ES2034711T3 - Herramental para el moldeo de paneles auto-tensados en material compuesto. - Google Patents
Herramental para el moldeo de paneles auto-tensados en material compuesto.Info
- Publication number
- ES2034711T3 ES2034711T3 ES198989403042T ES89403042T ES2034711T3 ES 2034711 T3 ES2034711 T3 ES 2034711T3 ES 198989403042 T ES198989403042 T ES 198989403042T ES 89403042 T ES89403042 T ES 89403042T ES 2034711 T3 ES2034711 T3 ES 2034711T3
- Authority
- ES
- Spain
- Prior art keywords
- composite material
- panel
- volume
- plate
- tool
- 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
- 239000002131 composite material Substances 0.000 title abstract 2
- 238000000465 moulding Methods 0.000 title 1
- 238000001035 drying Methods 0.000 abstract 1
- 239000011159 matrix material Substances 0.000 abstract 1
- 230000002093 peripheral effect Effects 0.000 abstract 1
- 238000007789 sealing Methods 0.000 abstract 1
- 239000007787 solid Substances 0.000 abstract 1
- 238000001029 thermal curing Methods 0.000 abstract 1
Classifications
-
- 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
- B29D99/0017—Producing wall or panel-like structures, e.g. for hulls, fuselages, or buildings provided with ridges or ribs, e.g. joined ribs with filled hollow ridges
-
- 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
-
- 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
-
- 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
- B29C43/00—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor
- B29C43/02—Compression moulding, i.e. applying external pressure to flow the moulding material; Apparatus therefor of articles of definite length, i.e. discrete articles
- B29C43/10—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies
- B29C43/12—Isostatic pressing, i.e. using non-rigid pressure-exerting members against rigid parts or dies using bags surrounding the moulding material or using membranes contacting the moulding material
-
- 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
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S425/00—Plastic article or earthenware shaping or treating: apparatus
- Y10S425/06—Vacuum
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Architecture (AREA)
- Civil Engineering (AREA)
- Structural Engineering (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
Abstract
PARA REALIZAR EL MOLDEO DE PANELES AUTO-RIGIDIZADOS (A) DE MATERIAL COMPUESTO DE MATRIZ TERMOENDURECIBLE, SE UTILIZA UNA APARAMENTA QUE CONSTA DE UNA PLACA (10), UNA VEGIJA DE ESTANQUEIDAD (12) CUYO BORDE PERIFERICO ESTA UNIDO A LA PLACA MEDIANTE UN BURLETE DE ESTANQUEIDAD (14), Y UNOS PIEZAS DE CALIBRADO SOLIDAS E INDEFORMABLES (22). ESTANDO SITUADO EL PANEL (A) EN UN VOLUMEN ESTANCO (16) DELIMITADO ENTRE LA PLACA Y LA VEJIGA, MIENTRAS QUE LAS PIEZAS (22) ESTAN SITUADAS FUERA DE ESTE VOLUMEN, POR ENCIMA DE LA VEGIJA, ENTRE LOS REFUERZOS (C) DEL PANEL. LAS PIEZAS DE CALIBRADO (22) ESTAN ENLAZADAS POR UNA ESTRUCTURA RIGIDA (24). ASI, CUANDO EL VOLUMEN (16) SUFRE UNA DEPRESION Y CUANDO LA APARAMENTA SE COLOCA EN UNA CAMARA DE SECADO O EN UN AUTOCLAVE, SE APLICA UNA PRESION UNIFORME AL PANEL MEDIANTE LA VEJIGA (12) Y LAS PIEZAS (22) GARANTIZAN LA GEOMETRIA DE LOS REFUERZOS.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8814561A FR2638673B1 (fr) | 1988-11-08 | 1988-11-08 | Outillage pour le moulage de panneaux auto-raidis en materiau composite |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2034711T3 true ES2034711T3 (es) | 1993-04-01 |
Family
ID=9371675
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES198989403042T Expired - Lifetime ES2034711T3 (es) | 1988-11-08 | 1989-11-06 | Herramental para el moldeo de paneles auto-tensados en material compuesto. |
Country Status (6)
Country | Link |
---|---|
US (1) | US5015168A (es) |
EP (1) | EP0368734B1 (es) |
CA (1) | CA2002302C (es) |
DE (1) | DE68902454T2 (es) |
ES (1) | ES2034711T3 (es) |
FR (1) | FR2638673B1 (es) |
Families Citing this family (37)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2670153B1 (fr) * | 1990-12-05 | 1993-03-26 | Aerospatiale | Outillage pour le moulage de panneaux autoraidis en materiau composite. |
GB9103378D0 (en) * | 1991-02-19 | 1991-04-03 | British Aerospace | Progressive moulding and curing of composite materials |
GB9111887D0 (en) * | 1991-06-03 | 1991-07-24 | Klein Andre | Improvements in composite structures |
FR2691922B1 (fr) * | 1992-06-03 | 1994-07-22 | Snecma | Procede et dispositif de moulage de piece en materiau composite constituee de deux secteurs. |
US5622733A (en) * | 1994-10-04 | 1997-04-22 | Rockwell International Corporation | Tooling for the fabrication of composite hollow crown-stiffened skins and panels |
US5683646A (en) * | 1995-05-10 | 1997-11-04 | Mcdonnell Douglas Corporation | Fabrication of large hollow composite structure with precisely defined outer surface |
DE19536675C1 (de) * | 1995-09-30 | 1997-02-20 | Deutsche Forsch Luft Raumfahrt | Vorrichtung und Verfahren zur Herstellung von großflächigen Bauelementen nach dem RTM-Verfahren |
US5882462A (en) * | 1996-02-02 | 1999-03-16 | Dow-United Technologies Composite Products | Method for fabricating a corrugated composite channel |
JPH10146898A (ja) * | 1996-11-15 | 1998-06-02 | Honda Motor Co Ltd | 繊維強化複合材の成形方法 |
WO1999015323A1 (en) * | 1997-09-19 | 1999-04-01 | Dow-United Technologies Composite Products, Inc. | Method for fabricating a corrugated composite channel |
SE519268C2 (sv) * | 1999-12-23 | 2003-02-11 | Saab Ab | Anordning för att hålla en artikel och anläggning för värmebehandling av en artikel |
GB0021955D0 (en) * | 2000-09-07 | 2000-10-25 | Bae Systems Plc | Stiffening means for structural components |
SE519536C2 (sv) * | 2001-05-11 | 2003-03-11 | Saab Ab | Sätt och anordning för framställning av kompositmaterial och limmade plåtartiklar |
US6840750B2 (en) * | 2001-06-11 | 2005-01-11 | The Boeing Company | Resin infusion mold tool system and vacuum assisted resin transfer molding with subsequent pressure bleed |
FR2863198B1 (fr) * | 2003-12-04 | 2006-03-03 | Airbus France | Panneaux auto-raidis en composite pre-impregne et procedes de mise en place des elements de tels panneaux |
US7622066B2 (en) * | 2004-07-26 | 2009-11-24 | The Boeing Company | Methods and systems for manufacturing composite parts with female tools |
US8601694B2 (en) | 2008-06-13 | 2013-12-10 | The Boeing Company | Method for forming and installing stringers |
US8557165B2 (en) | 2008-10-25 | 2013-10-15 | The Boeing Company | Forming highly contoured composite parts |
CN101370643B (zh) * | 2005-12-30 | 2011-02-02 | 空客西班牙公司 | 具有u-型加强构件的复合面板的制备方法 |
GB0622691D0 (en) * | 2006-11-14 | 2006-12-27 | Airbus Uk Ltd | Method and apparatus for controlling the geometry of a composite component |
DE102007062872A1 (de) | 2007-12-28 | 2009-07-09 | Airbus Deutschland Gmbh | Verfahren zur Herstellung eines Profils aus Faserverbundwerkstoff |
US8052826B2 (en) | 2009-03-24 | 2011-11-08 | The Boeing Company | Method of making bead-stiffened composite parts and parts made thereby |
DE102010062871A1 (de) * | 2009-12-29 | 2011-06-30 | Airbus Operations GmbH, 21129 | Infusionsverfahren und Aufbau eines Infusionsverfahrens |
DE102010025068B4 (de) * | 2010-06-25 | 2016-07-28 | Airbus Defence and Space GmbH | Vorrichtung und Verfahren zur Herstellung von faserverstärkten Bauteilen |
US8961732B2 (en) | 2011-01-03 | 2015-02-24 | The Boeing Company | Method and device for compressing a composite radius |
US9023265B1 (en) | 2013-01-28 | 2015-05-05 | The Boeing Company | Systems, tools, and methods for forming corrugated structures and apparatuses including corrugated structures |
ES2626352T3 (es) * | 2013-05-30 | 2017-07-24 | Airbus Operations S.L. | Herramienta híbrida para curar piezas de material compuesto |
WO2015169272A1 (de) * | 2014-05-06 | 2015-11-12 | Piekenbrink Composite Gmbh | Segmentierte vakuumhaube |
US9511520B1 (en) * | 2014-08-20 | 2016-12-06 | The Boeing Company | Method, apparatus and device for preventing vacuum bag wrinkling |
JP6463094B2 (ja) * | 2014-11-25 | 2019-01-30 | 三菱重工業株式会社 | 接合装置及び接合方法 |
US11104113B2 (en) | 2017-04-19 | 2021-08-31 | The Boeing Company | Systems and methods for assembling elongate composite structures |
US10710319B2 (en) * | 2017-08-02 | 2020-07-14 | The Boeing Company | Controlling application of forces to different portions of object surface using bladder |
DE102019114710A1 (de) * | 2019-05-31 | 2020-12-03 | Airbus Operations Gmbh | Vorrichtung und Verfahren |
US11498288B2 (en) | 2020-02-11 | 2022-11-15 | The Boeing Company | Forming systems and methods for drape forming a composite charge |
US11260607B2 (en) | 2020-02-11 | 2022-03-01 | The Boeing Company | Forming systems and methods for drape forming a composite charge |
US11931975B2 (en) | 2021-02-19 | 2024-03-19 | The Boeing Company | Forming systems and methods for forming an elongate charge of composite material |
FR3121383A1 (fr) * | 2021-04-01 | 2022-10-07 | Airbus Operations | Outil pour la fabrication d’un panneau auto-raidi et procédé de fabrication d’un panneau auto-raidi utilisant un tel outil |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3666600A (en) * | 1969-03-10 | 1972-05-30 | North American Rockwell | Apparatus for forming layup laminate |
US3703422A (en) * | 1970-01-02 | 1972-11-21 | North American Rockwell | Polyaromatic resin faced honeycomb panel and method for making same |
US3861977A (en) * | 1972-11-21 | 1975-01-21 | Rudkin Wiley Corp | Process for vacuum bag molding |
US3972766A (en) * | 1975-01-17 | 1976-08-03 | Andre Fontvieille | Apparatus for fabricating flat objects |
DE2650859C3 (de) * | 1976-11-06 | 1979-10-04 | Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen | Verfahren zur Herstellung von Großbauteilen aus faserverstärktem Kunststoff und Einrichtung zur Durchfuhrung des Verfahrens |
FR2440831A1 (fr) * | 1978-11-07 | 1980-06-06 | Dassault Avions | Panneaux a base de fibres a haute resistance, particulierement applicables a la construction des avions |
DE3418110C2 (de) * | 1984-05-16 | 1986-04-03 | Dornier Gmbh, 7990 Friedrichshafen | Verfahren zur Herstellung von ausgesteiften, tragenden Strukturen aus faserverstärktem härtbaren Kunststoff |
US4608220A (en) * | 1984-12-20 | 1986-08-26 | The Boeing Company | Method of forming composite material articles |
GB8508419D0 (en) * | 1985-04-01 | 1985-05-09 | Short Brothers Ltd | Moulding fibre reinforced resin |
DE3643502A1 (de) * | 1986-12-19 | 1988-07-21 | Messerschmitt Boelkow Blohm | Vorrichtung zum pressen einer form zur herstellung einer leichtbauschale aus faserverstaerktem kunststoff |
US4915896A (en) * | 1987-09-01 | 1990-04-10 | Phillips Petroleum Company | Vacuum bagging process for fiber reinforced thermoplastics |
-
1988
- 1988-11-08 FR FR8814561A patent/FR2638673B1/fr not_active Expired - Lifetime
-
1989
- 1989-10-19 US US07/424,066 patent/US5015168A/en not_active Expired - Lifetime
- 1989-11-06 ES ES198989403042T patent/ES2034711T3/es not_active Expired - Lifetime
- 1989-11-06 DE DE8989403042T patent/DE68902454T2/de not_active Expired - Fee Related
- 1989-11-06 CA CA002002302A patent/CA2002302C/en not_active Expired - Lifetime
- 1989-11-06 EP EP89403042A patent/EP0368734B1/fr not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5015168A (en) | 1991-05-14 |
DE68902454D1 (de) | 1992-09-17 |
FR2638673B1 (fr) | 1991-03-22 |
FR2638673A1 (fr) | 1990-05-11 |
CA2002302A1 (en) | 1990-05-08 |
EP0368734B1 (fr) | 1992-08-12 |
DE68902454T2 (de) | 1993-02-25 |
CA2002302C (en) | 1998-05-12 |
EP0368734A1 (fr) | 1990-05-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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