ATE553911T1 - Verfahren zur versteifung eines faserverbundbauteils sowie vakuummatte und anordnung zur herstellung eines versteiften faserverbundbauteils - Google Patents
Verfahren zur versteifung eines faserverbundbauteils sowie vakuummatte und anordnung zur herstellung eines versteiften faserverbundbauteilsInfo
- Publication number
- ATE553911T1 ATE553911T1 AT08865705T AT08865705T ATE553911T1 AT E553911 T1 ATE553911 T1 AT E553911T1 AT 08865705 T AT08865705 T AT 08865705T AT 08865705 T AT08865705 T AT 08865705T AT E553911 T1 ATE553911 T1 AT E553911T1
- Authority
- AT
- Austria
- Prior art keywords
- composite component
- fiber composite
- vacuum mat
- stiffen
- stiffening
- 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
- 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
- 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
- B29C33/38—Moulds or cores; Details thereof or accessories therefor characterised by the material or the manufacturing process
- B29C33/40—Plastics, e.g. foam or rubber
- B29C33/405—Elastomers, e.g. rubber
-
- 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
- B29C33/46—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 using 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
- B29C70/54—Component parts, details or accessories; Auxiliary operations, e.g. feeding or storage of prepregs or SMC after impregnation or during ageing
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2063/00—Use of EP, i.e. epoxy resins or derivatives thereof, as moulding material
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2707/00—Use of elements other than metals for preformed parts, e.g. for inserts
- B29K2707/04—Carbon
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Composite Materials (AREA)
- Chemical & Material Sciences (AREA)
- Fluid Mechanics (AREA)
- Manufacturing & Machinery (AREA)
- Physics & Mathematics (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
- Nonwoven Fabrics (AREA)
- Laminated Bodies (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US840107P | 2007-12-20 | 2007-12-20 | |
| DE102007061431A DE102007061431B4 (de) | 2007-12-20 | 2007-12-20 | Verfahren zur Versteifung eines Faserverbundbauteils sowie Vakuummatte und Anordnung zur Herstellung eines versteiften Faserverbundbauteils |
| PCT/EP2008/065699 WO2009080410A1 (de) | 2007-12-20 | 2008-11-17 | Verfahren zur versteifung eines faserverbundbauteils sowie vakuummatte und anordnung zur herstellung eines versteiften faserverbundbauteils |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE553911T1 true ATE553911T1 (de) | 2012-05-15 |
Family
ID=40689613
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT08865705T ATE553911T1 (de) | 2007-12-20 | 2008-11-17 | Verfahren zur versteifung eines faserverbundbauteils sowie vakuummatte und anordnung zur herstellung eines versteiften faserverbundbauteils |
Country Status (10)
| Country | Link |
|---|---|
| US (2) | US8137499B2 (enExample) |
| EP (1) | EP2219853B1 (enExample) |
| JP (1) | JP2011506149A (enExample) |
| CN (1) | CN101932433B (enExample) |
| AT (1) | ATE553911T1 (enExample) |
| BR (1) | BRPI0821382A2 (enExample) |
| CA (1) | CA2707932A1 (enExample) |
| DE (1) | DE102007061431B4 (enExample) |
| RU (1) | RU2480336C2 (enExample) |
| WO (1) | WO2009080410A1 (enExample) |
Families Citing this family (27)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102007061431B4 (de) | 2007-12-20 | 2013-08-08 | Airbus Operations Gmbh | Verfahren zur Versteifung eines Faserverbundbauteils sowie Vakuummatte und Anordnung zur Herstellung eines versteiften Faserverbundbauteils |
| DE102007062872A1 (de) * | 2007-12-28 | 2009-07-09 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Profils aus Faserverbundwerkstoff |
| DE102009001075A1 (de) * | 2009-02-23 | 2010-09-09 | Airbus Deutschland Gmbh | Verfahren zum zumindest teilweise Nachbearbeiten oder Ersetzen eines Versteifungselementes einer Faserverbundstruktur und zugehörige Anbindvorrichtung |
| DE102009029575B4 (de) * | 2009-09-18 | 2011-06-22 | Airbus Operations GmbH, 21129 | Verfahren zur Versteifung eines Faserverbundbauteils und Anordnung zur Herstellung eines versteiften Faserverbundteils |
| DE102009059720B4 (de) * | 2009-12-18 | 2012-04-12 | Airbus Operations Gmbh | Vorrichtung zur Herstellung einer aus Faserverbundwerkstoff bestehenden Rumpfschale für ein Luftfahrzeug |
| DE102010062871A1 (de) * | 2009-12-29 | 2011-06-30 | Airbus Operations GmbH, 21129 | Infusionsverfahren und Aufbau eines Infusionsverfahrens |
| DE102011015014A1 (de) * | 2010-11-10 | 2012-05-10 | Waldemar Piekenbrink GFK - Modell- und Formenbau, Produktions- und Vertriebs GmbH | Vakuumhauben-Vorrichtung |
| DE102011006047B4 (de) | 2011-03-24 | 2014-01-23 | Airbus Operations Gmbh | Verfahren sowie Vorrichtung zum Herstellen eines Faserverbundbauteils |
| DE102011014999A1 (de) * | 2011-03-25 | 2012-09-27 | Waldemar Piekenbrink GFK - Modell- und Formenbau, Produktions- und Vertriebs GmbH | Beheizbare Vakuumhauben-Vorrichtung |
| US9969131B2 (en) * | 2011-06-22 | 2018-05-15 | The Boeing Company | Automated ply layup system |
| US8985174B2 (en) * | 2011-08-26 | 2015-03-24 | The Boeing Company | Integrally stiffened, reusable vacuum bag and method of making the same |
| DE102011114206A1 (de) | 2011-09-23 | 2013-03-28 | Daimler Ag | Handhabungssystem und Handhabungsverfahren für Faseranordnungen |
| ES2626352T3 (es) * | 2013-05-30 | 2017-07-24 | Airbus Operations S.L. | Herramienta híbrida para curar piezas de material compuesto |
| JP6239272B2 (ja) * | 2013-06-04 | 2017-11-29 | 三菱航空機株式会社 | 繊維強化プラスチック部材の成形方法および成形装置 |
| JP6170347B2 (ja) * | 2013-06-07 | 2017-07-26 | 三菱航空機株式会社 | 繊維強化プラスチック構造体の製造方法および金型 |
| JP6220162B2 (ja) * | 2013-06-07 | 2017-10-25 | 三菱航空機株式会社 | 繊維強化プラスチック構造体の製造装置および製造方法 |
| EP2871045A1 (en) * | 2013-11-06 | 2015-05-13 | Airbus Operations GmbH | Arrangement and method for producing a composite material component |
| DE102015211671A1 (de) * | 2015-06-24 | 2016-12-29 | Airbus Operations Gmbh | Verfahren und Vorrichtung zur Herstellung eines Bauteils unter Verwendung einer Vakuumfolie |
| JP6563284B2 (ja) * | 2015-09-11 | 2019-08-21 | 三菱重工業株式会社 | 繊維強化プラスチック成型品の製造装置及びその製造方法 |
| CN106696304A (zh) * | 2016-11-23 | 2017-05-24 | 安徽佳力奇碳纤维科技股份公司 | 一种碳纤维复合材料抽真空装置及其抽真空的方法 |
| RU2675563C1 (ru) * | 2017-11-30 | 2018-12-19 | Федеральное государственное бюджетное образовательное учреждение высшего образования "Саратовский государственный технический университет имени Гагарина Ю.А." (СГТУ имени Гагарина Ю.А.) | Способ изготовления армированной волокном термопластичной композитной структуры с воздействием ультразвука и СВЧ электромагнитного поля |
| JP7114266B2 (ja) * | 2018-02-13 | 2022-08-08 | 三菱重工業株式会社 | 複合材料の製造方法および繊維基材 |
| FR3092785B1 (fr) * | 2019-02-19 | 2021-03-12 | Airbus Operations Sas | procédé de formage d’un film d’ensachage sous vide comprenant la formation de nervures par flambage du film |
| US11701801B2 (en) * | 2019-03-04 | 2023-07-18 | The Boeing Company | Caul plate with feature for separating from composite part |
| DE102019114710A1 (de) * | 2019-05-31 | 2020-12-03 | Airbus Operations Gmbh | Vorrichtung und Verfahren |
| US12049047B2 (en) * | 2020-06-17 | 2024-07-30 | Mitsubishi Heavy Industries, Ltd. | Jig and composite material processing method |
| US11840361B1 (en) | 2022-08-15 | 2023-12-12 | The Boeing Company | Magnetic handling systems for hat stringers and related methods |
Family Cites Families (22)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3145698A1 (de) * | 1981-11-19 | 1983-05-26 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Vorrichtung zum fertigen von bauteilen aus faserverstaerkten werkstoffen |
| US4451321A (en) * | 1983-02-16 | 1984-05-29 | Shatterproof Glass Corporation | Flexible vacuum bag |
| US4822651A (en) * | 1985-08-30 | 1989-04-18 | Newsom Cosby M | Vacuum diaphragm device |
| DE3605256C1 (de) * | 1986-02-19 | 1991-03-28 | Dornier Gmbh | Verfahren zur Herstellung von ebenen oder schalenfoermig gekruemmten Bauteilen aus faserverstaerkten Kunststoffen |
| US5217669A (en) | 1987-09-08 | 1993-06-08 | United Technologies Corporation | Method for forming complex composite articles |
| DE3739753A1 (de) * | 1987-11-24 | 1989-06-08 | Dornier Gmbh | Verfahren zum herstellen von bauteilen aus faserverstaerkten kunststoffen |
| JPH0517211Y2 (enExample) * | 1987-12-21 | 1993-05-10 | ||
| JP2647530B2 (ja) * | 1990-03-20 | 1997-08-27 | 三菱重工業株式会社 | 複合材一体成形用形状保持装置 |
| CA2056224A1 (en) * | 1990-12-19 | 1992-06-20 | Terry Martin Boustead | Conformal composite molding |
| JP3193064B2 (ja) * | 1991-04-22 | 2001-07-30 | 富士重工業株式会社 | 複合材料の一体成形方法 |
| JP2666878B2 (ja) * | 1992-12-28 | 1997-10-22 | 株式会社パイロット | 焼結体製造における成形方法及び焼結体 |
| US5709893A (en) * | 1995-06-06 | 1998-01-20 | The Boeing Company | Breathable tooling for forming parts from volatile-emitting composite materials |
| US5716488A (en) * | 1996-08-26 | 1998-02-10 | The Boeing Company | Reusable vacuum bag for making laminated articles |
| JPH10146898A (ja) * | 1996-11-15 | 1998-06-02 | Honda Motor Co Ltd | 繊維強化複合材の成形方法 |
| DE10013409C1 (de) * | 2000-03-17 | 2000-11-23 | Daimler Chrysler Ag | Verfahren und Vorrichtung zur Herstellung von faserverstärkten Bauteilen mittels eines Injektionsverfahrens |
| US6551091B1 (en) * | 2000-09-14 | 2003-04-22 | The Boeing Company | Flexible inflatable support structure for use with a reusable compaction bag |
| JP4713780B2 (ja) * | 2001-07-27 | 2011-06-29 | 富士重工業株式会社 | 補強パネルの製造方法 |
| US7147818B1 (en) * | 2002-05-16 | 2006-12-12 | The United States Of America As Represented By The Secretary Of The Army | Process and apparatus for improved composite fiber volume fraction and dimensional stability by removal of accumulated excess resin using the vacuum assisted resin transfer molding (VARTM) process |
| US6851945B2 (en) * | 2002-12-11 | 2005-02-08 | Northrop Grumman Corporation | Seal-less reusable vacuum bag |
| BRPI0520807A2 (pt) * | 2005-12-29 | 2009-06-09 | Airbus Espana Sl | processo para fabricar estruturas de composto com ferramentas pré-curadas embutidas |
| EP1972427B1 (en) * | 2005-12-30 | 2012-09-26 | Airbus Operations S.L. | Method for producing panels of composite materials with u-shaped stiffening elements |
| DE102007061431B4 (de) | 2007-12-20 | 2013-08-08 | Airbus Operations Gmbh | Verfahren zur Versteifung eines Faserverbundbauteils sowie Vakuummatte und Anordnung zur Herstellung eines versteiften Faserverbundbauteils |
-
2007
- 2007-12-20 DE DE102007061431A patent/DE102007061431B4/de not_active Expired - Fee Related
-
2008
- 2008-11-17 CN CN200880122130.5A patent/CN101932433B/zh not_active Expired - Fee Related
- 2008-11-17 EP EP08865705A patent/EP2219853B1/de not_active Not-in-force
- 2008-11-17 WO PCT/EP2008/065699 patent/WO2009080410A1/de not_active Ceased
- 2008-11-17 JP JP2010538525A patent/JP2011506149A/ja active Pending
- 2008-11-17 RU RU2010122661/05A patent/RU2480336C2/ru not_active IP Right Cessation
- 2008-11-17 AT AT08865705T patent/ATE553911T1/de active
- 2008-11-17 CA CA2707932A patent/CA2707932A1/en not_active Abandoned
- 2008-11-17 BR BRPI0821382A patent/BRPI0821382A2/pt not_active IP Right Cessation
-
2010
- 2010-06-16 US US12/816,853 patent/US8137499B2/en not_active Expired - Fee Related
-
2012
- 2012-02-29 US US13/408,660 patent/US20120152461A1/en not_active Abandoned
Also Published As
| Publication number | Publication date |
|---|---|
| JP2011506149A (ja) | 2011-03-03 |
| CA2707932A1 (en) | 2009-07-02 |
| CN101932433B (zh) | 2014-04-16 |
| US20100314042A1 (en) | 2010-12-16 |
| RU2010122661A (ru) | 2012-01-27 |
| DE102007061431A1 (de) | 2009-06-25 |
| BRPI0821382A2 (pt) | 2017-05-23 |
| EP2219853B1 (de) | 2012-04-18 |
| EP2219853A1 (de) | 2010-08-25 |
| DE102007061431B4 (de) | 2013-08-08 |
| WO2009080410A1 (de) | 2009-07-02 |
| RU2480336C2 (ru) | 2013-04-27 |
| US20120152461A1 (en) | 2012-06-21 |
| US8137499B2 (en) | 2012-03-20 |
| CN101932433A (zh) | 2010-12-29 |
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