WO2006134079A1 - Composite part such as a panel, comprising a honeycomb structure - Google Patents

Composite part such as a panel, comprising a honeycomb structure Download PDF

Info

Publication number
WO2006134079A1
WO2006134079A1 PCT/EP2006/063065 EP2006063065W WO2006134079A1 WO 2006134079 A1 WO2006134079 A1 WO 2006134079A1 EP 2006063065 W EP2006063065 W EP 2006063065W WO 2006134079 A1 WO2006134079 A1 WO 2006134079A1
Authority
WO
WIPO (PCT)
Prior art keywords
foam
honeycomb structure
cells
part according
facing
Prior art date
Application number
PCT/EP2006/063065
Other languages
French (fr)
Inventor
Antoine Antoine
Original Assignee
Antoine Antoine
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Antoine Antoine filed Critical Antoine Antoine
Priority to DE202006020359U priority Critical patent/DE202006020359U1/en
Publication of WO2006134079A1 publication Critical patent/WO2006134079A1/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C44/00Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/12Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
    • B29C44/18Filling preformed cavities
    • B29C44/186Filling multiple cavities
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C44/00Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/12Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
    • B29C44/18Filling preformed cavities
    • B29C44/188Sealing off parts of the cavities
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C59/00Surface shaping of articles, e.g. embossing; Apparatus therefor
    • B29C59/10Surface shaping of articles, e.g. embossing; Apparatus therefor by electric discharge treatment
    • B29C59/103Surface shaping of articles, e.g. embossing; Apparatus therefor by electric discharge treatment of profiled articles, e.g. hollow or tubular articles
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C59/00Surface shaping of articles, e.g. embossing; Apparatus therefor
    • B29C59/14Surface shaping of articles, e.g. embossing; Apparatus therefor by plasma treatment
    • B29C59/142Surface shaping of articles, e.g. embossing; Apparatus therefor by plasma treatment of profiled articles, e.g. hollow or tubular articles

Definitions

  • Composite part such as a panel, having a honeycomb honeycomb structure.
  • the invention relates to a panel or composite part comprising honeycomb honeycomb structure.
  • panels are frequently used for which good qualities of mechanical strength, lightness, sound and heat insulation are desired.
  • insulating panels made of expanded or extruded polystyrene are used.
  • these panels have low mechanical properties. For example, if one wishes to realize an isolated floor, one can use such plates distributed on the ground and on which a screed is made. The load acceptable by such an embodiment is limited because of the compressibility of the panels.
  • So-called "sandwich” panels which comprise external faces, parallel to each other, connected by a core of expanded synthetic material, such as polystyrene or polyurethane.
  • the facings are for example plaster, sheet metal, wood or composite synthetic material.
  • Such panels make partitions, walls or roofs.
  • These panels also have limited mechanical strength.
  • EP 8 960 there is provided a panel comprising two facings connected by a core having a honeycomb honeycomb structure and cells filled with synthetic foam.
  • Such a panel combines the mechanical properties of a honeycomb structural panel with the thermal insulation properties of the foam.
  • the foam is reinforced with fibers from a layer covering the inner face of the facing. The use of fibers is expensive and decreases the facilities for recycling materials at the end of the life of the panel or the product.
  • the invention aims to provide a composite part such as a panel having good properties of mechanical strength and thermal and sound insulation. It is also an object of the invention to provide a composite part easy to recycle at the end of life.
  • the subject of the invention is a composite part such as a composite panel comprising at least one honeycomb honeycomb structure, a synthetic foam material at least partially filling the cells.
  • the honeycomb structure is made of synthetic material whose surface tension before treatment does not allow the adhesion of the foam, at least a portion of the internal surface of the cells being treated so that the foam adheres directly or indirectly thereto.
  • Some synthetic materials normally have a surface on which it is difficult, if not impossible, to adhere foam or glue.
  • the surface of the honeycomb structure is modified so that the foam adheres to it.
  • the structure and the foam form a complex combining the mechanical properties and insulation.
  • the foam is for example polyurethane foam or polystyrene. It may also be expanded polystyrene or expanded polypropylene. In this case, the expansion is carried out when the balls are in the cells, and a glue suitable for adhering the foam against the treated walls is used.
  • polyethylene polypropylene
  • polyester polypropylene
  • polyamide polyamide
  • the material can be chosen for its recycling facilities.
  • the surface tension of the cellular structure before treatment is less than 38 mN / r.
  • Foams or adhesives generally do not adhere to materials having such surface tension, such as polypropylene.
  • the value of the surface tension of the honeycomb structure increases, reaching for example a value greater than 38 mN / m (milli-Newton per meter, or dynes per square centimeter).
  • the foam completely fills the cells.
  • the inner surface of the honeycomb structure is preferably treated completely, so that the foam adheres to the largest possible area.
  • the rigidity of such a piece is greater than that of a honeycomb structure alone, due to the filling of the cells with the foam and the attachment of said foam to the inner surface of the cells.
  • Such a panel can be used as a building block for building other products.
  • a door is made by placing the panel in a box or between two facings attached by gluing. It is also used to make a floor by interposing it between a floor and a screed.
  • the mechanical resistance to compression is greatly increased by the presence of the honeycomb structure, while maintaining good sound and heat insulation properties.
  • the panel or the part comprises at least one facing extending along the honeycomb structure so as to close the cells and adhering to the foam.
  • the facing is attached to the honeycomb structure by means of the foam which adheres to the walls of the honeycomb structure and on the inner surface of the cladding.
  • the facing may be of conventionally used material, such as wood, plaster, sheets of synthetic composite material or metal sheets. If the facing has an inner face that does not allow sufficient adhesion of the foam, the inner face can also be treated beforehand.
  • the piece may have only one facing or siding on each face.
  • the two facings are not necessarily of the same nature.
  • One of the facings may be a sheet having an adhesive outer face covered by a silicone paper.
  • the panel can be attached to a support surface after removing the silicone film and applying the adhesive side to the support surface. This reinforces the support and improves the insulation qualities.
  • This panel may be used directly as a partition, wall or floor element, roof, in a building or an air vehicle, land or sea. You can also make a pontoon or a buoy, because of its insubmersibility. You can also give it a shape like the inside of a car bumper. Compared to a foamless panel, the compression damping properties are improved by the that the air is better trapped in the bubbles of the foam that adheres to the cells of the honeycomb.
  • the panel or the composite part has two facings parallel to each other, extending along the honeycomb structure so as to close the cells, the foam being distributed in two layers respectively adhering to the facings.
  • the foam being distributed in two layers respectively adhering to the facings.
  • a light panel is obtained, which has mechanical damping properties of a shock perpendicular to the panel, ie in the axis of the cells.
  • the panel or the piece can crash during a localized shock by the approximation of the foam layers between them and the crushing of the median portion of the honeycomb structure.
  • the part comprises two honeycomb structures separated by a sheet and sandwiched by two parallel sections to the sheet so as to seal the cells, the sheet and the facings adhering to the foam.
  • the sheet can serve as a metal shield, such as steel or aluminum, and a particularly strong panel is thus obtained.
  • a panel can be used as a fire-fighting element.
  • the honeycomb structure is formed by tubular elements juxtaposed and interconnected by the foam. A honeycomb structure is thus reconstituted with the tubular elements, and by assembling them together with the foam that acts as glue between them.
  • the part comprises a fastener inserted in at least one cell and held by the foam.
  • the insert can be a nut or a screw and is anchored to the honeycomb structure by means of the foam which acts as glue.
  • the invention also relates to a method of manufacturing a part as described above, wherein the method of depositing synthetic material expanding in the cells of the honeycomb structure. At least a portion of the internal surface of the cells is pretreated in order to increase the surface tension of the surface and thus the adhesion of the foam.
  • the treatment of the cellular structure is carried out by one of the methods among a corona treatment, a plasma treatment or a chemical treatment.
  • Corona treatment is also referred to as a corona effect and involves subjecting the synthetic material to an electric field to ionize the atmosphere on the surface of the material.
  • the chemical structure on the surface is modified, in a manner known per se, in particular by the creation of peroxide functions (00H), so that the surface tension of the surface is increased.
  • the foam is formed by balls of material to be foamed, the honeycomb structure being coated with glue, and then the balls are expanded by adhering to the structure via the glue and between them.
  • Methods of making plates by bead expansion such as polystyrene, polypropylene or polyethylene are known. Having pre-glued the honeycomb structure, the expansion is carried out in the cells, which allows the balls to fill the cells and agglomerate together. In addition, thanks to the glue, this formed foam also adheres to the walls of the cells.
  • the process can also be perfected by also coating or only the balls with glue, to increase their adhesion between them.
  • the expansion is for example 20 to 50% of volume.
  • a vinyl glue such as Bostik Vinycol 1520 glue.
  • a composite part with the tubular elements the entire inner and outer surface of the tubular elements is treated.
  • FIG. 1 is a sectional view of a panel according to a first embodiment embodiment of the invention
  • Figure 2 is a view similar to Figure 1 of a panel according to a second embodiment of the invention
  • Figure 3 is a sectional view during a manufacturing phase of a panel according to a third embodiment
  • FIG. 4 is a view similar to FIG. 1 of the panel according to the third embodiment of FIG. the invention
  • Figure 5 is a view similar to Figure 1 of a panel according to a fourth embodiment of the invention
  • FIG. 6 is a perspective view of a tubular element for producing a panel according to a fifth embodiment of the invention
  • Figure 7 is a sectional view parallel to the facings of a panel according to the fifth embodiment of the invention.
  • Composite panels or technical parts according to the invention are made with honeycomb honeycomb structure and synthetic foam.
  • honeycomb structure may be made conventionally, for example by extrusion of thermoplastic material, or by assembly of continuous strips joined alternately with one or the other of two adjacent strips, as described in the WO document.
  • the structure can also be achieved by the assembly by gluing or welding of tubular elements of hexagonal or circular section.
  • the material is for example polypropylene.
  • the inner surface of the honeycomb structure is corona treated, for example by passing the end of the cells near an electrode.
  • the document FR 2 443 753 describes an example of a machine and method capable of treating the honeycomb structure.
  • the electrical voltage used may be up to 50 kilovolts or more and the frequency may be less than
  • the foam is for example polyurethane, conventionally obtained by foaming a mixture of a polyol and a diisocyanate with a swelling agent type HFC.
  • the foamable mixture is spread on a first molding plate, not shown, then the honeycomb structure 10 is deposited on the molding plate, and the honeycomb structure is sandwiched with a second molding plate, not shown, parallel at the first plate.
  • the entire foaming of the mixture is expected throughout the volume of the cells and the hardening of the foam 11.
  • the plates are removed to extract the panel 1 formed by the cellular structure 10 and the foam 11.
  • the plates are for example covered by a Silicone or PTFE-based coating to prevent adhesion of the foam to the plates.
  • the honeycomb structure 10 is deposited on the first plate and then the mixture is deposited on the plate or introduced directly into each cell.
  • the molding plates are replaced by facings 22, 23.
  • the foam 21 then adheres to the facings 22, 23 as well as to the walls 25 of the honeycomb structure, which gives a cohesion to the panel 2. It is also possible to manufacture a panel with a single facing.
  • the mixture is first spread on a first face 32 and then the honeycomb structure 30 is placed on the first face 32.
  • the mixture is transformed into a foam 31 which develops in the lower part 301 of the cells.
  • the foam adheres to the walls 35 of the cells in said lower portion 301.
  • the second layer 33 is prepared with a layer of mixture and the assembly 36 formed by the first layer 32 and the honeycomb structure 30 is applied to the second layer 33.
  • a second layer 37 of foam is formed symmetrically to the first layer 31, leaving a vacuum 38 between the two layers 31, 37 of foam. For to limit the expansion of the foam, it is possible to treat only the lower part and the symmetrical part of the cells.
  • a panel is obtained by completing the panel 2 according to the second embodiment with a layer of mixture deposited on one of the facings 23 which is a sheet or other metal part such as aluminum, then a second honeycomb structure 40 and finally another facing 42.
  • the honeycomb structure 40 is filled with foam 41.
  • a panel could be made with only the sheet and the two cellular structures, without the facings 22, 42.
  • the procedure is as in the second embodiment, but the honeycomb structure consists of the juxtaposition of tubular elements 5, not interconnected before laying on the facing, as shown in Figure 6
  • the section of the tubular elements is substantially hexagonal, with curved faces towards the outside.
  • the tubular elements 5 are made of polypropylene or other synthetic material and are treated over their entire surface, both inside 50 and outside 51.
  • the tubular elements are arranged in contact with each other by their curved faces so that there remains a space between them, as shown in Figure 7
  • the polyurethane 52 then wraps the tubular elements 5 and fills them so that they are finally glued together and at the siding.
  • This honeycomb structure can also be used with the other embodiments.

Landscapes

  • Laminated Bodies (AREA)

Abstract

The invention concerns a composite part such as a panel, comprising a honeycomb cellular structure (20), a synthetic foam material (21) filling at least partly the cells. The honeycomb structure (20) is made of synthetic material whereof the surface tension prior to the surface being treated does not allow the foam to adhere, and at last part of the inner surface of the cells is treated such that the foam adheres thereto directly or indirectly. The invention also concerns a method for making such a part.

Description

Pièce composite telle qu'un panneau, comportant une structure alvéolaire à nids d'abeille. Composite part such as a panel, having a honeycomb honeycomb structure.
L'invention concerne un panneau ou une pièce composite comportant une structure alvéolaire à nids d' abeille .The invention relates to a panel or composite part comprising honeycomb honeycomb structure.
Dans la construction de bâtiments, de véhicules terrestres, aériens ou de bateaux, on utilise fréquemment des panneaux pour lesquels on souhaite de bonnes qualités de résistance mécanique, de légèreté, d'isolation phonique et thermique. On utilise par exemple des panneaux d'isolant en polystyrène expansé ou extrudé. Cependant, ces panneaux ont de faibles propriétés mécaniques. Par exemple, si on souhaite réaliser un plancher isolé, on peut utiliser de telles plaques réparties au sol et sur lesquelles on réalise une chape. La charge admissible par une telle réalisation est limitée à cause de la compressibilité des panneaux.In the construction of buildings, land vehicles, air vehicles or boats, panels are frequently used for which good qualities of mechanical strength, lightness, sound and heat insulation are desired. For example, insulating panels made of expanded or extruded polystyrene are used. However, these panels have low mechanical properties. For example, if one wishes to realize an isolated floor, one can use such plates distributed on the ground and on which a screed is made. The load acceptable by such an embodiment is limited because of the compressibility of the panels.
On connaît des panneaux dits "sandwich" qui comportent des parements extérieurs, parallèles entre eux, reliés par une âme en matière synthétique expansée, telle que du polystyrène ou du polyuréthane . Les parements sont par exemple en plâtre, en tôle métallique, en bois ou en matériau synthétique composite. De tels panneaux permettent de réaliser des cloisons, des parois ou des toitures . Ces panneaux ont également une résistance mécanique limitée. Dans le document EP 8 960, il est proposé un panneau comportant deux parements reliés par une âme ayant une structure alvéolaire en nids d'abeille et des alvéoles remplies de mousse synthétique. Un tel panneau combine les propriétés mécaniques d'un panneau à structure en nids d'abeille avec les propriétés d'isolation thermique de la mousse. Cependant, pour maintenir l'assemblage entre les parements, la mousse est renforcée de fibres provenant d'une couche recouvrant la face intérieure du parement. L'utilisation de fibres est onéreuse et diminue les facilités de recyclage des matériaux en fin de vie du panneau ou du produit.So-called "sandwich" panels are known which comprise external faces, parallel to each other, connected by a core of expanded synthetic material, such as polystyrene or polyurethane. The facings are for example plaster, sheet metal, wood or composite synthetic material. Such panels make partitions, walls or roofs. These panels also have limited mechanical strength. In EP 8 960, there is provided a panel comprising two facings connected by a core having a honeycomb honeycomb structure and cells filled with synthetic foam. Such a panel combines the mechanical properties of a honeycomb structural panel with the thermal insulation properties of the foam. However, to maintain assembly between the facings, the foam is reinforced with fibers from a layer covering the inner face of the facing. The use of fibers is expensive and decreases the facilities for recycling materials at the end of the life of the panel or the product.
L'invention vise à fournir une pièce composite telle qu'un panneau ayant de bonnes propriétés de résistance mécanique et d'isolation thermique et phonique. C'est aussi un objectif de l'invention de fournir une pièce composite facile à recycler en fin de vie . Avec ces objectifs en vue, l'invention a pour objet une pièce composite telle qu'un panneau composite comportant au moins une structure alvéolaire en nids d'abeille, un matériau en mousse synthétique remplissant au moins partiellement les alvéoles . La structure alvéolaire est en matière synthétique dont la tension superficielle avant traitement ne permet pas l'adhérence de la mousse, au moins une partie de la surface interne des alvéoles étant traitée pour que la mousse y adhère directement ou indirectement. Certaines matières synthétiques présentent normalement une surface sur laquelle il est difficile, voire impossible, de faire adhérer de la mousse ou de la colle. Cependant, par un traitement de surface adapté, on modifie la surface de la structure en nids d'abeille pour que la mousse y adhère. Ainsi, après durcissement de la mousse, la structure et la mousse forment un complexe alliant les propriétés mécaniques et d'isolation. La mousse est par exemple de la mousse de polyuréthane ou de polystyrène. Ce peut-être aussi du polystyrène expansé ou du polypropylène expansé. Dans ce cas, l'expansion est réalisée quand les billes sont dans les alvéoles, et on utilise une colle adaptée pour faire adhérer la mousse contre les parois traitées.The invention aims to provide a composite part such as a panel having good properties of mechanical strength and thermal and sound insulation. It is also an object of the invention to provide a composite part easy to recycle at the end of life. With these objectives in view, the subject of the invention is a composite part such as a composite panel comprising at least one honeycomb honeycomb structure, a synthetic foam material at least partially filling the cells. The honeycomb structure is made of synthetic material whose surface tension before treatment does not allow the adhesion of the foam, at least a portion of the internal surface of the cells being treated so that the foam adheres directly or indirectly thereto. Some synthetic materials normally have a surface on which it is difficult, if not impossible, to adhere foam or glue. However, by a suitable surface treatment, the surface of the honeycomb structure is modified so that the foam adheres to it. Thus, after curing the foam, the structure and the foam form a complex combining the mechanical properties and insulation. The foam is for example polyurethane foam or polystyrene. It may also be expanded polystyrene or expanded polypropylene. In this case, the expansion is carried out when the balls are in the cells, and a glue suitable for adhering the foam against the treated walls is used.
Parmi les matières utilisables pour réaliser la structure alvéolaire, on peut citer à titre d'exemple le polyéthylène, le polypropylène, le polyester ou le polyamide. On peut choisir la matière pour ses facilités de recyclage.Among the materials that can be used to produce the cellular structure, mention may be made, for example, of polyethylene, polypropylene, polyester or polyester. polyamide. The material can be chosen for its recycling facilities.
A titre d'exemple, la tension superficielle de la structure alvéolaire avant traitement est inférieure à 38 mN/ra. Les mousses ou les colles n'adhère en général pas sur les matières ayant une telle tension superficielle, tel que du polypropylène .By way of example, the surface tension of the cellular structure before treatment is less than 38 mN / r. Foams or adhesives generally do not adhere to materials having such surface tension, such as polypropylene.
Après le traitement de surface, la valeur de la tension superficielle de la structure alvéolaire augmente, pour atteindre par exemple une valeur supérieure à 38 mN/m (milli-Newton par mètre, ou dynes par centimètre carré) .After the surface treatment, the value of the surface tension of the honeycomb structure increases, reaching for example a value greater than 38 mN / m (milli-Newton per meter, or dynes per square centimeter).
Dans un mode de réalisation particulier, la mousse emplit entièrement les alvéoles. Dans ce cas, la surface interne de la structure alvéolaire est traitée de préférence en totalité, pour que la mousse adhère sur la plus grande surface possible. La rigidité d'une telle pièce est plus importante que celle d'une structure à nids d'abeille seule, due au remplissage des alvéoles par la mousse et à l'accrochage de ladite mousse à la surface intérieure des alvéoles .In a particular embodiment, the foam completely fills the cells. In this case, the inner surface of the honeycomb structure is preferably treated completely, so that the foam adheres to the largest possible area. The rigidity of such a piece is greater than that of a honeycomb structure alone, due to the filling of the cells with the foam and the attachment of said foam to the inner surface of the cells.
Un tel panneau peut être utilisé comme élément de base pour construire d'autres produits. On réalise par exemple une porte en plaçant le panneau dans un caisson ou entre deux parements rapportés par collage. On l'utilise aussi pour réaliser un plancher en l'intercalant entre un sol et une chape. Par rapport à un panneau de mousse selon l'art antérieur, la résistance mécanique à la compression est fortement augmentée par la présence de la structure alvéolaire, tout en conservant de bonnes propriétés d'isolation phonique et thermique.Such a panel can be used as a building block for building other products. For example, a door is made by placing the panel in a box or between two facings attached by gluing. It is also used to make a floor by interposing it between a floor and a screed. Compared to a foam board according to the prior art, the mechanical resistance to compression is greatly increased by the presence of the honeycomb structure, while maintaining good sound and heat insulation properties.
On constate que, même en l'absence de parement, ce panneau ne se disperse pas, car la mousse présente dans les alvéoles est retenue par l'adhérence aux parois des alvéoles. De plus, lorsque le panneau est par exemple découpé, la mousse reste dans les alvéoles, même si celles-ci sont ouvertes. Le chant présente alors une surface continue sur laquelle on peut coller un parement de chant ou par laquelle on peut assembler les panneaux entre eux. Selon un deuxième mode de réalisation, le panneau, ou la pièce comporte au moins un parement s ' étendant le long de la structure alvéolaire de manière à obturer les alvéoles et adhérant à la mousse. Le parement est fixé à la structure alvéolaire par l'intermédiaire de la mousse qui adhère aux parois de la structure alvéolaire et sur la surface intérieure du parement. En fonction de la destination du panneau ou de la pièce, le parement peut être en matériau utilisé classiquement, comme du bois, du plâtre, des feuilles de matière composite synthétique ou des tôles métalliques . Si le parement comporte une face intérieure ne permettant pas une adhérence suffisante de la mousse, la face intérieure peut être également traitée préalablement .It is found that, even in the absence of siding, this panel does not disperse, because the foam present in the cells is retained by the adhesion to the walls of the cells. In addition, when the panel is cut for example, the foam remains in the cells, even if these are open. The song then has a continuous surface on which we can stick a siding or by which we can assemble the panels between them. According to a second embodiment, the panel or the part comprises at least one facing extending along the honeycomb structure so as to close the cells and adhering to the foam. The facing is attached to the honeycomb structure by means of the foam which adheres to the walls of the honeycomb structure and on the inner surface of the cladding. Depending on the destination of the panel or the room, the facing may be of conventionally used material, such as wood, plaster, sheets of synthetic composite material or metal sheets. If the facing has an inner face that does not allow sufficient adhesion of the foam, the inner face can also be treated beforehand.
La pièce peut comporter un seul parement ou un parement sur chaque face. Les deux parements ne sont pas nécessairement de même nature. L'un des parements peut être une feuille comportant une face extérieure adhésive recouverte par un papier siliconé. Ainsi, on peut fixer le panneau sur une surface de support après avoir retiré le film siliconé et appliqué la face adhésive sur la surface de support. On renforce ainsi le support et on améliore les qualités d'isolation.The piece may have only one facing or siding on each face. The two facings are not necessarily of the same nature. One of the facings may be a sheet having an adhesive outer face covered by a silicone paper. Thus, the panel can be attached to a support surface after removing the silicone film and applying the adhesive side to the support surface. This reinforces the support and improves the insulation qualities.
On peut utiliser ce panneau directement comme cloison, paroi ou élément de plancher, de toiture, dans un bâtiment ou un véhicule aérien, terrestre ou marin. On peut aussi réaliser un ponton ou une bouée, du fait de son insubmersibilité . On peut également lui donner une forme comme l'intérieur d'un pare-chocs de voiture. Par rapport à un panneau sans mousse, les propriétés d'amortissement à la compression sont améliorées par le fait que l'air est mieux emprisonné dans les bulles de la mousse qui adhère aux alvéoles du nids d'abeille.This panel may be used directly as a partition, wall or floor element, roof, in a building or an air vehicle, land or sea. You can also make a pontoon or a buoy, because of its insubmersibility. You can also give it a shape like the inside of a car bumper. Compared to a foamless panel, the compression damping properties are improved by the that the air is better trapped in the bubbles of the foam that adheres to the cells of the honeycomb.
De manière particulière, le panneau ou la pièce composite comporte deux parements parallèles entre eux, s ' étendant le long de la structure alvéolaire de manière à obturer les alvéoles, la mousse étant répartie en deux couches adhérant respectivement aux parements. Ainsi, il subsiste un espace vide entre les deux couches de mousse. On obtient un panneau léger, et qui a des propriétés mécaniques d'amortissement d'un choc perpendiculaire au panneau, c'est à dire dans l'axe des alvéoles. En effet, le panneau ou la pièce peut s'écraser lors d'un choc localisé par le rapprochement des couches de mousse entre elles et l'écrasement de la partie médiane de la structure alvéolaire.In a particular way, the panel or the composite part has two facings parallel to each other, extending along the honeycomb structure so as to close the cells, the foam being distributed in two layers respectively adhering to the facings. Thus, there remains an empty space between the two layers of foam. A light panel is obtained, which has mechanical damping properties of a shock perpendicular to the panel, ie in the axis of the cells. Indeed, the panel or the piece can crash during a localized shock by the approximation of the foam layers between them and the crushing of the median portion of the honeycomb structure.
Selon un troisième mode de réalisation, la pièce comporte deux structures alvéolaires séparées par une tôle et enserrées par deux parements parallèles à la tôle de manière à obturer les alvéoles, la tôle et les parements adhérant à la mousse. La tôle peut servir de blindage en métal, tel que de l'acier ou de l'aluminium et on obtient ainsi un panneau particulièrement résistant. Un tel panneau peut être utilisé comme élément séparatif anti-incendie. Selon une disposition particulière, la structure alvéolaire est formée par des éléments tubulaires juxtaposés et liés entre eux par la mousse. On reconstitue ainsi une structure en nids d'abeille avec les éléments tubulaires, et en réalisant l'assemblage de ceux-ci par la mousse qui fait office de colle entre eux.According to a third embodiment, the part comprises two honeycomb structures separated by a sheet and sandwiched by two parallel sections to the sheet so as to seal the cells, the sheet and the facings adhering to the foam. The sheet can serve as a metal shield, such as steel or aluminum, and a particularly strong panel is thus obtained. Such a panel can be used as a fire-fighting element. According to a particular arrangement, the honeycomb structure is formed by tubular elements juxtaposed and interconnected by the foam. A honeycomb structure is thus reconstituted with the tubular elements, and by assembling them together with the foam that acts as glue between them.
Selon une autre disposition particulière, la pièce comporte un élément de fixation inséré dans au moins une alvéole et maintenu par la mousse. L 'insert peut être un écrou ou une vis et est ancré à la structure alvéolaire par l'intermédiaire de la mousse qui fait office de colle . L'invention a aussi pour objet un procédé de fabrication d'une pièce telle que décrite précédemment, procédé selon lequel on dépose de la matière synthétique en expansion dans les alvéoles de la structure alvéolaire. On traite au préalable au moins une partie de la surface interne des alvéoles pour augmenter la tension superficielle de la surface et ainsi l'adhérence de la mousse .According to another particular arrangement, the part comprises a fastener inserted in at least one cell and held by the foam. The insert can be a nut or a screw and is anchored to the honeycomb structure by means of the foam which acts as glue. The invention also relates to a method of manufacturing a part as described above, wherein the method of depositing synthetic material expanding in the cells of the honeycomb structure. At least a portion of the internal surface of the cells is pretreated in order to increase the surface tension of the surface and thus the adhesion of the foam.
Le traitement de la structure alvéolaire est réalisé par l'un des procédés parmi un traitement par effet de couronne, un traitement au plasma ou un traitement par voie chimique.The treatment of the cellular structure is carried out by one of the methods among a corona treatment, a plasma treatment or a chemical treatment.
Le traitement par effet de couronne est appelé aussi effet corona et il consiste à soumettre le matériau synthétique à un champ électrique pour ioniser l'atmosphère à la surface du matériau. La structure chimique à la surface est modifiée, d'une manière connue en soi, en particulier par la création de fonctions peroxydes (00H) , de telle sorte que la tension superficielle de la surface est augmentée.Corona treatment is also referred to as a corona effect and involves subjecting the synthetic material to an electric field to ionize the atmosphere on the surface of the material. The chemical structure on the surface is modified, in a manner known per se, in particular by the creation of peroxide functions (00H), so that the surface tension of the surface is increased.
Un effet similaire peut être obtenu en créant un plasma à proximité de la surface du matériau. La modification chimique de la surface peut aussi être obtenue par un bain dans une solution de chromites . Selon un procédé particulier, la mousse est formée par des billes de matière à expanser, la structure alvéolaire étant enduite de colle, puis les billes sont expansées en adhérant à la structure par l'intermédiaire de la colle et entre elles . On connaît des procédés de fabrication de plaques par expansion de billes telles que du polystyrène, du polypropylène ou du polyéthylène . En ayant préencollé la structure alvéolaire, l'expansion est réalisée dans les alvéoles, ce qui permet aux billes de remplir les alvéoles et de s'agglomérer entre elles. De plus, grâce à la colle, cette mousse formée adhère également aux parois des alvéoles. Le procédé peut aussi être perfectionné en enduisant également ou uniquement les billes avec la colle, pour augmenter leur adhérence entre elles. L'expansion est par exemple de 20 à 50 % de volume. Pour une mousse et une structure alvéolaire en polypropylène, on peut par exemple utiliser une colle vinylique telle que de la colle Bostik Vinycol 1520A similar effect can be achieved by creating a plasma near the surface of the material. The chemical modification of the surface can also be obtained by bathing in a chromite solution. According to a particular method, the foam is formed by balls of material to be foamed, the honeycomb structure being coated with glue, and then the balls are expanded by adhering to the structure via the glue and between them. Methods of making plates by bead expansion such as polystyrene, polypropylene or polyethylene are known. Having pre-glued the honeycomb structure, the expansion is carried out in the cells, which allows the balls to fill the cells and agglomerate together. In addition, thanks to the glue, this formed foam also adheres to the walls of the cells. The process can also be perfected by also coating or only the balls with glue, to increase their adhesion between them. The expansion is for example 20 to 50% of volume. For a foam and a polypropylene honeycomb structure, it is possible for example to use a vinyl glue such as Bostik Vinycol 1520 glue.
(marque déposée) avec 5% de durcisseur Desmodur RC(registered trademark) with 5% hardener Desmodur RC
(marque déposée) .(trademark) .
Pour fabriquer un panneau aux deux parements et deux couches de mousse, on peut par exemple utiliser un procédé selon lequel on dépose sur un premier des parements une première couche de matière synthétique en expansion, on dépose sur le premier parement la structure alvéolaire à travers la première couche, pour former un premier ensemble, on dépose sur le deuxième parement une deuxième couche de matière synthétique en expansion, et on dépose le premier ensemble sur le deuxième parement, la structure alvéolaire passant à travers la deuxième couche . De préférence, pour fabriquer une pièce composite avec les éléments tubulaires, on traite toute la surface interne et externe des éléments tubulaires .In order to manufacture a panel with two facings and two layers of foam, it is possible, for example, to use a method according to which a first layer of expanding synthetic material is deposited on a first facing, the honeycomb structure is deposited on the first face through the first layer, to form a first set, is deposited on the second facing a second layer of synthetic material expanding, and depositing the first set on the second facing, the honeycomb structure passing through the second layer. Preferably, to manufacture a composite part with the tubular elements, the entire inner and outer surface of the tubular elements is treated.
L'invention sera mieux comprise et d'autres particularités et avantages apparaîtront à la lecture de la description qui va suivre, la description faisant référence aux dessins annexés parmi lesquels : la figure 1 est une vue en coupe d'un panneau selon un premier mode de réalisation de l'invention ; la figure 2 est une vue similaire à la figure 1 d'un panneau selon un deuxième mode de réalisation de l ' invention ; la figure 3 est une vue en coupe pendant une phase de fabrication d'un panneau selon un troisième mode de réalisation ; - la figure 4 est une vue similaire à la figure 1 du panneau selon le troisième mode de réalisation de l ' invention ; la figure 5 est une vue similaire à la figure 1 d'un panneau selon un quatrième mode de réalisation de l ' invention ; - la figure 6 est une vue en perspective d'un élément tubulaire pour la réalisation d'un panneau selon un cinquième mode de réalisation de l'invention ; la figure 7 est une vue en coupe parallèle aux parements d'un panneau selon le cinquième mode de réalisation de l'invention.The invention will be better understood and other features and advantages will appear on reading the description which follows, the description referring to the appended drawings in which: FIG. 1 is a sectional view of a panel according to a first embodiment embodiment of the invention; Figure 2 is a view similar to Figure 1 of a panel according to a second embodiment of the invention; Figure 3 is a sectional view during a manufacturing phase of a panel according to a third embodiment; FIG. 4 is a view similar to FIG. 1 of the panel according to the third embodiment of FIG. the invention; Figure 5 is a view similar to Figure 1 of a panel according to a fourth embodiment of the invention; FIG. 6 is a perspective view of a tubular element for producing a panel according to a fifth embodiment of the invention; Figure 7 is a sectional view parallel to the facings of a panel according to the fifth embodiment of the invention.
Des panneaux ou pièces techniques composites selon l'invention sont réalisés avec une structure alvéolaire à nids d'abeille et de la mousse synthétique.Composite panels or technical parts according to the invention are made with honeycomb honeycomb structure and synthetic foam.
La structure alvéolaire peut être réalisée de manière classique, par exemple par extrusion de matière thermoplastique, ou par assemblage de bandes continues jointes en alternance avec l'une ou l'autre de deux bandes adjacentes, tel que décrit dans le document WOThe honeycomb structure may be made conventionally, for example by extrusion of thermoplastic material, or by assembly of continuous strips joined alternately with one or the other of two adjacent strips, as described in the WO document.
98/41388. La structure peut aussi être réalisée par l'assemblage par collage ou soudure d'éléments tubulaires de section hexagonale ou circulaire. La matière est par exemple du polypropylène .98/41388. The structure can also be achieved by the assembly by gluing or welding of tubular elements of hexagonal or circular section. The material is for example polypropylene.
La surface interne de la structure alvéolaire est traitée par effet de couronne, par exemple en faisant passer l'extrémité des alvéoles à proximité d'une électrode. Le document FR 2 443 753 décrit un exemple de machine et de procédé aptes à traiter la structure alvéolaire. Pour permettre le traitement des conduits internes du nids d'abeille sur des hauteurs de 50 mm et plus, la tension électrique utilisée peut atteindre 50 kilovolts ou plus et la fréquence peut être inférieure àThe inner surface of the honeycomb structure is corona treated, for example by passing the end of the cells near an electrode. The document FR 2 443 753 describes an example of a machine and method capable of treating the honeycomb structure. To allow the treatment of honeycomb internal ducts at heights of 50 mm and above, the electrical voltage used may be up to 50 kilovolts or more and the frequency may be less than
15 kilohertz . La mousse est par exemple du polyuréthane, obtenue de manière classique par le moussage d'un mélange d'un polyol et d'un diisocyanate avec un agent gonflant type HFC.15 kilohertz. The foam is for example polyurethane, conventionally obtained by foaming a mixture of a polyol and a diisocyanate with a swelling agent type HFC.
Selon un premier mode de réalisation, montré sur la figure 1, on étend le mélange prêt à mousser sur une première plaque de moulage, non représentée, puis on dépose la structure alvéolaire 10 sur la plaque de moulage, et on enserre la structure alvéolaire avec une deuxième plaque de moulage, non représentée, parallèle à la première plaque. On attend le moussage complet du mélange dans tout le volume des alvéoles et le durcissement de la mousse 11. Puis on écarte les plaques pour extraire le panneau 1 formé par la structure alvéolaire 10 et la mousse 11. Les plaques sont par exemple recouvertes par un revêtement à base de silicone ou de PTFE pour éviter l'adhérence de la mousse sur les plaques. Dans une variante, la structure alvéolaire 10 est déposée sur la première plaque puis le mélange est déposé sur la plaque ou introduit directement dans chaque alvéole .According to a first embodiment, shown on the FIG. 1, the foamable mixture is spread on a first molding plate, not shown, then the honeycomb structure 10 is deposited on the molding plate, and the honeycomb structure is sandwiched with a second molding plate, not shown, parallel at the first plate. The entire foaming of the mixture is expected throughout the volume of the cells and the hardening of the foam 11. Then the plates are removed to extract the panel 1 formed by the cellular structure 10 and the foam 11. The plates are for example covered by a Silicone or PTFE-based coating to prevent adhesion of the foam to the plates. In a variant, the honeycomb structure 10 is deposited on the first plate and then the mixture is deposited on the plate or introduced directly into each cell.
Selon un deuxième mode de réalisation, montré sur la figure 2, on remplace les plaques de moulage par des parements 22, 23. La mousse 21 adhère alors aux parements 22, 23 ainsi qu'aux parois 25 de la structure alvéolaire, ce qui donne une cohésion au panneau 2. On peut aussi fabriquer un panneau avec un seul parement.According to a second embodiment, shown in FIG. 2, the molding plates are replaced by facings 22, 23. The foam 21 then adheres to the facings 22, 23 as well as to the walls 25 of the honeycomb structure, which gives a cohesion to the panel 2. It is also possible to manufacture a panel with a single facing.
Selon un troisième mode de réalisation, montré sur la figure 2, le mélange est d'abord étalé sur un premier parement 32 puis la structure alvéolaire 30 est disposée sur le premier parement 32. Le mélange se transforme en mousse 31 qui se développe dans la partie inférieure 301 des alvéoles. La mousse adhère aux parois 35 des alvéoles dans ladite partie inférieure 301 . Après durcissement de cette première couche 31 de mousse, on prépare le deuxième parement 33 avec une couche de mélange et on applique l'ensemble 36 formé par le premier parement 32 et la structure alvéolaire 30 sur le deuxième parement 33. Une deuxième couche 37 de mousse se forme de manière symétrique à la première couche 31, en laissant subsister un vide 38 entre les deux couches 31, 37 de mousse. Pour limiter l'expansion de la mousse, il est possible de ne traiter que la partie inférieure et la partie symétrique des alvéoles .According to a third embodiment, shown in FIG. 2, the mixture is first spread on a first face 32 and then the honeycomb structure 30 is placed on the first face 32. The mixture is transformed into a foam 31 which develops in the lower part 301 of the cells. The foam adheres to the walls 35 of the cells in said lower portion 301. After curing of this first layer 31 of foam, the second layer 33 is prepared with a layer of mixture and the assembly 36 formed by the first layer 32 and the honeycomb structure 30 is applied to the second layer 33. A second layer 37 of foam is formed symmetrically to the first layer 31, leaving a vacuum 38 between the two layers 31, 37 of foam. For to limit the expansion of the foam, it is possible to treat only the lower part and the symmetrical part of the cells.
Selon un quatrième mode de réalisation, illustré par la figure 5, on obtient un panneau en complétant le panneau 2 selon le deuxième mode de réalisation par une couche de mélange déposée sur l'un des parements 23 qui est une tôle ou autre partie métallique comme l'aluminium, puis une deuxième structure alvéolaire 40 et enfin un autre parement 42. La structure alvéolaire 40 se remplit de mousse 41. On pourrait réaliser un panneau avec uniquement la tôle et les deux structures alvéolaires, sans les parements 22, 42.According to a fourth embodiment, illustrated in FIG. 5, a panel is obtained by completing the panel 2 according to the second embodiment with a layer of mixture deposited on one of the facings 23 which is a sheet or other metal part such as aluminum, then a second honeycomb structure 40 and finally another facing 42. The honeycomb structure 40 is filled with foam 41. A panel could be made with only the sheet and the two cellular structures, without the facings 22, 42.
Dans un cinquième mode de réalisation, on procède comme dans le deuxième mode de réalisation, mais la structure alvéolaire est constituée par la juxtaposition d'éléments tubulaires 5, non reliés entre eux avant la pose sur le parement, tels que représentés sur la figure 6. La section des éléments tubulaires est sensiblement hexagonale, avec des faces bombées vers l'extérieur Les éléments tubulaires 5 sont en polypropylène ou autre matière synthétique et sont traités sur toute leur surface, tant intérieure 50 qu'extérieure 51. Les éléments tubulaires sont disposés en contact les uns avec les autres par leurs faces bombées de telle sorte qu'il subsiste un espace entre eux, comme montré à la figure 7 Le polyuréthane 52 enveloppe alors les éléments tubulaires 5 et les remplit de manière à ce qu'ils soient finalement collés entre eux et aux parements . On peut aussi utiliser cette structure alvéolaire avec les autres modes de réalisation. In a fifth embodiment, the procedure is as in the second embodiment, but the honeycomb structure consists of the juxtaposition of tubular elements 5, not interconnected before laying on the facing, as shown in Figure 6 The section of the tubular elements is substantially hexagonal, with curved faces towards the outside. The tubular elements 5 are made of polypropylene or other synthetic material and are treated over their entire surface, both inside 50 and outside 51. The tubular elements are arranged in contact with each other by their curved faces so that there remains a space between them, as shown in Figure 7 The polyurethane 52 then wraps the tubular elements 5 and fills them so that they are finally glued together and at the siding. This honeycomb structure can also be used with the other embodiments.

Claims

REVENDICATIONS
1. Pièce composite comportant au moins une structure alvéolaire (10) en nid d'abeille, un matériau en mousse (11) synthétique remplissant au moins partiellement les alvéoles, caractérisée en ce que la structure alvéolaire (10) est en matière synthétique dont la tension superficielle avant traitement ne permet pas l'adhérence de la mousse, au moins une partie de la surface interne des alvéoles étant traitée pour que la mousse y adhère directement ou indirectement. Composite part comprising at least one cellular honeycomb structure (10), a synthetic foam material (11) at least partially filling the cells, characterized in that the honeycomb structure (10) is made of synthetic material whose surface tension before treatment does not allow the adhesion of the foam, at least a portion of the inner surface of the cells being treated so that the foam adheres directly or indirectly.
2. Pièce selon la revendication 1, dans laquelle la tension superficielle de la structure alvéolaire (10) avant traitement est inférieure à 38 mN/ra.2. Part according to claim 1, wherein the surface tension of the honeycomb structure (10) before treatment is less than 38 mN / r.
3. Pièce selon la revendication 1, dans laquelle la mousse (11) emplit entièrement les alvéoles. 3. Part according to claim 1, wherein the foam (11) completely fills the cells.
4. Pièce selon la revendication 3, caractérisée en ce qu'elle comporte au moins un parement (22, 23) s ' étendant le long de la structure alvéolaire (20) de manière à obturer les alvéoles et adhérant à la mousse4. Part according to claim 3, characterized in that it comprises at least one facing (22, 23) extending along the honeycomb structure (20) so as to seal the cells and adhering to the foam
(21) . (21).
5. Pièce selon la revendication 1, caractérisé en ce qu'elle comporte deux parements (32, 33) parallèles entre eux, s ' étendant le long de la structure alvéolaire (30) de manière à obturer les alvéoles, la mousse étant répartie en deux couches (31, 37) adhérant respectivement aux parements (32, 33) .5. Part according to claim 1, characterized in that it comprises two facing (32, 33) parallel to each other, extending along the honeycomb structure (30) so as to close the cells, the foam being distributed in two layers (31, 37) respectively adhering to the facings (32, 33).
6. Pièce selon la revendication 1, caractérisé en ce qu'elle comporte deux structures alvéolaires (20, 40) séparées par une tôle (23) et enserrées par deux parements (22, 42) parallèles à la tôle (23) de manière à obturer les alvéoles, la tôle et les parements adhérant à la mousse.6. Part according to claim 1, characterized in that it comprises two honeycomb structures (20, 40) separated by a sheet (23) and sandwiched by two facing (22, 42) parallel to the sheet (23) so as to close the cells, sheet metal and siding adhering to the foam.
7. Pièce selon la revendication 1, dans laquelle la structure alvéolaire est formée par des éléments tubulaires (5) juxtaposés et liés entre eux par la mousse (52), la surface externe (50) des éléments tubulaires (5) étant traitée comme la surface interne (51) .7. Part according to claim 1, wherein the honeycomb structure is formed by tubular elements (5) juxtaposed and bonded together by the foam (52), the outer surface (50) of the tubular elements (5) being treated as the inner surface (51).
8. Pièce selon la revendication 1, caractérisée en ce qu'elle comporte un élément de fixation inséré dans au moins une alvéole et maintenu par la mousse.8. Part according to claim 1, characterized in that it comprises a fastener inserted in at least one cell and held by the foam.
9. Procédé de fabrication d'une pièce selon la revendication 1, dans lequel on dépose de la matière synthétique en expansion dans les alvéoles de la structure alvéolaire (10), caractérisé en ce qu'on traite au préalable au moins une partie de la surface interne des alvéoles pour augmenter la tension superficielle de la surface et ainsi l'adhérence de la matière synthétique9. A method of manufacturing a workpiece according to claim 1, wherein the expanding synthetic material is deposited in the cells of the honeycomb structure (10), characterized in that before processing at least a portion of the internal surface of the cells to increase the surface tension of the surface and thus the adhesion of the synthetic material
(H) •(H) •
10. Procédé de fabrication selon la revendication 9, dans lequel le traitement de la structure alvéolaire (10) est réalisé par l'un des procédés parmi un traitement par effet de couronne, un traitement au plasma ou un traitement par voie chimique.10. The manufacturing method according to claim 9, wherein the treatment of the honeycomb structure (10) is carried out by one of the methods among a corona treatment, a plasma treatment or a chemical treatment.
11. Procédé de fabrication selon la revendication 9, dans lequel la mousse est formée par des billes de matière à expanser, la structure ou les billes étant enduites de colle, puis les billes sont expansées en adhérant à la structure par l'intermédiaire de la colle et entre elles . 11. The manufacturing method according to claim 9, wherein the foam is formed by balls of material to be foamed, the structure or the beads being coated with glue, then the balls are expanded by adhering to the structure via the glue and between them.
12. Procédé de fabrication selon la revendication 9, pour fabriquer une pièce selon la revendication 4, dans lequel : on dépose sur un premier des parements (32) une première couche (31) de matière synthétique en expansion, on dépose sur le premier parement la structure alvéolaire (30) à travers la première couche (31) , pour former un premier ensemble (36) , on dépose sur le deuxième parement (33) une deuxième couche (37) de matière synthétique en expansion, on dépose le premier ensemble (36) sur le deuxième parement (33) , la structure alvéolaire (30) passant à travers la deuxième couche (37) .12. Manufacturing method according to claim 9, for manufacturing a part according to claim 4, wherein: a first layer (31) of expanding synthetic material is deposited on a first face (32), deposited on the first facing. the honeycomb structure (30) through the first layer (31), to form a first assembly (36), is deposited on the second facing (33) a second layer (37) of synthetic material expanding, the first set is deposited (36) on the second facing (33), the honeycomb structure (30) passing through the second layer (37).
13. Procédé de fabrication selon la revendication 9, pour fabriquer une pièce selon la revendication I1 dans lequel on traite toute la surface (50, 51) des éléments tubulaires (5) . 13. The manufacturing method according to claim 9, for manufacturing a part according to claim I 1 wherein the entire surface (50, 51) of the tubular elements (5).
PCT/EP2006/063065 2005-06-15 2006-06-09 Composite part such as a panel, comprising a honeycomb structure WO2006134079A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE202006020359U DE202006020359U1 (en) 2005-06-15 2006-06-09 Component made of composite material, for example a plate, with a honeycomb-like cell structure

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0506029 2005-06-15
FR0506029A FR2887174B1 (en) 2005-06-15 2005-06-15 COMPOSITE PIECE SUCH AS A PANEL, COMPRISING AN ALVEOLAR STRUCTURE WITH A BEES NIDS

Publications (1)

Publication Number Publication Date
WO2006134079A1 true WO2006134079A1 (en) 2006-12-21

Family

ID=35709225

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2006/063065 WO2006134079A1 (en) 2005-06-15 2006-06-09 Composite part such as a panel, comprising a honeycomb structure

Country Status (3)

Country Link
DE (1) DE202006020359U1 (en)
FR (1) FR2887174B1 (en)
WO (1) WO2006134079A1 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2456659A (en) * 2008-01-22 2009-07-29 Matthew Smyth High structural strength sandwich panel
WO2016026217A1 (en) * 2014-08-19 2016-02-25 株洲时代新材料科技股份有限公司 Flame-retardant lightweight structural core and manufacturing method therefor
US9604442B2 (en) 2008-11-24 2017-03-28 Applied Ft Composite Solutions Inc. Peeling process for making resilient pad composite
CN110154974A (en) * 2019-06-28 2019-08-23 东莞职业技术学院 For improving the automotive hood of pedestrian safety
DE102018122098A1 (en) * 2018-09-11 2020-03-12 Rehau Ag + Co Process for making a foamed sheet
US11890843B2 (en) 2010-11-24 2024-02-06 Applied Ft Composite Solutions Inc. Composite cushioning material and jigless method for making the same

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102011117165A1 (en) 2011-05-03 2012-11-08 Khs Gmbh Method and device for packaging groups of objects combined into packaging units

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0008960A2 (en) * 1978-09-13 1980-03-19 Sekisui Kagaku Kogyo Kabushiki Kaisha A foamed resin structural material and process for manufacturing the same
DE4111638A1 (en) * 1991-04-10 1992-10-15 Basf Ag Multilayer board with honeycomb core and thermoset adhesive layers - has outer layers of partly crystalline thermoplastic activated by corona treatment or application of amorphous thermoplastic
US5290489A (en) * 1992-06-25 1994-03-01 R. Lee Williams Apparatus and method for treating the interior surfaces of hollow plastic objects for improving adhesive properties
DE19926374A1 (en) * 1998-06-17 1999-12-23 Arcotec Oberflaechentech Gmbh Corona discharge unit pretreating both sides of material band and dispensing with costly vacuum plant
US20040067309A1 (en) * 2001-04-17 2004-04-08 Fts Systems Llc (Aka Fts Llc) Method and apparatus, with redundancies, for treating substrate plastic parts to accept paint without using adhesion promoters

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2443753A1 (en) 1978-12-07 1980-07-04 Antoine Antoine Surface treatment of plastics to improve paint or adhesive bonding - to improve paint or adhesive bonding properties by corona bombardment using demountable electrodes
FR2760999B1 (en) 1997-03-19 1999-04-30 Guy Ducruy METHOD FOR MANUFACTURING AN ALVEOLAR STRUCTURE IN THERMOFUSIBLE MATERIAL, AND DEVICE FOR CARRYING OUT SAID METHOD

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0008960A2 (en) * 1978-09-13 1980-03-19 Sekisui Kagaku Kogyo Kabushiki Kaisha A foamed resin structural material and process for manufacturing the same
DE4111638A1 (en) * 1991-04-10 1992-10-15 Basf Ag Multilayer board with honeycomb core and thermoset adhesive layers - has outer layers of partly crystalline thermoplastic activated by corona treatment or application of amorphous thermoplastic
US5290489A (en) * 1992-06-25 1994-03-01 R. Lee Williams Apparatus and method for treating the interior surfaces of hollow plastic objects for improving adhesive properties
DE19926374A1 (en) * 1998-06-17 1999-12-23 Arcotec Oberflaechentech Gmbh Corona discharge unit pretreating both sides of material band and dispensing with costly vacuum plant
US20040067309A1 (en) * 2001-04-17 2004-04-08 Fts Systems Llc (Aka Fts Llc) Method and apparatus, with redundancies, for treating substrate plastic parts to accept paint without using adhesion promoters

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2456659A (en) * 2008-01-22 2009-07-29 Matthew Smyth High structural strength sandwich panel
US9604442B2 (en) 2008-11-24 2017-03-28 Applied Ft Composite Solutions Inc. Peeling process for making resilient pad composite
US11890843B2 (en) 2010-11-24 2024-02-06 Applied Ft Composite Solutions Inc. Composite cushioning material and jigless method for making the same
WO2016026217A1 (en) * 2014-08-19 2016-02-25 株洲时代新材料科技股份有限公司 Flame-retardant lightweight structural core and manufacturing method therefor
DE102018122098A1 (en) * 2018-09-11 2020-03-12 Rehau Ag + Co Process for making a foamed sheet
CN110154974A (en) * 2019-06-28 2019-08-23 东莞职业技术学院 For improving the automotive hood of pedestrian safety

Also Published As

Publication number Publication date
DE202006020359U1 (en) 2008-07-10
FR2887174B1 (en) 2007-08-24
FR2887174A1 (en) 2006-12-22

Similar Documents

Publication Publication Date Title
EP2878427B1 (en) Method for manufacturing a part made of sandwich material and part manufactured according to such a method
WO2006134079A1 (en) Composite part such as a panel, comprising a honeycomb structure
EP0686520B1 (en) Composite trimming with double wall for motor vehicle
EP2268482B1 (en) Damping skin for protecting composite parts
EP3445578B1 (en) Multilayer panel
EP2855140A1 (en) Method for producing a piece of reinforced equipment, in particular for a motor vehicle
EP2412613B1 (en) Body module for refrigerated vehicles including a vacuum insulation panel, and associated manufacturing method
EP0744281B1 (en) Sound absorbing product having an integrated energy absorber and production method thereof
EP1859978B1 (en) Thermoplastic sheet with adhesive mass for a body element
FR2753673A1 (en) SHELL STRUCTURE IN PLASTIC MATERIAL ARMED WITH FIBERS FOR VEHICLES OR CONTAINERS, IN PARTICULAR FOR RAIL VEHICLE CASES
EP1333222B1 (en) Method for making a thin composite vacuum insulation panel with high stiffness facings
FR2905391A1 (en) Coating material for use as e.g. building`s roof coating, has thermal insulating component extended on ribbed or wavy foil by using self-adhesive mass, where component is constituted of polyethylene foam between foil and polyester film
EP2671782A1 (en) Bodywork module for a refrigerated vehicle comprising a vacuum insulating panel, and process for manufacturing such module
EP2725162A1 (en) Building block formed from an aerated concrete body wrapped in plastic
FR2860533A1 (en) INSULATING PANEL
FR2591147A1 (en) Novel rigid laminated composite material
WO1995015870A1 (en) Sealing panel, particularly for cars, comprising a loud speaker mounting location
BE1005424A6 (en) Building element with a cell structure and method for manufacturing construction element.
EP2468500A1 (en) Vibration damping membrane structure and roof covers using said structure
FR2862078A1 (en) Temporary structure manufacturing procedure uses insulating panels joined by at least one integral membrane extending from one panel to next
FR2989021A1 (en) Sandwich panel, useful for thermal and/or acoustics insulation in e.g. walls of buildings, comprises outer facing covered with antivibratory membranous complex including external membrane consisted of thin layer or sheet of PVC
FR2916775A1 (en) BUILDING ELEMENT SUCH AS AN HOURDIS
FR2854418A1 (en) Sandwich panel with high acoustic insulation has outer skin made from sheet metal with surface coating of impact absorbing material
BE1005425A6 (en) Construction component having a welded cellular structure
FR3096923A1 (en) Manufacturing process of a part of motor vehicle equipment and associated part

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application
NENP Non-entry into the national phase

Ref country code: DE

WWW Wipo information: withdrawn in national office

Country of ref document: DE

122 Ep: pct application non-entry in european phase

Ref document number: 06763631

Country of ref document: EP

Kind code of ref document: A1