FR2791600B1 - Procede destine a la fabrication d'elements en matiere plastique a geometrie non integralement developpable renforces par des fibres - Google Patents
Procede destine a la fabrication d'elements en matiere plastique a geometrie non integralement developpable renforces par des fibresInfo
- Publication number
- FR2791600B1 FR2791600B1 FR0003979A FR0003979A FR2791600B1 FR 2791600 B1 FR2791600 B1 FR 2791600B1 FR 0003979 A FR0003979 A FR 0003979A FR 0003979 A FR0003979 A FR 0003979A FR 2791600 B1 FR2791600 B1 FR 2791600B1
- Authority
- FR
- France
- Prior art keywords
- integrally
- manufacture
- fiber reinforced
- finished material
- plastic elements
- 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.)
- Expired - Lifetime
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
- B29C70/30—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
- B29C70/34—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation
- B29C70/342—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 and shaping or impregnating by compression, i.e. combined with compressing after the lay-up operation using isostatic 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
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19915083A DE19915083C1 (de) | 1999-04-01 | 1999-04-01 | Verfahren zur Herstellung faserverstärkter Kunststoffbauteile mit nicht-vollständig abwickelbarer Geometrie |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2791600A1 FR2791600A1 (fr) | 2000-10-06 |
FR2791600B1 true FR2791600B1 (fr) | 2005-02-25 |
Family
ID=7903389
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0003979A Expired - Lifetime FR2791600B1 (fr) | 1999-04-01 | 2000-03-29 | Procede destine a la fabrication d'elements en matiere plastique a geometrie non integralement developpable renforces par des fibres |
Country Status (6)
Country | Link |
---|---|
US (1) | US6527894B1 (fr) |
DE (1) | DE19915083C1 (fr) |
ES (1) | ES2176076B2 (fr) |
FR (1) | FR2791600B1 (fr) |
GB (1) | GB2351937B (fr) |
SE (1) | SE519225C2 (fr) |
Families Citing this family (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19915083C1 (de) | 1999-04-01 | 2000-04-13 | Daimler Chrysler Ag | Verfahren zur Herstellung faserverstärkter Kunststoffbauteile mit nicht-vollständig abwickelbarer Geometrie |
DE10062899A1 (de) * | 2000-12-16 | 2002-06-20 | Volkswagen Ag | Verfahren und Vorrichtung zur Herstellung eines Innenverkleidungsteils eines Fahrzeugs, insbesondere eines Kraftfahrzeugs, sowie Innenverkleidungsteil |
DE10156123B4 (de) * | 2001-11-16 | 2006-07-27 | Eads Deutschland Gmbh | Verfahren und Vorrichtung zur Herstellung von faserverstärkten Kunststoffbauteilen |
US7052573B2 (en) * | 2003-11-21 | 2006-05-30 | The Boeing Company | Method to eliminate undulations in a composite panel |
US7332049B2 (en) * | 2004-12-22 | 2008-02-19 | General Electric Company | Method for fabricating reinforced composite materials |
DE102005008252B4 (de) * | 2005-02-21 | 2014-03-20 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbund-Bauelements |
JP2008529849A (ja) | 2005-02-21 | 2008-08-07 | エアバス・ドイチュラント・ゲーエムベーハー | 繊維複合材料構造要素および繊維複合材料構造要素を製造する方法 |
DE102006002198B4 (de) * | 2006-01-16 | 2011-04-28 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbund-Bauelements |
DE102005026010B4 (de) * | 2005-06-07 | 2010-12-30 | Airbus Deutschland Gmbh | Verfahren zur Herstellung einer verstärkten Schale zur Bildung von Teilkomponenten für Luftfahrzeuge |
US7633040B2 (en) * | 2005-11-14 | 2009-12-15 | The Boeing Company | Bulk resin infusion system apparatus and method |
GB2447964B (en) * | 2007-03-29 | 2012-07-18 | Gurit Uk Ltd | Moulding material |
US8449709B2 (en) | 2007-05-25 | 2013-05-28 | The Boeing Company | Method of fabricating fiber reinforced composite structure having stepped surface |
DE102007048449A1 (de) | 2007-10-10 | 2009-04-23 | Eads Deutschland Gmbh | Auftriebsklappenträgersystem |
ITTO20070796A1 (it) * | 2007-11-08 | 2009-05-09 | Alenia Aeronautica Spa | Attrezzatura per infusione di resina in una preforma in stampo chiuso. |
DE102008015070B3 (de) * | 2008-03-19 | 2009-10-01 | Eurocopter Deutschland Gmbh | VAP-Autoklav-Verfahren zur Herstellung von Faserverbundbauteilen und Vorrichtung dafür |
DE102009047340B4 (de) | 2009-12-01 | 2011-07-14 | Airbus Operations GmbH, 21129 | Verfahren zum Bilden eines Strukturbauteils eines Luft- oder Raumfahrzeuges und Umformvorrichtung |
CA2803414C (fr) | 2010-07-02 | 2018-09-04 | Hexcel Holding Gmbh | Objet moule composite renforce par des fibres |
DE102011006032A1 (de) * | 2011-03-24 | 2012-09-27 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Strukturbauteils sowie Strukturbauteil |
DE102011079947A1 (de) * | 2011-07-27 | 2013-01-31 | Airbus Operations Gmbh | Vorrichtung zur Herstellung eines Klebebauteils mit Faserverbundkunststoffen sowie Verfahren |
FR2987779A1 (fr) * | 2012-03-12 | 2013-09-13 | Airbus Operations Sas | Procede de realisation d'une piece en materiau composite et outillage pour sa mise en oeuvre |
US20140166191A1 (en) * | 2012-12-14 | 2014-06-19 | Aurora Flight Sciences Corporation | Methods for combining components of varying stages of cure |
CN103963319B (zh) * | 2014-05-29 | 2016-06-15 | 上海飞机制造有限公司 | 一种复合材料加筋壁板的预浸料/树脂膜熔渗共固化成型方法 |
CN105904828A (zh) * | 2016-05-04 | 2016-08-31 | 哈尔滨飞机工业集团有限责任公司 | 一种飞机上板-板零件的成型方法 |
DE102016116024B4 (de) | 2016-08-29 | 2021-05-12 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Herstellen eines Faserverbundformteils durch sequenzielle Infusion |
US11332228B2 (en) | 2018-04-06 | 2022-05-17 | Aurora Flight Sciences Corporation | Aircraft fuselage with composite pre-form |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59165647A (ja) * | 1983-03-10 | 1984-09-18 | 東レ株式会社 | 複合材料用補強材 |
US4622091A (en) * | 1984-11-29 | 1986-11-11 | The Boeing Company | Resin film infusion process and apparatus |
US4816106A (en) * | 1984-12-13 | 1989-03-28 | Aeritalia Saipa - Gruppo Velivoli Da Trasporto | Method for the controlled curing of composites |
US4786343A (en) * | 1985-05-10 | 1988-11-22 | The Boeing Company | Method of making delamination resistant composites |
US4942013A (en) * | 1989-03-27 | 1990-07-17 | Mcdonnell Douglas Corporation | Vacuum resin impregnation process |
JPH03109437A (ja) * | 1989-09-21 | 1991-05-09 | Sekisui Chem Co Ltd | 光硬化性プリプレグシート及びその複合成形体の製造方法 |
JPH03109436A (ja) * | 1989-09-21 | 1991-05-09 | Sekisui Chem Co Ltd | 光硬化性プリプレグシート及び複合成形体の製造方法 |
US5593633A (en) * | 1990-05-03 | 1997-01-14 | Dull; Kenneth M. | Edge and surface breather for high temperature composite processing |
US5281388A (en) * | 1992-03-20 | 1994-01-25 | Mcdonnell Douglas Corporation | Resin impregnation process for producing a resin-fiber composite |
US5433165A (en) | 1994-03-30 | 1995-07-18 | Outboard Marine Corporation | Method of manufacturing a boat hull |
JPH07276233A (ja) * | 1994-04-08 | 1995-10-24 | Mitsubishi Heavy Ind Ltd | 複合材製多孔面板の製造方法 |
US5567499A (en) * | 1995-01-03 | 1996-10-22 | The Boeing Company | Resin transfer molding in combination with honeycomb core |
FR2744054B1 (fr) * | 1996-01-29 | 1998-04-30 | Aerospatiale | Procede de realisation de pieces en materiau composite a haute precision dimensionnelle mettant en oeuvre une polymerisation par ionisation et pieces ainsi obtenues |
US5980665A (en) * | 1996-05-31 | 1999-11-09 | The Boeing Company | Z-pin reinforced bonds for connecting composite structures |
US6139942A (en) * | 1997-02-06 | 2000-10-31 | Cytec Technology, Inc. | Resin composition, a fiber reinforced material having a partially impregnated resin and composites made therefrom |
DE19813104A1 (de) * | 1998-03-25 | 1999-09-30 | Daimler Chrysler Ag | Verfahren zur Herstellung von Faserverbundbauteilen |
DE19915083C1 (de) * | 1999-04-01 | 2000-04-13 | Daimler Chrysler Ag | Verfahren zur Herstellung faserverstärkter Kunststoffbauteile mit nicht-vollständig abwickelbarer Geometrie |
-
1999
- 1999-04-01 DE DE19915083A patent/DE19915083C1/de not_active Expired - Lifetime
-
2000
- 2000-03-24 SE SE0001065A patent/SE519225C2/sv not_active IP Right Cessation
- 2000-03-29 FR FR0003979A patent/FR2791600B1/fr not_active Expired - Lifetime
- 2000-03-30 ES ES200000794A patent/ES2176076B2/es not_active Expired - Fee Related
- 2000-03-31 GB GB0007914A patent/GB2351937B/en not_active Expired - Lifetime
- 2000-04-03 US US09/541,696 patent/US6527894B1/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE19915083C1 (de) | 2000-04-13 |
GB0007914D0 (en) | 2000-05-17 |
FR2791600A1 (fr) | 2000-10-06 |
SE0001065D0 (sv) | 2000-03-24 |
GB2351937B (en) | 2004-01-07 |
ES2176076A1 (es) | 2002-11-16 |
ES2176076B2 (es) | 2003-08-01 |
SE0001065L (sv) | 2000-10-02 |
SE519225C2 (sv) | 2003-02-04 |
US6527894B1 (en) | 2003-03-04 |
GB2351937A (en) | 2001-01-17 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 17 |
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PLFP | Fee payment |
Year of fee payment: 18 |
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PLFP | Fee payment |
Year of fee payment: 19 |
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PLFP | Fee payment |
Year of fee payment: 20 |