WO1995023179A1 - Sheet material - Google Patents
Sheet material Download PDFInfo
- Publication number
- WO1995023179A1 WO1995023179A1 PCT/NL1995/000071 NL9500071W WO9523179A1 WO 1995023179 A1 WO1995023179 A1 WO 1995023179A1 NL 9500071 W NL9500071 W NL 9500071W WO 9523179 A1 WO9523179 A1 WO 9523179A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- fibers
- layer
- plastic
- substrate
- sheet material
- Prior art date
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
- B29C37/00—Component parts, details, accessories or auxiliary operations, not covered by group B29C33/00 or B29C35/00
- B29C37/0078—Measures or configurations for obtaining anchoring effects in the contact areas between layers
- B29C37/0082—Mechanical anchoring
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/114—Single butt joints
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/303—Particular design of joint configurations the joint involving an anchoring effect
- B29C66/3034—Particular design of joint configurations the joint involving an anchoring effect making use of additional elements, e.g. meshes
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/45—Joining of substantially the whole surface of the articles
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/47—Joining single elements to sheets, plates or other substantially flat surfaces
- B29C66/472—Joining single elements to sheets, plates or other substantially flat surfaces said single elements being substantially flat
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
- B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/04—Interconnection of layers
-
- C—CHEMISTRY; METALLURGY
- C08—ORGANIC MACROMOLECULAR COMPOUNDS; THEIR PREPARATION OR CHEMICAL WORKING-UP; COMPOSITIONS BASED THEREON
- C08J—WORKING-UP; GENERAL PROCESSES OF COMPOUNDING; AFTER-TREATMENT NOT COVERED BY SUBCLASSES C08B, C08C, C08F, C08G or C08H
- C08J5/00—Manufacture of articles or shaped materials containing macromolecular substances
- C08J5/12—Bonding of a preformed macromolecular material to the same or other solid material such as metal, glass, leather, e.g. using adhesives
- C08J5/124—Bonding of a preformed macromolecular material to the same or other solid material such as metal, glass, leather, e.g. using adhesives using adhesives based on a macromolecular component
-
- 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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/481—Non-reactive adhesives, e.g. physically hardening adhesives
- B29C65/4815—Hot melt adhesives, e.g. thermoplastic adhesives
-
- 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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
-
- 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
- B29C65/00—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
- B29C65/48—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding
- B29C65/4805—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor using adhesives, i.e. using supplementary joining material; solvent bonding characterised by the type of adhesives
- B29C65/483—Reactive adhesives, e.g. chemically curing adhesives
- B29C65/485—Multi-component adhesives, i.e. chemically curing as a result of the mixing of said multi-components
-
- 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
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/70—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material
- B29C66/71—General aspects of processes or apparatus for joining preformed parts characterised by the composition, physical properties or the structure of the material of the parts to be joined; Joining with non-plastics material characterised by the composition of the plastics material of the parts to be joined
Definitions
- the present invention relates to a sheet material based on a substrate coated with at least one layer of a thermoplastic plastic.
- a sheet material based on a substrate coated with at least one layer of a thermoplastic plastic.
- Such material can be flat, but can also have a round or other bent form.
- the manufacture of sheet materials based on more than one layer involves the problem that a proper bond should be provided between the various layers. This problem for instance occurs when sandwich sheets are manufactured, but also when protective and/or decorative surfaces are provided on composite or non-composite sheet materials. Particularly in the case of sheet materials having a non-flat form, this may be a greater problem.
- US Patent 5,037,690 describes a sandwich material built up of a core layer having its two surfaces provided with a layer of fiber material impregnated with a polyurethane resin. Especially in the case where the core material has a honeycomb structure, a proper bond can thus be obtained between the fiber layer and the honeycomb structure, because the honeycomb material i_ --.lightly pressed into the fiber layer where the polyurethane resin provides a bond between fiber and core.
- the polyurethane resin also has the function of binding agent for the surface layer.
- a layer of plastic is often provided on the surface.
- acrylate polymers or olefin polymers are preferably used, because they are chemically particularly inert and typically have a mechanically strong surface (scratch-resistant) .
- this inertness has the problem that the bond of the plastic to the base material, the substrate, is difficult.
- sandwich materials consist of a typically light-weight core material, for instance a honeycomb material, comprising two top layers.
- a typically light-weight core material for instance a honeycomb material
- the consequence could be that the strength of the entire sheet is too slight. This may for instance occur if it is desired to incorporate a polyolefin or poly ethacrylate into the sheet.
- the invention provides a solution to the problem of obtaining a sufficient bond between various materials.
- the invention relates to a sheet material comprising a substrate coated with at least one layer of a prefi --- ij thermoplastic plastic, which substrate and/or substrate side of this layer is provided with fibers that are anchored to the plastic layer and/or the substrate and partly project therefrom, while this plastic layer is bonded to the substrate by means of a bonding agent.
- this means that the layer of plastic material to be applied is treated so that a fiber layer is anchored to its surface.
- This may for instance be effected by means of a (direct or indirect) heating of the surface layer, whereupon a fiber layer is partly pressed into the surface.
- heating methods are heat radiation, open-flame heating, induction heating, electromagnetic radiation and radiation utilizing a hot plate or a hot liquid. It is also possible to soften the surface with a suitable solvent or to use a combination of the two methods.
- the thus produced thermoplastic plastic whose surface has been provided with fibers is subsequently provided on the surface of the substrate by means of a bonding agent.
- a fiber layer to a base by means of an adhesive, such as an acrylate adhesive or a thermosetting plastic, such as an epoxy or unsaturated polyester resin.
- an adhesive such as an acrylate adhesive or a thermosetting plastic, such as an epoxy or unsaturated polyester resin.
- a single or a composite material is generally employed as substrate.
- This material can be selected from the group consisting of sheet material of thermoplastic plastic, wood, plywood, chipboard, sheet material from fillers (popcorn, polystyrene granules, microspheres, glass globules or glass fibers, earth, clay, foamed rock, and the like) , bound with organic and/or inorganic binders (thermosetting plastics, biological binders, cement, water glass, gypsum and the like), multilayer systems on the basis of core material and/or film material and optionally filled honeycomb material. If a honeycomb material is employed, this material will have two top layers on which the plastic provided with f be s is provided. It is also possible to use various combinations of this type of materials.
- An interesting variant is f ⁇ rs-ed by ⁇ ater-resistant gypsum board, with which, according to the invention, an excellent non-inflammable sheet material can be produced, without it having the somewhat unattractive appearance of conventional gypsum boards .
- the above-mentioned products are divisible into two groups, i.e. the single materials, suitable for the manufacture of worktops and other sheet-shaped objects, and the composite materials or sandwich materials, consisting of a light core and two surface layers.
- both groups of materials concern relatively high-grade materials, as opposed to the materials described in European patent application 179.451.
- This application particularly relates to bituminous roofing materials that are constructed by means of a fiber layer as bonding layer.
- thermoplastic plastic Providing the coating of a thermoplastic plastic on the substrate can be effected in a number of manners . It can for instance be effected by means of hot melts or a thermosetting plastic (resin with hardener) .
- thermosetting plastics are epoxy resins, polyurethane resins and unsaturated polyester resins.
- the fibers to the substrate in the same manner as to the coating, for instance by providing the fibers of the coating in a softened surface of the substrate.
- This softening can be realized by heating the surface of the substrate, or by softening by means of a solvent.
- an adhesive is used that is dissolved in a solvent for the plastic, a combination of the two effects occurs .
- the fiber layer is provided in the surface of the substrate, after which the coating is bonded to the surface of the fibers by the use of techniques suitable for that purpose, such as the use of adhesive, or by means of softening.
- various materials can be used as fibers, which may each in itself be incorporated in various structures into the thermoplastic plastic.
- materials for the fibers synthetic and/or natural fibers and/or metal fibers can be used.
- fibers are used selected from the group consisting of hemp, flax, elephant grass, jute, bagasse, glass fibers, carbon fibers and synthetic fibers such as polyester fibers, acrylic fibers, polyethylene fibers, polypropylene fibers and polyamide fibers.
- These fibers can be provided in the thermoplastic plastic material as separate fibers, or as non-woven, knit fabric, felt, a woven material or a scrim.
- metal fibers it is also possible to use a net of metal.
- the sheet materials according to the invention may consist of single materials provided with a coating or of composite materials. With respect to the synthesis and structure of these material there are hardly any limitations.
- the form can be adjusted to the eventual application, which means that it can be flat, but it is also possible to create round or other forms.
- An important use of the invention lies in the manufacture of worktops, such as drainboard tops or tabletops, which worktops should have a plastic finishing layer. It is not easy to apply such a layer, because the materials that can most suitably be used as finishing layer, such as acrylate polymers and more particularly polymethylmethacrylate, exhibit a poor bond to the conventional substrate materials.
- the invention provides a simple system for these worktops which also permits realization of a good bond of acrylates to the conventional base materials, such as wood, plywood, chipboard, MDF and the like. It is observed that two problems play a part in the production of such worktops. In the first place, the top layer should be properly bonded to the substrate.
- a second aspect forms the finishing strip that is to be provided on the lateral side of the material afterwards.
- This strip should bond properly and uiu-cct to the material so as to be water-resistant.
- PMMA polymethyl methacrylate
- honeycomb materials As material for the core of the sandwich material, various types of honeycomb materials can be used, for instance produced from paper, metal, or plastic. It is also possible to use plastic foams such as polyurethane foam, polyether foam, polyolefin foam or styrene polymer foam.
- the core can also be built up of a number of layers of a different nature. Because it is now possible to provide relatively inert materials as coating on other materials, light-weight construction materials can be provided according to the invention in a relatively cheap manner and for various applications.
- Examples thereof are, inter alia, sheet materials for grease traps, sewer components and (insulating) sandwich boards, for instance for wall or roof panels, by incorporating blister padding that can optionally be provided with an aluminum layer, in combination with honeycomb materials in the core, on which a finishing layer has been provided.
- blister padding can optionally be provided with an aluminum layer, in combination with honeycomb materials in the core, on which a finishing layer has been provided.
- wall and roof panels can be provided with a brickwork structure or a rooftile structure.
- heating elements in the material for instance in the form of heating strips of conductive plastic (having a fiber layer), or to use decorative materials in or under the top layer.
- sandwich panels according to the invention are silos for solids or liquids, housings for air-ventilation/airconditioning systems, gas washers and cooling towers and the like. Generally, it applies that these materials can be used where a supporting power should be combined with a low weight and possibly a chemical resistance.
- Both the worktops and the sandwich materials according to the invention can be provided with a decorative layer.
- a possible embodiment of such decorative layers is formed by synthetic resin bound solids with a decorative effect. Examples thereof are natural stone, waste materials with glittering effect (anthracite grit and the like), natural substances such as maize, peas, rice and other seeds.
- such a decorative layer based on a transparent synthetic resin, may comprise glass particles, preferably provided in the top layer of the resin, resulting in a strong, scratch-resistant and decorative top.
- the resin and the glass particles are chosen so that the refractive indices are identical, which is advantageous from a decorative point of view.
- a suitable material that according to the invention can be used as core material for a sandwich sheet comprises an optionally filled honeycomb material and two upper layers built up of a layer of a plastic, bonded to a fibrous web containing expanded microglobules, the upper layers being bonded to the honeycomb material via the fibrous web utilizing a thermosetting plastic.
- a finishing layer may be provided again, with this core material functioning as substrate for the finishing layer.
- Fig. 1 shows a conventional sandwich panel built up of a core material (honeycomb) combined with two layers of thermosetting material.
- Fig. 2 shows a thermoplastic sheet to which a fiber mat is anchored.
- Fig. 3 shows a comparable sheet to which a glass fabric is anchored.
- Fig. 4 shows a sheet as in Fig. 2, having a fiber mat on both sides.
- Fig. 5 shows a sandwich material based on a conventional sandwich material, having two sheets according to Fig. 2 provided thereon by means of a thermosetting resin.
- Fig. 6 shows a -multi-layer construction built up of a sheet according to Fig. 4 and two sheets according to Fig. 2, bonded together with layers of thermosetting resin.
- Fig. 7 shows an insulating sandwich construction built up of a honeycomb core material and two layers of plastic blister padding, provided with the blisters facing the honeycomb and having a layer of aluminum on the outer side.
- a layer of aluminum by means of the invention is a coating of a thermoplastic plastic, such as polyolefin or polyester.
- Fig. 8 shows the principle of providing a finishing strip on the lateral side of a worktop.
Abstract
Description
Claims
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP95909131A EP0796290A1 (en) | 1994-02-23 | 1995-02-23 | Sheet material |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
NL9400274A NL9400274A (en) | 1994-02-23 | 1994-02-23 | Plate-shaped material. |
NL9400274 | 1994-02-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
WO1995023179A1 true WO1995023179A1 (en) | 1995-08-31 |
Family
ID=19863866
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/NL1995/000071 WO1995023179A1 (en) | 1994-02-23 | 1995-02-23 | Sheet material |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0796290A1 (en) |
NL (1) | NL9400274A (en) |
WO (1) | WO1995023179A1 (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL1020062C2 (en) * | 2002-02-26 | 2004-04-06 | Rombouts Kunststof Techniek B | Bonding articles to fibre reinforced amorphous plastic bodies, e.g. for making shuttering sections, by heating surface of body prior to applying adhesive |
WO2006119149A2 (en) * | 2005-05-04 | 2006-11-09 | Shawmut Corporation | Halogen and plasticizer free permeable laminate |
WO2009002815A1 (en) * | 2007-06-22 | 2008-12-31 | Ocv Intellectual Capital, Llc | Process for assembly of thermoplastic pieces |
FR2962362A1 (en) * | 2010-07-12 | 2012-01-13 | Alain Catherineau | Composite panel for aircraft interior fitting e.g. partition element, has aluminum film interposed between thin log veneer and resin fabric layer and integrated on one of faces of thin log veneer by adhesive layer |
WO2015014687A1 (en) * | 2013-08-01 | 2015-02-05 | Thyssenkrupp Ag | Method for producing tubular fiber composite bodies |
WO2015015202A1 (en) * | 2013-08-01 | 2015-02-05 | Blade Dynamics Limited | Erosion resistant aerodynamic fairing |
EP2993030A1 (en) * | 2014-09-05 | 2016-03-09 | Airbus Defence and Space GmbH | Fiber composite component, adhesive fitting for fiber composite components, and method for manufacturing a fiber composite component and an adhesion assembly |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1034738A (en) * | 1963-05-09 | 1966-07-06 | Reinforced Plastics Ltd | Improved method of bonding together thermo-plastic and thermo-setting materials |
US3431157A (en) * | 1965-12-20 | 1969-03-04 | Gen Motors Corp | Method of bonding glass fiber reinforced plastic panels to other materials |
DE2156481A1 (en) * | 1970-11-19 | 1972-05-31 | Gebrüder Sulzer AG, Winterthur (Schweiz) | Table top, in particular for garden tables |
US4135019A (en) * | 1977-03-16 | 1979-01-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Low density bismaleimide-carbon microballoon composites |
EP0179451A2 (en) * | 1984-10-22 | 1986-04-30 | The Dow Chemical Company | Method for adhering a coating material to a random-fiber composite sheet |
-
1994
- 1994-02-23 NL NL9400274A patent/NL9400274A/en not_active Application Discontinuation
-
1995
- 1995-02-23 EP EP95909131A patent/EP0796290A1/en not_active Ceased
- 1995-02-23 WO PCT/NL1995/000071 patent/WO1995023179A1/en not_active Application Discontinuation
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1034738A (en) * | 1963-05-09 | 1966-07-06 | Reinforced Plastics Ltd | Improved method of bonding together thermo-plastic and thermo-setting materials |
US3431157A (en) * | 1965-12-20 | 1969-03-04 | Gen Motors Corp | Method of bonding glass fiber reinforced plastic panels to other materials |
DE2156481A1 (en) * | 1970-11-19 | 1972-05-31 | Gebrüder Sulzer AG, Winterthur (Schweiz) | Table top, in particular for garden tables |
US4135019A (en) * | 1977-03-16 | 1979-01-16 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Low density bismaleimide-carbon microballoon composites |
EP0179451A2 (en) * | 1984-10-22 | 1986-04-30 | The Dow Chemical Company | Method for adhering a coating material to a random-fiber composite sheet |
Cited By (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
NL1020062C2 (en) * | 2002-02-26 | 2004-04-06 | Rombouts Kunststof Techniek B | Bonding articles to fibre reinforced amorphous plastic bodies, e.g. for making shuttering sections, by heating surface of body prior to applying adhesive |
WO2006119149A2 (en) * | 2005-05-04 | 2006-11-09 | Shawmut Corporation | Halogen and plasticizer free permeable laminate |
WO2006119149A3 (en) * | 2005-05-04 | 2007-01-18 | Shawmut Corp | Halogen and plasticizer free permeable laminate |
US8216660B2 (en) | 2005-05-04 | 2012-07-10 | Shawmut Corporation | Halogen and plasticizer free permeable laminate |
WO2009002815A1 (en) * | 2007-06-22 | 2008-12-31 | Ocv Intellectual Capital, Llc | Process for assembly of thermoplastic pieces |
FR2962362A1 (en) * | 2010-07-12 | 2012-01-13 | Alain Catherineau | Composite panel for aircraft interior fitting e.g. partition element, has aluminum film interposed between thin log veneer and resin fabric layer and integrated on one of faces of thin log veneer by adhesive layer |
WO2015014687A1 (en) * | 2013-08-01 | 2015-02-05 | Thyssenkrupp Ag | Method for producing tubular fiber composite bodies |
WO2015015202A1 (en) * | 2013-08-01 | 2015-02-05 | Blade Dynamics Limited | Erosion resistant aerodynamic fairing |
CN105934327A (en) * | 2013-08-01 | 2016-09-07 | 叶片动力学有限公司 | Erosion resistant aerodynamic fairing |
US10240578B2 (en) | 2013-08-01 | 2019-03-26 | Blade Dynamics Limited | Erosion resistant aerodynamic fairing |
EP2993030A1 (en) * | 2014-09-05 | 2016-03-09 | Airbus Defence and Space GmbH | Fiber composite component, adhesive fitting for fiber composite components, and method for manufacturing a fiber composite component and an adhesion assembly |
US10047465B2 (en) | 2014-09-05 | 2018-08-14 | Airbus Defence and Space GmbH | Method for manufacturing a fiber composite component |
EP3489000A1 (en) * | 2014-09-05 | 2019-05-29 | Airbus Defence and Space GmbH | Method for producing a fibre compound component |
Also Published As
Publication number | Publication date |
---|---|
EP0796290A1 (en) | 1997-09-24 |
NL9400274A (en) | 1995-10-02 |
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