mold core for manufacturing a component made of fiber composite material |
DE102022105064A1 (en) | 2022-03-03 | 2023-09-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Process for producing a fiber composite component from a fiber composite material |
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DE102006031326B4 (en) * | 2006-07-06 | 2010-09-23 | Airbus Deutschland Gmbh | Mold core and method for producing a fiber composite component for the aerospace industry |
DE102006031325B4 (en) * | 2006-07-06 | 2010-07-01 | Airbus Deutschland Gmbh | Method for producing a fiber composite component for aerospace applications |
DE102006031335B4 (en) * | 2006-07-06 | 2011-01-27 | Airbus Operations Gmbh | Method for producing a fiber composite component for aerospace applications |
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-
2006
- 2006-07-06 DE DE102006031323A patent/DE102006031323B4/en not_active Expired - Fee Related
-
2007
- 2007-07-05 JP JP2009517271A patent/JP2009542494A/en active Pending
- 2007-07-05 WO PCT/EP2007/056799 patent/WO2008003740A1/en active Application Filing
- 2007-07-05 CN CN2007800256590A patent/CN101484291B/en active Active
- 2007-07-05 BR BRPI0714004-5A patent/BRPI0714004A2/en not_active IP Right Cessation
- 2007-07-05 EP EP07787094A patent/EP2043832B8/en not_active Not-in-force
- 2007-07-05 RU RU2009103203/05A patent/RU2445206C2/en not_active IP Right Cessation
- 2007-07-05 US US12/308,793 patent/US20100092708A1/en not_active Abandoned
- 2007-07-05 CA CA002655710A patent/CA2655710A1/en not_active Abandoned
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0491650A2 (en) * | 1990-12-19 | 1992-06-24 | United Technologies Corporation | Conformal composite molding |
US5262121A (en) * | 1991-12-18 | 1993-11-16 | Goodno Kenneth T | Method of making and using flexible mandrel |
WO1995014563A1 (en) * | 1993-11-26 | 1995-06-01 | Alan Roger Harper | Casting method and apparatus and products thereof |
GB2292332A (en) * | 1994-04-22 | 1996-02-21 | Alan Roger Harper | Moulding process and apparatus |
FR2745745A1 (en) * | 1996-03-07 | 1997-09-12 | Snecma | Manufacturing procedure for vessel of composition material with protective inner coating |
WO2005105402A1 (en) * | 2004-04-20 | 2005-11-10 | The Boeing Company | Co-cured stringers and associated mandrel and fabrication method |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8500085B2 (en) | 2006-07-06 | 2013-08-06 | Airbus Operations Gmbh | Method for manufacturing a composite fiber component for aerospace |
US8906489B2 (en) | 2006-07-06 | 2014-12-09 | Airbus Operations Gmbh | Method for producing a fibre composite component for aviation and spaceflight |
US9492974B2 (en) | 2006-07-06 | 2016-11-15 | Airbus Operations Gmbh | Method for producing a fiber composite component for aviation and spaceflight |
US10207463B2 (en) | 2006-07-06 | 2019-02-19 | Airbus Operations Gmbh | Method for producing a fiber composite component for aerospace |
Also Published As
Publication number | Publication date |
---|---|
EP2043832B1 (en) | 2012-10-03 |
CN101484291B (en) | 2012-06-13 |
RU2445206C2 (en) | 2012-03-20 |
DE102006031323B4 (en) | 2010-07-15 |
EP2043832A1 (en) | 2009-04-08 |
US20100092708A1 (en) | 2010-04-15 |
DE102006031323A1 (en) | 2008-01-10 |
JP2009542494A (en) | 2009-12-03 |
CA2655710A1 (en) | 2008-01-10 |
CN101484291A (en) | 2009-07-15 |
RU2009103203A (en) | 2010-08-20 |
EP2043832B8 (en) | 2012-11-07 |
BRPI0714004A2 (en) | 2012-12-18 |
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