ES2176076B2 - Procedimiento para la fabricacion de unas piezas de construccion de material plastico reforzado por fibras y con una forma geometrica no desarrollable por completo. - Google Patents
Procedimiento para la fabricacion de unas piezas de construccion de material plastico reforzado por fibras y con una forma geometrica no desarrollable por completo.Info
- Publication number
- ES2176076B2 ES2176076B2 ES200000794A ES200000794A ES2176076B2 ES 2176076 B2 ES2176076 B2 ES 2176076B2 ES 200000794 A ES200000794 A ES 200000794A ES 200000794 A ES200000794 A ES 200000794A ES 2176076 B2 ES2176076 B2 ES 2176076B2
- Authority
- ES
- Spain
- Prior art keywords
- developable
- procedure
- manufacture
- plastic material
- construction parts
- 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 - Fee Related
Links
- 238000010276 construction Methods 0.000 title abstract 4
- 238000004519 manufacturing process Methods 0.000 title abstract 2
- 239000000463 material Substances 0.000 title abstract 2
- 238000000034 method Methods 0.000 title abstract 2
- 229920002430 Fibre-reinforced plastic Polymers 0.000 title 1
- 239000011151 fibre-reinforced plastic Substances 0.000 title 1
- 239000004753 textile Substances 0.000 abstract 2
- 239000000835 fiber Substances 0.000 abstract 1
- 239000011347 resin Substances 0.000 abstract 1
- 229920005989 resin Polymers 0.000 abstract 1
- 238000011282 treatment Methods 0.000 abstract 1
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
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Mechanical Engineering (AREA)
- Moulding By Coating Moulds (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Procedimiento para la fabricación de unas piezas de construcción de material plástico reforzado por fibras y con una forma geométrica no desarrollable por completo. Este objetivo se alcanza según la invención, debido a que la parte desarrollable de la pieza de construcción de material plástico (1) es prefabricada automáticamente a la manera de un producto impregnado previamente (2) (pre-preg), porque la parte no desarrollable de la pieza de construcción de material plástico (1) es prefabricada a la manera de un producto textil semielaborado (3), porque el producto textil semielaborado (3) forrado con una película de resina (4) y ensamblado con el producto impregnado previamente (2) se dispone en un dispositivo de curado (5) con la campana de vacío (7) flexible, y porque el dispositivo de curado (5) después de montado y hecho el vacío se somete a ciertos tratamientos de temperatura y presión en el interior de un autoclave.
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 |
---|---|
ES2176076A1 ES2176076A1 (es) | 2002-11-16 |
ES2176076B2 true ES2176076B2 (es) | 2003-08-01 |
Family
ID=7903389
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES200000794A Expired - Fee Related ES2176076B2 (es) | 1999-04-01 | 2000-03-30 | Procedimiento para la fabricacion de unas piezas de construccion de material plastico reforzado por fibras y con una forma geometrica no desarrollable por completo. |
Country Status (6)
Country | Link |
---|---|
US (1) | US6527894B1 (es) |
DE (1) | DE19915083C1 (es) |
ES (1) | ES2176076B2 (es) |
FR (1) | FR2791600B1 (es) |
GB (1) | GB2351937B (es) |
SE (1) | SE519225C2 (es) |
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 |
DE102006002198B4 (de) * | 2006-01-16 | 2011-04-28 | Airbus Operations Gmbh | Verfahren zur Herstellung eines Faserverbund-Bauelements |
RU2419542C2 (ru) | 2005-02-21 | 2011-05-27 | Эйрбас Дойчланд Гмбх | Волокнистый композитный конструктивный элемент и способ изготовления волокнистого композитного конструктивного элемента |
DE102005008252B4 (de) * | 2005-02-21 | 2014-03-20 | 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 |
EP2588296B1 (en) | 2010-07-02 | 2018-05-02 | Hexcel Holding GmbH | Fibre reinforced composite moulding |
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 |
---|---|
SE519225C2 (sv) | 2003-02-04 |
SE0001065L (sv) | 2000-10-02 |
FR2791600A1 (fr) | 2000-10-06 |
DE19915083C1 (de) | 2000-04-13 |
GB0007914D0 (en) | 2000-05-17 |
FR2791600B1 (fr) | 2005-02-25 |
US6527894B1 (en) | 2003-03-04 |
GB2351937A (en) | 2001-01-17 |
ES2176076A1 (es) | 2002-11-16 |
SE0001065D0 (sv) | 2000-03-24 |
GB2351937B (en) | 2004-01-07 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 2176076B2 Country of ref document: ES |
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PC2A | Transfer of patent | ||
FD2A | Announcement of lapse in spain |
Effective date: 20200706 |