Classifications

• • 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
  • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
  • B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
  • B29C70/68—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks
  • B29C70/84—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts by incorporating or moulding on preformed parts, e.g. inserts or layers, e.g. foam blocks by moulding material on preformed parts to be joined
• • B—PERFORMING OPERATIONS; TRANSPORTING
  • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
  • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
  • B29C70/00—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts
  • B29C70/88—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced
  • B29C70/887—Shaping composites, i.e. plastics material comprising reinforcements, fillers or preformed parts, e.g. inserts characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced locally reinforced, e.g. by fillers
• • 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
  • B32B27/00—Layered products comprising a layer of synthetic resin
  • B32B27/06—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material
  • B32B27/065—Layered products comprising a layer of synthetic resin as the main or only constituent of a layer, which is next to another layer of the same or of a different material of foam
• • 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
  • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
  • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
  • B32B5/024—Woven fabric
• • 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
  • B32B5/00—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts
  • B32B5/02—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by structural features of a fibrous or filamentary layer
  • B32B5/026—Knitted fabric
• • 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
  • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
  • B32B2260/02—Composition of the impregnated, bonded or embedded layer
  • B32B2260/021—Fibrous or filamentary layer
• • 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
  • B32B2260/00—Layered product comprising an impregnated, embedded, or bonded layer wherein the layer comprises an impregnation, embedding, or binder material
  • B32B2260/04—Impregnation, embedding, or binder material
  • B32B2260/046—Synthetic resin
• • 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
  • B32B2419/00—Buildings or parts thereof

Definitions

• This invention relates to a method for modifying a sheet ⁇ like sandwich material comprising a core material provided between two top layers.
• Sheet-like materials such as sandwich constructions, are often used for those applications where high strength or rigidity in combination with a light weight is required. This is the case, for example, in air, space, and transport applications.
• Sandwich constructions generally consist of a core material that is light in weight, with a top layer, often reinforced, on both surfaces thereof. Owing to the good bonding between the top layers and the core material, the . proper stiffness is obtained. The other properties of the material are partly determined by the nature of the various materials .
• Known sandwich constructions are based on a core material having a honeycomb structure.
• Another type of sandwich material is described in European patent applications Nos. 264,495 and 269,148, the contents of which are incorporated herein by reference.
• This material is fully thermoplastic and consists of a core material including inter alia a thermoplastic foam and two top layers consisting of a fiber-reinforced synthetic plastics material, such as polycarbonate or polyether imide.
• U.S. Patent No. 4,889,763 discloses a flame-resistant sheet-like material which is also thermoplastic.
• European patent application No. 345,855 relates to a non- foamed film which can be used for the manufacture of a thermoplastic sandwich material.
• Sandwich constructions are typically in the form of a plate, for instance a wall panel, to which various objects must be secured. As this may locally involve rather considerable forces, it is necessary to provide local reinforcement to enable objects, such as auxiliary means, to be secured thereto.
• European patent application 383,409 describes a method for providing reinforcements in a preferably thermoplastic core of a sandwich material by injecting under pressure an amount of plastic material through one of the top layers into the core material, which plastic material hardens after injection. This method provides good possibilities for the application of auxiliary means, such as fastening means, brackets, lamp holders, and the like.
• the present invention accordingly relates to a method for modifying a sheet-like sandwich material comprising a core material provided between two top layers, wherein under pressure an amount of thermoplastic material is injected through one of the top layers into the core material, an object is placed in the still plastic material, whereafter the plastic material hardens.
• the modification of the sandwich material can occur in different manners.
• a first possibility is to provide a reinforcement in which an object is fixedly secured in the manner according to the invention. Through the specific method, a very * good bonding is obtained, even in the case where an object of an unusual form is provided. With the known method, in which first the reinforcement is provided and subsequently, after hardening, an auxiliary means is arranged, it is impossible or practically impossible to arrange such o ects.
• a second variant of the method according to the invention is to arrange an object which is subsequently removed during or after hardening. In that case, the removal should occur after the thermoplastic material has become sufficiently form- retaining.
• a modification is manufactured which consists of a reinforcement which is eminently bonded within the sandwich material and which is provided with an opening extending, for instance, all the way through the material or only through a part of the material.
• a screw thread in the modification it is also possible to provide a screw thread in the modification.
• an object is arranged which is provided with a screw thread on the outside thereof. After hardening of the synthetic material, the object is unscrewed from the modification.
• a releasing agent for instance a silicone compound
• the object when carrying out the method, it is preferred if the object, at the time of its arrangement in the plastic material, has a temperature which is lower than the temperature of the plastic material of the reinforcement. It has been found that in such a case an optimum bonding of the object in the core is obtained. If this temperature is equal to or higher than the temperature of the plastic material, a lesser but no poor bonding is obtained. More specifically, the object has a temperature which is not higher than 75°C and most preferably not higher than 35°C.
• the material of the reinforcement should not have hardened yet when the object is arranged in the core.
• the temperature of the plastic material should be above the softening point thereof, it being noted that it is preferred, for reasons of applicability under more or less extreme temperature conditions, to use a thermoplastic synthetic material having a softening temperature which is at least 50°C and preferably above 75°C (HDT, according to ASTM D 648-56) .
• a thermoplastic synthetic material having a softening temperature which is at least 50°C and preferably above 75°C (HDT, according to ASTM D 648-56) .
• the plastic material is forced into the core under pressure.
• the material can be injected directly through the top layer, provided the top layer is suitable for that purpose. Otherwise, first an opening must be provided in the top layer. This may be necessary in particular in the case where one or both top layers are made of metal or any other material that is difficult to penetrate.
• the core material is displaced and/or caused to melt by the plastic material at the place of the injection.
• the core of the sandwich material consists of a thermoplastic material, for instance a thermoplastic synthetic plastics foam or a thermoplastic honeycomb material, fusion in particular occurs, as described in European patent application 383,409. If the core material is not thermoplastic, it is displaced by the injected material. With -regard to bonding and material properties, it is preferred to use a thermoplastic core material.
• the amount of material to be injected and the temperature thereof are set such that a part of the core material, more specifically the foam, melts away at the place of the injection.
• thermoplastic synthetic material preferably a thermoplastic synthetic material or mixture of thermoplastic synthetic materials is used, having a softening temperature of at least 50°C.
• synthetic materials can be selected inter alia from the group consisting of polystyrene, styrene polymers, acrylate and/or methacrylate polymers, polyolefins, polyesters, such as PET and PBT, polycarbonate, polyether imide, polyamide, polysulfone, polyether sulfone, polyether ketone, polyether ether ketone, polyether ketone ketone, polyphenylene oxide, polyphenylene sulfide and mixtures of two or more of these synthetic materials.
• Such materials not only have the advantage of being injectable into the core with facility, but also contribute to the improvement of the pressure resistance of the sheetd-like material.
• the sandwich material to be modified can be structured in different manners.
• the material consists of a core and two top layers .
• the core may made of a plurality of layers, for instance reinforcing layers and filling layers.
• the core may consist of any suitable core material, such as a synthetic foam which may or may not be thermoplastic, a honeycomb material which may or may not be thermoplastic, or any other suitable material.
• the thermoplastic foamed core material is a polyether imide foam, a polycarbonate foam, a polymethacrylamide foam, a polyester foam, such as a foam of PET or PBT, a polyether sulfone foam, a polyether ketone foam, a polyether ether ketone foam, a polyether ketone ketone foam, a polyphenylene oxide foam, a polyphenylene sulfide foam, or foam materials made from mixtures of thermoplastic synthetic materials incorporating at least one of the thermoplastic synthetic materials mentioned. It is also possible to use, as core material, a combination of two or more foams .
• liquid crystalline materials in the foam.
• the foam is generated in situ during the manufacture of the sandwich material, the use of such materials has been found to give good results .
• the above foam materials are used in combination with the thermoplastic synthetic materials, to be mentioned hereinafter, for the top layer and the reinforcement, an optimum construction of the reinforcement and a maximum strength of the total construction and of the reinforcement points are obtained.
• these synthetic materials are preferably reinforced with glass fibers, polyamide fibers, such as aramid fibers, polyethylene fibers, polyester fibers and carbon fibers .
• the nature of the fiber reinforcement in the top layer has substantially no influence on the conditions for injecting the thermoplastic synthetic material into the core, but the degree of reinforcement may have an effect on them.
• the density of the fiber reinforcement in the skin is higher, the more pressure will have to be exerted for injection through the top layer.
• these pressure variations always range within conventional injection molding pressures. In the case of very high densities of the fibers in the skin, it may in certain cases be desirable or advantageous to pre-drill a small hole in the skin.
• the sandwich construction can be manufactured by arranging the components, core material and top layers to be used on top of each other, optionally with bonding layers between them, with or without the use of softening agents, and subsequently bonding the layers together by applying heat and pressure.
• a foamed core material When a foamed core material is used, it is also possible to generate the material in situ by using an expandable material which foams and bonds to the top layers upon heating and/or reduction of the pressure.
• an expandable material An example of such an expandable material is described in European patent application 345,855, the contents of which are incorporated herein by reference. This material can be used for both the core material and an additional bonding layer. It is also possible to use the known thermosetting foam materials.
• the first step of the method according to the invention is quite simple to. perform utilizing existing equipment. In fact, when an injection molding machine is used, one only has to move the nozzle thereof to the place to be reinforced and to inject a metered dose of molten thermoplastic synthetic material.
• injection molding machines can be used. To the extent necessary, an adjustment can be effected so as to bring the nozzle to the proper place for the injection. It is also possible, however, to use modified equipment, for instance injection molding machines enabling injection of the plastic material directly into the core material. For this purpose, for example, use can be made of an apparatus comprising a kind of "needle-shaped" injection nozzle, which is introduced through the top layer into the core. It is also possible to use nozzles provided with more than one outlet opening, so that more than one plastic material can be utilized.
• the sheet-like material be supported at the back, i.e., the side where no injection takes place, so as to prevent the plastic material from being injected through the sheet.
• thermoplastic synthetic material from two sides of the sandwich material, for instance simultaneously or with a short interval.
• thermoplastic synthetic material is dosed depending on the nature of the material, the desired reinforcement in the core and the thickness of the sandwich construction. However, it has been found that the quantity is not very critical. For a sandwich construction of a thickness of 8 mm, a dosage of 0.5-20 ml of plastic material can be utilized. A good local reinforcement is then obtained.
• modified sandwich materials are obtained which are suitable for various applications.
• objects which are useful in the air and space industry. Examples include wall panels of aeroplanes, component parts of aeroplane chairs, component parts of trolleys and the like.
• the objects to be arranged may differ strongly.
• inserts can be arranged, such as screwed bushes or other anchoring points.
• forming blocks which may or may not be removable. These forming blocks can be provided on the same side where injection took place. It is also possible to mount the object from a lateral side.
• the object may also be an aid onto which a product can be injection molded. This may take place at the top, but also at the sides or at the bottom.
• the method according to the invention is applicable to flat sheet-like materials, but also to sheet-like objects already shaped. It is also of importance here that the reinforcement and the object generally have no influence on the further processability and deformability of the sheet-like material. This is of great importance for the thermoplastic sandwich constructions of the European patent applications mentioned, whose major advantage is in fact that they continue to be thermoplastically deformable.
• the manufacturing and processing methods described in the European patent applications mentioned in the introductory part of this specification can be applied without any problems to the materials according to the invention, both before and after the arrangement of the object. Examples of objects that can be provided include threaded bushes, hinges, pivots, and the like.
• a sandwich panel consisting of a foam core of polyether imide with a specific gravity of 90 kg/m 3 and two top layers of glass fiber web (107 g/m 2 ) , impregnated with polyether imide (50%), and 5 mm thick, was provided with a reinforcement. This was effected by injecting molten polyether imide through the top layer by means of an injection molding nozzle.
• the sandwich panel was supported on one side thereof by means of a metal plate, while on the other side the injection nozzle was positioned against the surface of the top layer.
• the injection nozzle was provided with a surface extension. Through the force of the injection, the material was injected into the core with an injection period of 2 seconds.
• a threaded bush of room temperature was subsequently placed in the still plastic material of the reinforcement.
• the reinforced surface obtained had a diameter of 30 mm.
• the compression strength at the place of the reinforcement was 170 N/mm 2 .
• the compressive strength of the panel itself was 3 N/mm 2 .
• the extraction value of the threaded bush was 240 kg.

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• Engineering & Computer Science (AREA)
• Chemical & Material Sciences (AREA)
• Composite Materials (AREA)
• Mechanical Engineering (AREA)
• Textile Engineering (AREA)
• Laminated Bodies (AREA)

Applications Claiming Priority (3)

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• 1992
  • 1992-04-28 NL NL9200781A patent/NL9200781A/nl not_active Application Discontinuation
• 1993
  • 1993-04-27 AU AU40916/93A patent/AU4091693A/en not_active Abandoned
  • 1993-04-27 EP EP93910437A patent/EP0671992A1/de not_active Withdrawn
  • 1993-04-27 JP JP5519140A patent/JPH07508938A/ja active Pending
  • 1993-04-27 WO PCT/NL1993/000088 patent/WO1993022135A1/en not_active Application Discontinuation

Non-Patent Citations (1)

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