WO2002030657A1 - Procede, appareil et matrice de fabrication de plaques composites - Google Patents
Procede, appareil et matrice de fabrication de plaques composites Download PDFInfo
- Publication number
- WO2002030657A1 WO2002030657A1 PCT/DK2001/000669 DK0100669W WO0230657A1 WO 2002030657 A1 WO2002030657 A1 WO 2002030657A1 DK 0100669 W DK0100669 W DK 0100669W WO 0230657 A1 WO0230657 A1 WO 0230657A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fibres
- matrix
- composite
- conducting
- web
- 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.)
- Ceased
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
- B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
- B29C70/882—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced partly or totally electrically conductive, e.g. for EMI shielding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29B—PREPARATION OR PRETREATMENT OF THE MATERIAL TO BE SHAPED; MAKING GRANULES OR PREFORMS; RECOVERY OF PLASTICS OR OTHER CONSTITUENTS OF WASTE MATERIAL CONTAINING PLASTICS
- B29B15/00—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00
- B29B15/08—Pretreatment of the material to be shaped, not covered by groups B29B7/00 - B29B13/00 of reinforcements or fillers
- B29B15/10—Coating or impregnating independently of the moulding or shaping step
- B29B15/12—Coating or impregnating independently of the moulding or shaping step of reinforcements of indefinite length
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/0272—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould using lost heating elements, i.e. heating means incorporated and remaining in the formed article
-
- 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
- B29C70/50—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC]
- B29C70/504—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands
- B29C70/506—Shaping or impregnating by compression not applied for producing articles of indefinite length, e.g. prepregs, sheet moulding compounds [SMC] or cross moulding compounds [XMC] using rollers or pressure bands and impregnating by melting a solid material, e.g. sheet, powder, fibres
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C2035/0211—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould resistance heating
-
- 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
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
- B29C35/0805—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
- B29C2035/0811—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using induction
-
- 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
- B29K2995/00—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds
- B29K2995/0003—Properties of moulding materials, reinforcements, fillers, preformed parts or moulds having particular electrical or magnetic properties, e.g. piezoelectric
- B29K2995/0005—Conductive
Definitions
- the present invention concerns a method of production of composite plates as described in the introductory part of claim 1.
- the invention also concerns an apparatus for production of composite plates, a matrix of fibre, a composite plate, a tubular composite plate, a product containing a composite plate and a method for post-forming of a composite plate.
- fibres are to have certain preferred directions, for example, lie at certain angles with respect to the direc- tion of web in the production.
- Such fibre matrices are called web. This term covers not only woven matrices but also matrices where long fibres in array are assembled by stitching.
- web is used for long fibre composites as opposed to "non- woven" materials which are mixtures of short fibres and are used, for example, for insulation mats.
- a so-called belt press In order to produce composite plates in great lengths, a so-called belt press can be used, which is known e.g. from WO 97/26397.
- a matrix of fibres is passed through a heating process and a pressing process, where the pressing process takes place between pressure rollers with belts running around them in such a way, that composite plate is produced as lengths between the belts on each side of the plate.
- belt presses are very expensive machines, why other apparatuses have been developed for the production of composite plates in web form without using belts around the rollers. These apparatuses cost only a small fraction of the corresponding belt presses.
- This method has some disadvantages.
- To achieve a complete melting of web it is exposed to a strong thermal radiation on a preheating stage.
- the disadvantage of this preheating stage is that a temperature is reached on the external side of the web, which is close to decomposition temperature for the polymer, for example, 230°C for poly- propylene, abbreviated PP, while the temperature in the center of the web is much lower, for example, 140°C, and often below melting point, which for PP is 165°C. Consequently, the web undergoes a decomposition of external polymer fibres, which is very undesirable but accepted in order to obtain the necessary preheating for the final temperature at which the polymer melts to consolidate the composite plate.
- Another disadvantage is lack of homogenization in the material when the web initially is heated to the melting temperature and then pressed at a lower temperature. Homogenization is the process in which the polymer melts completely and then settles, enclosing the reinforcement material.
- the prior art methods have to run at a relatively high speed in order to minimize the time span between the heating and the subsequent pressing with cold rollers. But at high speed it is impossible to heat the web up to the correct working temperature, which is somewhat higher than the melting temperature and preferably close to decomposition temperature. This is one of the reasons why the thermal radiation preheating stage is used in the prior art methods and systems. It has, however, not been possible to solve this problem completely as high process speed results in poor preheating and unsatisfactory homogenization of the material, while slow process speed results in better heating but, on the other hand, it takes long time for the web to reach the pressing rollers why the pressing takes place at too low temperature, also resulting in unsatisfactory homogenization.
- the purpose of this invention is to provide a method and an apparatus for production of composite plates from the web, where the above described disadvantages are avoided, and where preheating of web by thermal radiation is not necessary.
- matrix of fibres a composite which can include short, non-woven fibres that are stitched or pressed together, and/or long fibres, woven or sewn together.
- the invention will be explained with a composite web as an example, which however shall by no means delimit the invention to not being applicable with so-called non- woven matrices of fibres.
- Temperature action for the production of composite plates is achieved by heat transfer from an electrically conducting web or fibre forming part of composite matrix and which is heated by means of electric current.
- the current conducting fibres may, for example, form part of the matrix during the production of the matrix, but it is also possible to put these fibres or stitch them into the matrix subsequently.
- conducting fibres which are commercially available. These conducting fibres, which are e.g. used for heating clothes, can be heated up to above 200°C, even up to 400° C, which makes them suitable for heating the web. If the matrix is heated to a temperature above the melting point for the polymer in the matrix, for example 200° C for polypropylene, conducting fibres will melt together with the polymer and possible other fibres in the matrix. It is assumed that melting temperature of conducting fibres is higher than melting temperature of the polymer in the matrix.
- the web is heated up and pressed at a temperature where at least one, however preferably one, of the composite materials are mel- ting.
- the composite is made of polymer fibres, which by melting settle around reinforcing fibres, such as glass, and other fibres in the composite, if any. Pressing may occur by placing the web, which is at a temperature higher than the melting temperature of the polymer, between two press plates, which are then moved to- wards each other until a predetermined distance. The composite plate formed thereby will then assume this predetermined dimension at the most.
- pressing can be performed by leading the web between a pair of rollers adjusted to a certain distance or a certain pressing force whereby the composite plate is formed as a long web which after cooling, when the polymer has set or hardened, can be rolled together, depending on the flexibility, for further transport.
- Heating of the web which occurs by conducting current through the web, can be achieved by conveying the web over a first and a second roller with electric potential bet- ween these rollers for conduction electric current through the conducting fibres in the web between the first and the second roller.
- Such two rollers which are acting as electrodes, can with advantage be used respectively before and after the press mold. It is, however, also possible that electric potential is established between a first roller and the press mold itself.
- the web can be formed in different ways and may comprise fibres of PP, PET or
- PTFE as well as fibres of reinforcing material, such as glass fibre, carbon fibre, ara- mide fibres, kevlar fibres, metal fibres, carbon coated glass fibres, vegetable fibres and other organic fibres, or synthetic fibres.
- the web according to the invention also contains current carrying fibres.
- Such current carrying fibres in the web can, for example, be carbon fibres or metal fibres woven or stitched into a web of polymer fibres and reinforcing fibres, preferably glass fibres. It is also possible, however, for reinforcing fibres to act as current conducting fibres. Carbon fibres can, for example, constitute the reinforcing material. But also glass fibres as reinforcing material can be made conducting by coating their surface with a conducting material. The web has proved to be particularly usable if the share of reinforcing fibres in the web is between 40% and 80%, preferably between 60% and 70%, and most preferred 60%.
- Cooling of the web after pressing can be performed in different ways, but it is preferred that the web is cold pressed by at least one rotating cold roller.
- the roller acts as an additional mould for the composite plate where, for example, the surface of composite plate can be structured.
- Such structuring in which embossing of the surface may form a part in the shape of, for example, patterns or logos, may, however, be done during pressing in hot condition.
- the matrix has been supplied with contact tracks, e.g. alongside the track, for electric contact with skates (like collector shoes) or rollers suited for this purpose.
- Examples of applications, where subsequent heating is desirable, are especially those when the composite has to be post-formed, i.e. formed after actual production of con- solidated composite.
- the composite is heated to a temperature below melting point, yet high enough for plastic deformation of the composite.
- a differentiated forming may be performed as these areas will be softer than the others.
- Heating of the composite is also a useful property of a composite according to the invention.
- such a composite can very easily be kept frost-free in cold areas, for example, if used for feed or drinking troughs in outdoors farming of domestic animals in the winter time.
- the composite can be very usable for rooms requiring heating and particularly if a very uniform heating is required without significant temperature gradients.
- Another application of the composite is on inside walls of caravans or railway cars, which are known for lack of comfort in cold seasons as the walls are cold.
- the inside walls can be heated up in a simple way, thus avoiding such discomfort.
- One more application of the conductive composite material is to use it as a screening wall for electronic equipment, for example in mobile or stationary military installations.
- Such screening can, for example, be used for protection from tapping.
- the composite web it is further possible to add a surface layer on the composite web, for example, a synthetic material or metal layer.
- a surface layer on the composite web for example, a synthetic material or metal layer.
- the surface of the composite web can be structured if this is suitable.
- FIG. 1 illustrates the production of a composite plate according to the invention
- FIG. 2 illustrates the second production method according to the invention
- FIG. 3 illustrates the third production method according to the invention
- FIG. 4 illustrates the fourth production method according to the invention
- FIG. 5 shows a matrix according to the invention, viewed from the flat side
- FIG. 6 shows an alternative production method for composite plates in accordance with the invention, where the composite plate is shaped as a pipe
- FIG. 7 shows a second alternative production method for composite plates according to the invention, where the composite plate is shaped as a pipe.
- FIG. 1 illustrates production of a composite plate according to the invention.
- FIG. 2 illustrates a production method according to the invention, in which the electric potential is established between the first set of rollers 4, 4' and pressure rollers 3, 3'.
- FIG. 3 illustrates a production method according to the invention, where the web is subjected to pressure by a set of pressure plates 10, 10'. Electric potential is established between the first set of rollers 4, 4' and pressure plates 10, 10'.
- belt presses can be used.
- FIG. 4 illustrates a production method according to the invention, where different electric potentials 8, 8', 8" are established between several sets of rollers 4, 4', 9, 9', 3, 3' and 6, 6'.
- the matrix in this process is subjected to pressure between the rollers 3,3', but it is also possible to subject the matrix to pressure between the other rollers, if this is considered to be necessary.
- the distance between different set of rollers, 4, 4', 6, 6', 3, 3', 9, 9' can vary according to need.
- a long distance between the rollers allows choosing a higher production speed compared to prior art techniques.
- FIG. 5 shows a matrix 1 according to the invention seen towards the flat side.
- a feeding roller 2 is also shown together with one of the pressure rollers, 3.
- the matrix is furnished with contact tracks 11, 11' which are designed for contacting external contact rollers 12, 12', contact skates, shoes or similar, in order to ensure heating of matrix 1 during forming.
- an electric potential 8 is established between contact rollers 12, 12'.
- the conducting tracks will still be accessible for contacting after consolidation of composite web 7. This way a later post-forming can be performed in a simple way, as discussed above.
- FIG. 6 shows an alternative production method for composite plates according to the invention, where the composite plate is shaped as a pipe.
- Such composite pipe is obtained by pulling a fibre stocking 1, preferably web, over an inner mould 14, for e- xample, a steel cylinder with Teflon coating. After that, the web 1 is heated by conducting current through two contact tracks 11, 11', which run, for example, longitudi- nally or transversely of the stocking, or in diagonal tracks.
- the stocking is encased by an external press mold 13.
- Pipe-shaped composite plates can also be produced by diagonal wrapping of a cylindrical steel mold 14 with a long web-shaped matrix according to the invention as illu- strated in FIG. 7.
- the matrix 1 is made with three contact tracks, namely two contact tracks 11, 11' along the sides and a third track 11", for example, in the middle of composite web 1.
- Diagonal wrapping allows contact tracks 11, 11' to be in contact with each otlier. Passage of current through the matrix is then achieved by the power source suitably contacting the central contact track 11" and at least one of contact tracks 11, 11' at the sides of the matrix.
- local heating of pipes can be appropriate for bending or other adjustment of pipes during installation.
- Heating the composite with conducting fibres can also be supplemented with techniques comprising magnetic induction, where the current is induced in the conductive fibres by means of varying magnetic fields.
- the advantage of such forms of technique is that there is no need for contact, for example, by means of contact tracks.
- such heating does not require the conductive fibres to be oriented in a certain direction or to have a certain pattern.
- thermosetting composite plates have been explained in connection with webs containing a thermoplastic polymer. It is, however, within the ability of the skilled in the art to utilize the invention by using hot fibres in thermosetting composite plates.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- Health & Medical Sciences (AREA)
- Oral & Maxillofacial Surgery (AREA)
- Thermal Sciences (AREA)
- Casting Or Compression Moulding Of Plastics Or The Like (AREA)
- Moulding By Coating Moulds (AREA)
- Laminated Bodies (AREA)
Abstract
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| AU2002210381A AU2002210381A1 (en) | 2000-10-13 | 2001-10-12 | A method, an apparatus and a matrix for making composite plates |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DK200001526A DK173919B1 (da) | 2000-10-13 | 2000-10-13 | Fremgangsmåde, apparat og matrix af tråde til fremstilling af kompositplader, disse plader og deres anvendelse |
| DKPA200001526 | 2000-10-13 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| WO2002030657A1 true WO2002030657A1 (fr) | 2002-04-18 |
Family
ID=8159786
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| PCT/DK2001/000669 Ceased WO2002030657A1 (fr) | 2000-10-13 | 2001-10-12 | Procede, appareil et matrice de fabrication de plaques composites |
Country Status (3)
| Country | Link |
|---|---|
| AU (1) | AU2002210381A1 (fr) |
| DK (1) | DK173919B1 (fr) |
| WO (1) | WO2002030657A1 (fr) |
Cited By (21)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2003026821A1 (fr) * | 2001-09-25 | 2003-04-03 | Gerhard Jack K | Appareil et procede de stratification par induction de materiaux composites renforces par des fibres conductrices |
| EP1526214A1 (fr) * | 2003-10-21 | 2005-04-27 | Materials Technics Holding Société Anonyme | Procede et dispositif d'impregnation d'un reseau fibreux par de la poudre utilisant un champ electrostatique alternatif |
| WO2007003879A1 (fr) * | 2005-06-30 | 2007-01-11 | Bae Systems Plc | Structure autoréparatrice |
| DE102011056686A1 (de) * | 2011-12-20 | 2013-06-20 | Institut Für Verbundwerkstoffe Gmbh | Verfahren zur Herstellung eines Faserverbundwerkstoffes, ein nach dem Verfahren hergestellter Faserverbundwerkstoff sowie eine Vorrichtung zur Durchführung des Verfahrens |
| US20130314491A1 (en) * | 2012-05-23 | 2013-11-28 | Google, Inc. | Multimedia conference endpoint transfer system |
| DE102012019915A1 (de) * | 2012-10-11 | 2014-04-17 | Premium Aerotec Gmbh | Verfahren zum Bereitstellen eines Faservorformlings zur Herstellung eines Faserverbundbauteils, sowie Transporteinrichtung für einen Fasermaterialzuschnitt |
| WO2014075663A1 (fr) * | 2012-11-19 | 2014-05-22 | Universität Stuttgart | Procédé et dispositif pour la fabrication de tôles organiques mises en forme |
| DE102013208426A1 (de) * | 2013-05-07 | 2014-11-13 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren und Vorrichtung zur Verarbeitung von Carbonfasersträngen |
| EP2821200A1 (fr) * | 2013-07-05 | 2015-01-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Dispositif de régulation de préformes en fibres |
| EP2821211A1 (fr) * | 2013-07-05 | 2015-01-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Dispositif de transport pour semi-produits |
| DE102013107102A1 (de) * | 2013-07-05 | 2015-01-08 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Faserhalbzeug-Temperiervorrichtung |
| WO2015005854A1 (fr) * | 2013-07-01 | 2015-01-15 | Sik - Institutet För Livsmedel Och Bioteknik Ab | Matériau composite façonnable et son procédé de préparation |
| CN104552986A (zh) * | 2014-12-30 | 2015-04-29 | 吉林大学 | 一种树脂基纤维增强复合材料连续轧制的生产方法 |
| DE102014212000A1 (de) * | 2014-06-23 | 2015-12-24 | Technische Universität Dresden | Verfahren und Vorrichtung zum thermischen Bearbeiten von textilverstärkten Faserverbundwerkstücken |
| WO2016087127A1 (fr) * | 2014-12-01 | 2016-06-09 | Thyssenkrupp Steel Europe Ag | Matériau composite fibreux, procédé de fabrication d'un élément composite et utilisation dudit matériau composite fibreux |
| US20160185014A1 (en) * | 2014-12-30 | 2016-06-30 | Deutsches Zentrum Fuer Luft- Und Raumfahrt E.V. | Fibrous-preform conveying device |
| DE102016110323A1 (de) | 2016-06-03 | 2017-12-07 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Fasertemperiereinrichtung, Faserappliziervorrichtung, Faserlegeanlage sowie Verfahren zum Temperieren |
| DE102018128086A1 (de) * | 2018-11-09 | 2020-05-14 | Bayerische Motoren Werke Aktiengesellschaft | Verfahren zur thermoplastischen Pultrusion eines Faserverbundwerkstoffs und Vorrichtung zur thermoplastischen Pultrusion eines Faserverbundwerkstoffs |
| CN111941988A (zh) * | 2019-05-15 | 2020-11-17 | 广州市香港科大霍英东研究院 | 一种用于复合材料连续层间粘接的辊压设备及其使用方法 |
| DE102020118703A1 (de) | 2020-07-15 | 2022-01-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren und Vorrichtung zum Imprägnieren mindestens eines Fasermaterials |
| DE102020118697A1 (de) | 2020-07-15 | 2022-01-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren und Vorrichtung zum Imprägnieren mindestens eines Fasermaterials |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102019005913A1 (de) * | 2019-08-22 | 2021-02-25 | Siempelkamp Maschinen- Und Anlagenbau Gmbh | Verfahren und Vorrichtung zum Herstellen eines Bauteils aus einem Faserverbundwerkstoff |
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| EP0321114A2 (fr) * | 1987-12-10 | 1989-06-21 | Imperial Chemical Industries Plc | Procédé de liaison de matières |
| US5500511A (en) * | 1991-10-18 | 1996-03-19 | The Boeing Company | Tailored susceptors for induction welding of thermoplastic |
| US5648137A (en) * | 1994-08-08 | 1997-07-15 | Blackmore; Richard | Advanced cured resin composite parts and method of forming such parts |
| WO2001060578A1 (fr) * | 2000-02-17 | 2001-08-23 | Thermocomp A/S | Procede et appareil de production de feuilles composites |
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- 2000-10-13 DK DK200001526A patent/DK173919B1/da not_active IP Right Cessation
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- 2001-10-12 WO PCT/DK2001/000669 patent/WO2002030657A1/fr not_active Ceased
- 2001-10-12 AU AU2002210381A patent/AU2002210381A1/en not_active Abandoned
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0321114A2 (fr) * | 1987-12-10 | 1989-06-21 | Imperial Chemical Industries Plc | Procédé de liaison de matières |
| US5500511A (en) * | 1991-10-18 | 1996-03-19 | The Boeing Company | Tailored susceptors for induction welding of thermoplastic |
| US5648137A (en) * | 1994-08-08 | 1997-07-15 | Blackmore; Richard | Advanced cured resin composite parts and method of forming such parts |
| WO2001060578A1 (fr) * | 2000-02-17 | 2001-08-23 | Thermocomp A/S | Procede et appareil de production de feuilles composites |
Cited By (39)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6881374B2 (en) | 2001-09-25 | 2005-04-19 | The United States Of America As Represented By The Secretary Of The Army | Method for induction lamination of electrically conductive fiber reinforced composite materials |
| US7419373B2 (en) | 2001-09-25 | 2008-09-02 | Alliant Techsystems Inc. | Apparatus and method for induction lamination of electrically conductive fiber-reinforced composite materials |
| WO2003026821A1 (fr) * | 2001-09-25 | 2003-04-03 | Gerhard Jack K | Appareil et procede de stratification par induction de materiaux composites renforces par des fibres conductrices |
| EP1526214A1 (fr) * | 2003-10-21 | 2005-04-27 | Materials Technics Holding Société Anonyme | Procede et dispositif d'impregnation d'un reseau fibreux par de la poudre utilisant un champ electrostatique alternatif |
| WO2005038123A1 (fr) * | 2003-10-21 | 2005-04-28 | Materials Technics Holding Sa | Procede et dispositif d'impregnation d'un reseau fibreux, par de la poudre un champ electrostatic alternatif |
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| WO2007003879A1 (fr) * | 2005-06-30 | 2007-01-11 | Bae Systems Plc | Structure autoréparatrice |
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| DE102020118703A1 (de) | 2020-07-15 | 2022-01-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren und Vorrichtung zum Imprägnieren mindestens eines Fasermaterials |
| DE102020118697A1 (de) | 2020-07-15 | 2022-01-20 | Deutsches Zentrum für Luft- und Raumfahrt e.V. | Verfahren und Vorrichtung zum Imprägnieren mindestens eines Fasermaterials |
Also Published As
| Publication number | Publication date |
|---|---|
| DK173919B1 (da) | 2002-02-18 |
| DK200001526A (da) | 2002-02-18 |
| AU2002210381A1 (en) | 2002-04-22 |
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