US20110091715A1 - Foamed plastic sheet - Google Patents
Foamed plastic sheet Download PDFInfo
- Publication number
- US20110091715A1 US20110091715A1 US12/947,190 US94719010A US2011091715A1 US 20110091715 A1 US20110091715 A1 US 20110091715A1 US 94719010 A US94719010 A US 94719010A US 2011091715 A1 US2011091715 A1 US 2011091715A1
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- US
- United States
- Prior art keywords
- structural element
- weld seams
- body segments
- plastic
- shaped
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
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Classifications
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- 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
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/18—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by an internal layer formed of separate pieces of material which are juxtaposed side-by-side
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- 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
- B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
- B29C44/34—Auxiliary operations
- B29C44/56—After-treatment of articles, e.g. for altering the shape
- B29C44/5627—After-treatment of articles, e.g. for altering the shape by mechanical deformation, e.g. crushing, embossing, stretching
- B29C44/5654—Subdividing foamed articles to obtain particular surface properties, e.g. on multiple modules
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- 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
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
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- 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
- B29C66/73—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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/739—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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset
- B29C66/7392—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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic
- B29C66/73921—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 intensive physical properties of the material of the parts to be joined, by the optical properties of the material of the parts to be joined, by the extensive physical properties of the parts to be joined, by the state of the material of the parts to be joined or by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of the parts to be joined being a thermoplastic or a thermoset characterised by the material of at least one of the parts being a thermoplastic characterised by the materials of both parts being thermoplastics
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- 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
- B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
- B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
- B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C35/00—Heating, cooling or curing, e.g. crosslinking or vulcanising; Apparatus therefor
- B29C35/02—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould
- B29C35/08—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation
- B29C35/0805—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation
- B29C2035/0822—Heating or curing, e.g. crosslinking or vulcanizing during moulding, e.g. in a mould by wave energy or particle radiation using electromagnetic radiation using IR radiation
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- 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
- B29C2793/00—Shaping techniques involving a cutting or machining operation
- B29C2793/009—Shaping techniques involving a cutting or machining operation after shaping
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- 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
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
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- 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
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/14—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation
- B29C65/1403—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using wave energy, i.e. electromagnetic radiation, or particle radiation characterised by the type of electromagnetic or particle radiation
- B29C65/1412—Infrared [IR] radiation
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- 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
- B29C65/02—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
- B29C65/18—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
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- 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
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- 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
- B29C66/72—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 structure of the material of the parts to be joined
- B29C66/725—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 structure of the material of the parts to be joined being hollow-walled or honeycombs
- B29C66/7254—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 structure of the material of the parts to be joined being hollow-walled or honeycombs honeycomb structures
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- 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
- B29C66/72—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 structure of the material of the parts to be joined
- B29C66/727—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 structure of the material of the parts to be joined being porous, e.g. foam
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2067/00—Use of polyesters or derivatives thereof, as moulding material
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
- B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
- B29K2105/04—Condition, form or state of moulded material or of the material to be shaped cellular or porous
- B29K2105/046—Condition, form or state of moulded material or of the material to be shaped cellular or porous with closed cells
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2009/00—Layered products
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- 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
- B32B2323/00—Polyalkenes
- B32B2323/04—Polyethylene
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- 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
- B32B2325/00—Polymers of vinyl-aromatic compounds, e.g. polystyrene
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- 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
- B32B2327/00—Polyvinylhalogenides
- B32B2327/06—PVC, i.e. polyvinylchloride
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- 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
- B32B2355/00—Specific polymers obtained by polymerisation reactions only involving carbon-to-carbon unsaturated bonds, not provided for in a single one of index codes B32B2323/00 - B32B2333/00
- B32B2355/02—ABS polymers, i.e. acrylonitrile-butadiene-styrene polymers
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B32—LAYERED PRODUCTS
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- B32B2367/00—Polyesters, e.g. PET, i.e. polyethylene terephthalate
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B32B2398/00—Unspecified macromolecular compounds
- B32B2398/20—Thermoplastics
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T156/00—Adhesive bonding and miscellaneous chemical manufacture
- Y10T156/10—Methods of surface bonding and/or assembly therefor
- Y10T156/1052—Methods of surface bonding and/or assembly therefor with cutting, punching, tearing or severing
- Y10T156/1062—Prior to assembly
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
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- Y10T428/00—Stock material or miscellaneous articles
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/18—Longitudinally sectional layer of three or more sections
- Y10T428/183—Next to unitary sheet of equal or greater extent
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
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- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249982—With component specified as adhesive or bonding agent
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
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- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249987—With nonvoid component of specified composition
- Y10T428/249991—Synthetic resin or natural rubbers
Definitions
- the invention relates to a large area structural element containing a plurality of body segments arranged adjacent to one another in a plane, interconnected and made of a closed-cell foamed plastic, and a process for manufacturing such a large area structural element and the use thereof.
- foamed thermoplastic as the core layer in sandwich-type composites.
- the production of foamed plastic panels may be achieved e.g. by an extrusion process.
- the structural load-bearing capacity, in particular the compressive strength of such core layers made using extrusion processes is however limited. For demanding applications, therefore, sandwich composites with the above mentioned core layers are often not suitable as structural components.
- sandwich composites that exhibit a high degree of strength, in particular compressive strength and stiffness, and core materials that exhibit high shear strength and stiffness.
- use is made e.g. of stronger and much thicker outer layers. As a rule this leads to an undesirable increase in the specific weight of the sandwich composites.
- the compressive strength of such sandwich composites can not be increased in an unlimited manner by use of thicker outer layers.
- Sandwich composites are therefore known that exhibit improved strength by use of specific design of the core layer.
- Described in DE 197 15 529 C1 for example is the production of a sandwich composite with a core layer and outer layers on both sides thereof, whereby the core layer is made up of horizontally abutting polygonals e.g. cube-shaped foam segments.
- the individual foam segments are covered over with a fibre layer and fitted together in a device such that the sides of the segments are in contact with the fibre layer in a strut-Ike manner.
- the strut-like fibre layers are soaked with an impregnating medium. By hardening the impregnating medium fibre-composite layers are produced between the foam segments, thus providing a stiffening and strengthening effect on the core layer.
- a core layer produced in accordance with the described process is of a mixed type as the foam segments, fibre layers and impregnating medium result in at least three different materials being used.
- the object of the present invention is to propose a large area, in particular sheet-like structural element which is suitable for core layers in sandwich-type composites, whereby the structural element should contain a foam with a closed-cell structure.
- a further object is a cost favourable process for manu-facturing the mentioned large area structural element.
- the large area structural element should in particular exhibit improved compressive strength in com-parison with conventional foam panels.
- the large area structural element should also be as unmixed in character as possible.
- the structural element is made wholly of plastic, and the body segments are welded together at their abutting lateral faces forming flat weld seams, whereby the flat weld seams form a plastic intermediate layer which has few pores or is pore-free and which is provided in the form of a web structure that, when viewed from above, is reticular and reinforces the plastic sheet.
- the large area structural element is preferably sheet-shaped.
- the large area structural element is preferably in the form of a sheet-type element, in particular a block-shaped sheet element.
- the large area structural element comprises a thermoplastic, preferably a poly-styrene (PS), acrylnitrile/butadiene/styrene-grafted coploymer (ABS).
- PS poly-styrene
- ABS acrylnitrile/butadiene/styrene-grafted coploymer
- PE poly-ethylene
- PP polypropylene
- PVC polyvinylchloride
- PC polycarbonate
- PET polyethylene-terephthalate
- PPE poly-phenylene-ether
- PPE-FPS poly-blends thereof
- SAN styrene/acrylnitrile copolymer
- the structural element according to the invention is preferably unmixed i.e. it is comprised of only one single plastic.
- the unmixed character requires in particular that the structural element contains no other kind of adhesive for joining the body segments together.
- the specific weight of a structural element according to the invention is e.g. more than 20 kg/m 3 , preferably more than 40 kg/m 3 , in particular more than 50 kg/m 3 and e.g. less than 200 kg/m 3 , preferably less than 130 kg/m 3 .
- the pore size of the foam is e.g. in the range 100 to 1000 ⁇ m.
- the weld seams are preferably formed by plastic of the body segment which is melted then solidified after fitting the segments together. To that end the body segments exhibit, in particular at the abutting sides, zones in the form of areas that melt and re-solidify.
- the thickness of the weld seams or melt zones is chosen such that the network-like strut structure of the weld seams increases the compressive strength of structural element with respect to area pressure.
- the weld seams represent not only joins between two body segments, but at the same time stiffening or reinforcing struts of foam between the body segments.
- the weld seams also effect stiffening of the structural element with respect to shear and bending stresses.
- the expression of strength or thickness of the weld seams refers therefore not only to a stable weld seam but also to effective stiffening or reinforcing of the structure.
- the thickness of the melt/re-solidified zone at the side wall faces that constitute the weld seams is selected therefore such that the structural element exhibits in particular high compressive strength with respect to surface pressure.
- the body segments are preferably fitted and welded together in a continuous manner i.e. free of voids.
- the body segments therefore preferably exhibit a cross-sectional shape that enables the segments to be fitted together in rows without gaps.
- the body segments exhibit—in a plan view of the structural element—a poloygonal shape, in particular an eight, six, four or three sided shape.
- the body segments may in plan view of the structural element exhibit e.g. a quadratic, rectangular, hexagonal or triangular outline which runs around the so called top faces of the body segments.
- the size of the body segments may vary according to the degree of stiffness or compressive strength desired.
- the geometry and size of the body segments are determined primarily by the specific require-ments placed on the structural element.
- the body segments are especially preferably in the form of cubes or blocks.
- Body segments of block or cube shape may e.g. be arranged in several rows and columns, whereby the weld joints form a network-type structure with intersecting longitudinal and transverse weld seams.
- the said body segments may also be arranged in several rows that are offset with respect to each other, whereby the weld joints form continuous transverse weld seams and offset longitudinal weld seams creating a pattern like a brick wall.
- Quadratic shaped body segments may e.g. (as viewing the structural element in plan view) exhibit a quadratic or rectangular shaped outline with side lengths (x, y) of 20 to 600 mm, preferably 30 to 400 mm, in particular 40 to 100 mm (see also FIG. 1 ).
- a rectangular body segment may e.g. (as viewing the structural element in plan view) exhibit a length of 100 to 250 mm and a breadth of 30 to 50 mm.
- the body segments may—viewing the structural element in plan view—also exhibit a curved outline shape e.g. concave or convex in whole or in part.
- the body segments may also be shaped in a manner of interlocking bricks i.e. the body segments are shaped such that the individual body segments lock into each other.
- the body segments of the structural element according to the invention are also preferably congruent with respect to each other.
- the side faces of the body segments are also preferably perpendicular to the outer faces of the structural element.
- the invention also relates to a process for manufacturing a large area structural element containing a plurality of body elements of a foamed plastic that are aligned next to each other in a plane and joined together.
- the rod-shaped or column-shaped foam bodies are preferably manufactured using an extrusion process.
- the orientation of the material of the foam bodies or body segments preferably is preferably stretched in the direction of extrusion.
- polymer chains exhibit stretching in the direction of extrusion as a result of the extrusion process.
- the stretching of the material effects an improvement in the mechanical properties, in particular the compressive strength in the direction of stretching.
- the foam bodies or body segments also preferably exhibit a cell structure or cell arrangement that is oriented in the direction of extrusion.
- the oriented cell structures of the foam body contribute to an increase in the compressive strength of the structural element.
- rod-shaped or column-shaped foam bodies may be taken from a prefabricated block of foam i.e. by cutting or sawing.
- the said block of foam is manufactured by means of an extrusion process.
- the production of the foam bodies takes place via an extrusion process, whereby the foam body comprises a plurality of expanded polymer strands that are brought together. Drawing the strands together takes place immediately after leaving the extrusion die by expanding the individual strands. Thereby, neighbouring strands make contact with each other, grow together or stick together forming a foam body. The foam body is then in the form of a closed package of strands.
- the strands lie preferably essentially parallel to each other and are arranged in the longitudinal or extrusion direction of the foam body.
- the manufacturing pro-cess may be arranged such that the individual strands remain visible in the foam body or are brought together or melted to give one single structure in which the individual strands are only slightly or no longer detectable.
- the strands are preferably packed together so tightly that the individual strands come to rest fully in contact with each other without forming any spaces.
- the strands may, however, also be arranged or packed together such that channel-like spaces are formed between the individual strands.
- the strands are usefully created via an extrusion tool e.g. die plate, whereby the extrusion tool contains a plurality of neighbouring openings through which the polymer is extruded in the form of strands.
- the said openings may be round e.g. circular or elliptical shaped, or polygonal e.g. rectangular, quadratic or hexagonal.
- the openings may also be in the form of slits.
- the foamed strands may have a diameter of e.g. 3 to 50 mm, in particular 4 to 20 mm.
- shaping tool Situated downstream of the extrusion die there may also be another shaping tool that specifies the outer contour of the foam body, in which tool the strands are packed together on emerging from the extrusion die, so that the foam body takes on the cross-sectional shape of the shaping tool.
- the orientation of the individual strands of the body segments lies essentially perpendicular to the outer faces of the large area structural element made up of body segments.
- the compressive strength is preferably greater in the longitudinal direction of the strands i.e. in the direction of extrusion than in the other directions.
- the foam bodies may be produced using physical or chemical foaming means.
- the foam bodies are foamed physically using CO 2 .
- the introduction of the foaming agent may take place directly in the extrusion device.
- the extruded foam bodies are welded into plastic blocks on their long sides i.e. along the long sides that come into contact with each other. Large area, in particular sheet-shaped structural elements are subsequently cut from these plastic blocks transverse or perpendicular to the long sides of the foam bodies.
- the cutting of the large area structural elements out of the plastic blocks may be performed by sawing or using a thermal cutting process.
- the foam bodies may also be already cut into body segments whereby the individual body segments are subsequently welded together to form large area structural elements.
- the welding takes place preferably by melting the side faces of the body segments that are to be joined, followed by fitting these together and solidifying the molten zones.
- means for controlling the melting process during welding are employed that allow weld seams of a specific thickness or thickness range to be produced, whereby the thickness range is selected such that the web-like strut structure of weld seams produces a stiffening effect on the plastic sheet.
- the welding process is usefully one of thermoplastic welding.
- the production of the weld joint may take place by means of radiation welding or contact welding.
- Plastic welding processes that can be employed are e.g. welding with heating elements or infrared welding.
- the welding process may take place with or without weld-feed materials.
- the large area structural elements according to the invention exhibit greater stiffness and in particular greater compressive strength.
- the properties are due essentially to the weld seams between the individual body segments.
- the weld seams form a network of strut-like connections like a framework, whereby the weld seams are in the form of low-pore or pore-free, dense intermediate plastic layers.
- the framework of strut-like connected weld seams increases the compressive strength as the struts forming the intermediate plastic layer are significantly less compressible than the foam body itself. If, for example, surface pressure is applied to the structural element according to the invention (e.g. in the case of a sandwich composite via the outer layers onto the structural element serving as core layer), then the compressive forces act mainly on the stiff strut-like structure and not on the foam bodies themselves.
- the increase in stiffness of the structural element according to the invention is also a result of the framework-like nature of the weld seams which lead to an increase in the torsional and bend strength of the structural element.
- the structural element according to the invention finds application preferably in composite elements, in particular composite sheets with at least one outer sheet on one side of the structural element.
- the structural element according to the invention finds highly preferable application as core in sandwich composite elements, in particular sandwich composite elements with outer layers on both sides of the core layer.
- the sandwich composite elements may e.g. comprise a large area structural element according to the invention with an outer layer on both sides of the structural element. Further, it is also possible for there to be several layers on one or both sides of the structural element. If the structural element according to the invention is employed as a core layer in a sandwich composite sheet, the structural element is usefully a sheet element.
- the said layers or outer layers may be joined to each other and/or to the core layer e.g. by adhesive joining means.
- the outer layers may e.g. be rigid or flexible sheets of plastic or fibre reinforced plastic such as glass fibre reinforced plastic. Further, the outer layers may also be sheets of metal, in particular aluminium or an aluminium alloy. The outer layers are, in comparison with the core layer, usefully relatively thin sheets.
- sandwich composite elements with structural elements according to the invention exhibit a high degree of stiffness and excellent shear and compressive strength.
- Such sandwich structures are therefore suitable especially for applications which require components which are light in eight but structurally high load bearing.
- Sandwich-type composite elements with structural elements according to the invention as core layer may e.g. be employed as construction elements in the building industry.
- construction elements are walls, floors, ceilings, doors, dividing walls or cladding elements.
- Sandwich composite elements with structural elements according to the invention as core layer also find preferred application in transportation on land (e.g. road or railway vehicle manufacture), on water (e.g. ship and boat building, equipment for water sports) or in the air (e.g. aircraft construction).
- This may be e.g. sandwich composite elements according to the invention for trunk structures, loading platforms, walls, ceilings, floors, lids, cladding or parts thereof, on or as part of lorries or railway trucks for goods transport, or walls, ceilings, floors, intermediate walls, cladding elements, doors, lids or parts hereof, on vehicles for public transport such as omnibusses, trams, railway carriages or on ships such as passenger ships, ferries, pleasure steamers or boots.
- the sandwich composite elements according to the invention may also find application in sports articles for use on land, water or air.
- Sandwich composite elements with structural elements as core layer according to the invention are highly preferred for application as vanes or rotor-blades for wind powered generating units.
- FIG. 1 an explosive view of a sandwich composite with a structural element according to the invention as core layer;
- FIG. 2 a cross-section through a sandwich composite with a structural element according to the invention as core layer;
- FIG. 3 plan view of a first version of structural element according to the invention
- FIG. 4 plan view of a second version of structural element according to the invention.
- FIG. 5 plan view of a third version of structural element according to the invention.
- FIG. 6 plan view of a fourth version of structural element according to the invention.
- FIG. 7 plan view of a fifth version of structural element according to the invention.
- FIG. 8 plan view of a sixth version of structural element according to the invention.
- FIG. 9 perspective view of a plastic block for manufacturing structural elements according to the invention as shown in FIG. 5 .
- FIG. 1 shows a sandwich composite element 1 with a core layer of structural element according to the invention, which is in the form of a plastic sheet 10 (see also FIG. 3 ).
- the plastic sheet 10 is made up of block-shaped body segments 11 which are joined together at their touching side faces 17 via longitudinal and transverse weld seams 12 , 13 that extend over the said side faces 17 .
- the weld seams 12 , 13 form thereby (as seen in plan view) a network-like, stiff structure of struts.
- an outer layer 2 , 3 Provided on each side of the core layer on the outer faces 16 of the body segments 11 is an outer layer 2 , 3 .
- the outer layers 2 , 3 may be in the form of plastic sheets, fibre reinforced sheets (e.g. fibre-glass reinforced duroplastics or thermoplastics) or metal sheets, in particular aluminium sheets.
- FIG. 2 shows a cross-sectional view of a sandwich composite element 1 as in FIG. 1 .
- the outer layers 2 , 3 are joined to the core layer by means of adhesive bonding.
- FIGS. 3 to 7 show various versions of structural elements according to the invention in the form of plastic sheets 10 , 20 , 30 , 40 , 50 , 60 made up of body segments 11 , 21 , 31 , 41 , 51 , 61 , of different geometrical shapes and arrangement that are arranged lying next to each other.
- the plastic sheets 10 , 20 shown in FIGS. 3 and 4 contain body segments 11 , 21 of rectangular cross-section as viewed in plan view.
- the body segments 11 as shown in FIG. 3 are arranged in a plane next to each other in several rows 14 and columns 15 , whereby the weld joints between the body segments 11 form a network-like structure of intersecting longitudinal and transverse weld seams 12 , 13 .
- the body segments 21 shown in FIG. 4 are arranged in a plane next to each other in several rows 24 that are offset with respect to each other, whereby the weld joints form a structure that has the appearance of a brick wall with uninterrupted transverse weld seams 23 and longitudinal weld seams 22 that are offset with respect to each other.
- the plastic sheets 30 , 40 shown in FIGS. 5 and 6 contain body segments 31 , 41 of quadratic cross-section as viewing the sheet in plan view.
- the body segments 31 shown in FIG. 5 are arranged next to each other in a plane in several rows 34 and columns 35 , whereby the weld joins form a network-like structure with intersecting longitudinal and transverse weld seams 32 , 33 .
- the body segments 41 shown in FIG. 6 are arranged in a plane next to each other in offset rows 44 , whereby the weld joins form uninterrupted transverse weld seams 43 and longitudinal weld seams 42 that are offset with respect to each other.
- FIG. 7 shows a further version of a plastic sheet 50 having—as viewed in plan view—hexagonal i.e. web-shaped body segments 51 which are arranged on a plane next to each other and are welded together forming weld seams 52 .
- FIG. 8 shows another version of a plastic sheet 60 according to the invention having—as viewed in plan view—triangular body segments 61 which are arranged on a plane next to each other and are welded together forming weld seams 62 .
- FIG. 9 shows a plastic block 5 made up of column-shaped or rod-shaped foam bodies 7 , whereby the foam bodies 7 are manufactured e.g. by means of extrusion or by dividing a homogeneous block of foam.
- the individual foam bodies 7 are, according to the invention, joined together along their long sides 8 by plastic welding, forming longitudinal and transverse weld seams 32 , 33 respectively.
- plastic block 5 By sawing or thermally cutting the plastic block 5 is divided into individual plastic sheets 30 according to the invention as shown in FIG. 5 , whereby the plastic sheets 30 are made up of body segments 31 that are arranged next to each other on a plane.
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Abstract
An unmixed plastic sheet, which is made of a thermoplastic material and which is composed of a number of body segments that are adjacent to one another in a plane, interconnected and made of a closed-cell foam material. The body segments are thermoplastically welded to one another at their abutting lateral faces while forming flat weld seams. The flat weld seams form a plastic intermediate layer, which has few pores, and which is provided in the form of a web structure that, when viewed from above, is reticular and reinforces the plastic sheet. The inventive plastic sheet is preferably used as a core layer in sandwich composites.
Description
- The invention relates to a large area structural element containing a plurality of body segments arranged adjacent to one another in a plane, interconnected and made of a closed-cell foamed plastic, and a process for manufacturing such a large area structural element and the use thereof.
- It is known to employ a foamed thermoplastic as the core layer in sandwich-type composites. The production of foamed plastic panels may be achieved e.g. by an extrusion process. The structural load-bearing capacity, in particular the compressive strength of such core layers made using extrusion processes is however limited. For demanding applications, therefore, sandwich composites with the above mentioned core layers are often not suitable as structural components.
- However, for demanding applications such as e.g. structural components in transportation it is necessary to have sandwich composites that exhibit a high degree of strength, in particular compressive strength and stiffness, and core materials that exhibit high shear strength and stiffness. In order to achieve these properties, use is made e.g. of stronger and much thicker outer layers. As a rule this leads to an undesirable increase in the specific weight of the sandwich composites. Further, the compressive strength of such sandwich composites can not be increased in an unlimited manner by use of thicker outer layers.
- It is therefore desirable not only for the outer layers but also the core layers to exhibit greater compressive and shear strength, however, without having to forego the advantage of smaller thickness of foamed bodies.
- This would enable sandwich composites with improved strength and stiffness characteristics to be achieved without significant increase in the specific weight. On the other hand, the use of core layers with increased stiffness and strength would also permit the use of thinner outer layers.
- Sandwich composites are therefore known that exhibit improved strength by use of specific design of the core layer.
- Described in DE 197 15 529 C1 for example is the production of a sandwich composite with a core layer and outer layers on both sides thereof, whereby the core layer is made up of horizontally abutting polygonals e.g. cube-shaped foam segments. In that case the individual foam segments are covered over with a fibre layer and fitted together in a device such that the sides of the segments are in contact with the fibre layer in a strut-Ike manner. The strut-like fibre layers are soaked with an impregnating medium. By hardening the impregnating medium fibre-composite layers are produced between the foam segments, thus providing a stiffening and strengthening effect on the core layer.
- The described manufacturing process is, however, found to be very complicated and costly. Further, a core layer produced in accordance with the described process is of a mixed type as the foam segments, fibre layers and impregnating medium result in at least three different materials being used.
- The document U.S. Pat. No. 4,837,060 describes a composite element with a core layer of mutually adhesively bonded or sealed cylindrical shaped foam elements with outer layers provided on both sides of the core layer. The axes of the cylinders of the foam elements run parallel to the planes of the outer surface layers.
- The document U.S. Pat. No. 4,536,427 describes a composite element with a core layer of mutually adhesively bonded balsa wood elements. The adhesive bond is flexible and elastic in design with the result that the core layer is able to bend.
- The object of the present invention is to propose a large area, in particular sheet-like structural element which is suitable for core layers in sandwich-type composites, whereby the structural element should contain a foam with a closed-cell structure. A further object is a cost favourable process for manu-facturing the mentioned large area structural element. The large area structural element should in particular exhibit improved compressive strength in com-parison with conventional foam panels. The large area structural element should also be as unmixed in character as possible.
- That objective is achieved by way of the invention in that the structural element is made wholly of plastic, and the body segments are welded together at their abutting lateral faces forming flat weld seams, whereby the flat weld seams form a plastic intermediate layer which has few pores or is pore-free and which is provided in the form of a web structure that, when viewed from above, is reticular and reinforces the plastic sheet.
- The large area structural element is preferably sheet-shaped. The large area structural element is preferably in the form of a sheet-type element, in particular a block-shaped sheet element.
- The large area structural element comprises a thermoplastic, preferably a poly-styrene (PS), acrylnitrile/butadiene/styrene-grafted coploymer (ABS). poly-ethylene (PE), polypropylene (PP), polyvinylchloride (PVC), polycarbonate (PC) and in particular polyethylene-terephthalate (PET), poly-phenylene-ether (PPE) or poly-blends thereof such as poly(phenylene-ether)-polystyrene (PPE-FPS), or a styrene/acrylnitrile copolymer (SAN).
- The structural element according to the invention is preferably unmixed i.e. it is comprised of only one single plastic. The unmixed character requires in particular that the structural element contains no other kind of adhesive for joining the body segments together.
- The specific weight of a structural element according to the invention is e.g. more than 20 kg/m3, preferably more than 40 kg/m3, in particular more than 50 kg/m3 and e.g. less than 200 kg/m3, preferably less than 130 kg/m3. The pore size of the foam is e.g. in the range 100 to 1000 μm.
- The weld seams are preferably formed by plastic of the body segment which is melted then solidified after fitting the segments together. To that end the body segments exhibit, in particular at the abutting sides, zones in the form of areas that melt and re-solidify.
- The thickness of the weld seams or melt zones is chosen such that the network-like strut structure of the weld seams increases the compressive strength of structural element with respect to area pressure. This means that the weld seams represent not only joins between two body segments, but at the same time stiffening or reinforcing struts of foam between the body segments. The weld seams also effect stiffening of the structural element with respect to shear and bending stresses. The expression of strength or thickness of the weld seams refers therefore not only to a stable weld seam but also to effective stiffening or reinforcing of the structure.
- The thickness of the melt/re-solidified zone at the side wall faces that constitute the weld seams is selected therefore such that the structural element exhibits in particular high compressive strength with respect to surface pressure.
- The body segments are preferably fitted and welded together in a continuous manner i.e. free of voids. The body segments therefore preferably exhibit a cross-sectional shape that enables the segments to be fitted together in rows without gaps.
- In a preferred version of the invention the body segments exhibit—in a plan view of the structural element—a poloygonal shape, in particular an eight, six, four or three sided shape. The body segments may in plan view of the structural element exhibit e.g. a quadratic, rectangular, hexagonal or triangular outline which runs around the so called top faces of the body segments.
- The size of the body segments may vary according to the degree of stiffness or compressive strength desired.
- As each of the above mentioned geometries and sizes of body segments results in large area structural elements with different properties, the geometry and size of the body segments are determined primarily by the specific require-ments placed on the structural element.
- The body segments are especially preferably in the form of cubes or blocks. Body segments of block or cube shape may e.g. be arranged in several rows and columns, whereby the weld joints form a network-type structure with intersecting longitudinal and transverse weld seams. The said body segments may also be arranged in several rows that are offset with respect to each other, whereby the weld joints form continuous transverse weld seams and offset longitudinal weld seams creating a pattern like a brick wall.
- Quadratic shaped body segments may e.g. (as viewing the structural element in plan view) exhibit a quadratic or rectangular shaped outline with side lengths (x, y) of 20 to 600 mm, preferably 30 to 400 mm, in particular 40 to 100 mm (see also
FIG. 1 ). A rectangular body segment may e.g. (as viewing the structural element in plan view) exhibit a length of 100 to 250 mm and a breadth of 30 to 50 mm. - The body segments may—viewing the structural element in plan view—also exhibit a curved outline shape e.g. concave or convex in whole or in part. The body segments may also be shaped in a manner of interlocking bricks i.e. the body segments are shaped such that the individual body segments lock into each other. The body segments of the structural element according to the invention are also preferably congruent with respect to each other.
- In sheet-shaped structural elements the side faces of the body segments are also preferably perpendicular to the outer faces of the structural element.
- The invention also relates to a process for manufacturing a large area structural element containing a plurality of body elements of a foamed plastic that are aligned next to each other in a plane and joined together.
- The process is characterised by way of the following steps:
- a) manufacture of closed-cell rod-shaped or column-shaped foamed plastic bodies;
- b) welding together the long sides of the rod-shaped or column-shaped foamed bodies into a plastic block thus creating weld seams over that face, whereby the weld seams are then present as low-pore or pore-free intermediate plastic layers;
- c) dividing the block of foamed plastic into individual large area structural elements, in particular foam sheets, running transverse or perpendicular to the longitudinal direction of the rod-shaped foam bodies,
whereby the weld seams, as viewed in plan view of the structural element, form a network like structure of struts. - The rod-shaped or column-shaped foam bodies are preferably manufactured using an extrusion process. The orientation of the material of the foam bodies or body segments preferably is preferably stretched in the direction of extrusion. Thereby, in particular polymer chains exhibit stretching in the direction of extrusion as a result of the extrusion process. The stretching of the material effects an improvement in the mechanical properties, in particular the compressive strength in the direction of stretching.
- The foam bodies or body segments also preferably exhibit a cell structure or cell arrangement that is oriented in the direction of extrusion. The oriented cell structures of the foam body contribute to an increase in the compressive strength of the structural element.
- In another version of the invention the rod-shaped or column-shaped foam bodies may be taken from a prefabricated block of foam i.e. by cutting or sawing. The said block of foam is manufactured by means of an extrusion process.
- According to a specific version of the invention the production of the foam bodies takes place via an extrusion process, whereby the foam body comprises a plurality of expanded polymer strands that are brought together. Drawing the strands together takes place immediately after leaving the extrusion die by expanding the individual strands. Thereby, neighbouring strands make contact with each other, grow together or stick together forming a foam body. The foam body is then in the form of a closed package of strands.
- The strands lie preferably essentially parallel to each other and are arranged in the longitudinal or extrusion direction of the foam body. The manufacturing pro-cess may be arranged such that the individual strands remain visible in the foam body or are brought together or melted to give one single structure in which the individual strands are only slightly or no longer detectable. The strands are preferably packed together so tightly that the individual strands come to rest fully in contact with each other without forming any spaces. The strands may, however, also be arranged or packed together such that channel-like spaces are formed between the individual strands.
- The strands are usefully created via an extrusion tool e.g. die plate, whereby the extrusion tool contains a plurality of neighbouring openings through which the polymer is extruded in the form of strands. In cross-section the said openings may be round e.g. circular or elliptical shaped, or polygonal e.g. rectangular, quadratic or hexagonal. The openings may also be in the form of slits. The foamed strands may have a diameter of e.g. 3 to 50 mm, in particular 4 to 20 mm.
- Situated downstream of the extrusion die there may also be another shaping tool that specifies the outer contour of the foam body, in which tool the strands are packed together on emerging from the extrusion die, so that the foam body takes on the cross-sectional shape of the shaping tool.
- With the above manufacturing process it is possible to produce rod-shaped or column-shaped foam bodies which have already been extruded with the desired cross-sectional shape and size so that the foam bodies can be cut to length individually or already in combination with further rod-shaped or column-shaped foam bodies into body segments or contain large area structural elements containing body segments.
- Further, using the above manufacturing process it is possible to produce foam bodies of a cross-sectional size which is larger the required cross-section of rod-shaped or column-shaped foam bodies, so that in the subsequent process-ing steps the extruded foam body is cut into individual rod-shaped or column-shaped foam bodies, whereby the strands run essentially in the longitudinal direction of the cut rod-shaped or column-shaped foam bodies.
- In a preferred version of the foam bodies or body segments manufactured according to the above described process the orientation of the individual strands of the body segments lies essentially perpendicular to the outer faces of the large area structural element made up of body segments. Thereby, as a result of the orientation of the strands, the compressive strength is preferably greater in the longitudinal direction of the strands i.e. in the direction of extrusion than in the other directions.
- The foam bodies may be produced using physical or chemical foaming means. In a preferred version the foam bodies are foamed physically using CO2. The introduction of the foaming agent may take place directly in the extrusion device.
- In a preferred version of the invention the extruded foam bodies are welded into plastic blocks on their long sides i.e. along the long sides that come into contact with each other. Large area, in particular sheet-shaped structural elements are subsequently cut from these plastic blocks transverse or perpendicular to the long sides of the foam bodies.
- The cutting of the large area structural elements out of the plastic blocks may be performed by sawing or using a thermal cutting process.
- Instead of the above described process steps the foam bodies may also be already cut into body segments whereby the individual body segments are subsequently welded together to form large area structural elements.
- The welding takes place preferably by melting the side faces of the body segments that are to be joined, followed by fitting these together and solidifying the molten zones.
- In a preferred version means for controlling the melting process during welding are employed that allow weld seams of a specific thickness or thickness range to be produced, whereby the thickness range is selected such that the web-like strut structure of weld seams produces a stiffening effect on the plastic sheet.
- The welding process is usefully one of thermoplastic welding. The production of the weld joint may take place by means of radiation welding or contact welding. Plastic welding processes that can be employed are e.g. welding with heating elements or infrared welding. The welding process may take place with or without weld-feed materials.
- Compared to conventional foamed plastic sheets, the large area structural elements according to the invention exhibit greater stiffness and in particular greater compressive strength. The properties are due essentially to the weld seams between the individual body segments. The weld seams form a network of strut-like connections like a framework, whereby the weld seams are in the form of low-pore or pore-free, dense intermediate plastic layers.
- The framework of strut-like connected weld seams increases the compressive strength as the struts forming the intermediate plastic layer are significantly less compressible than the foam body itself. If, for example, surface pressure is applied to the structural element according to the invention (e.g. in the case of a sandwich composite via the outer layers onto the structural element serving as core layer), then the compressive forces act mainly on the stiff strut-like structure and not on the foam bodies themselves.
- The increase in stiffness of the structural element according to the invention is also a result of the framework-like nature of the weld seams which lead to an increase in the torsional and bend strength of the structural element.
- The structural element according to the invention finds application preferably in composite elements, in particular composite sheets with at least one outer sheet on one side of the structural element.
- The structural element according to the invention finds highly preferable application as core in sandwich composite elements, in particular sandwich composite elements with outer layers on both sides of the core layer. The sandwich composite elements may e.g. comprise a large area structural element according to the invention with an outer layer on both sides of the structural element. Further, it is also possible for there to be several layers on one or both sides of the structural element. If the structural element according to the invention is employed as a core layer in a sandwich composite sheet, the structural element is usefully a sheet element.
- The said layers or outer layers may be joined to each other and/or to the core layer e.g. by adhesive joining means.
- The outer layers may e.g. be rigid or flexible sheets of plastic or fibre reinforced plastic such as glass fibre reinforced plastic. Further, the outer layers may also be sheets of metal, in particular aluminium or an aluminium alloy. The outer layers are, in comparison with the core layer, usefully relatively thin sheets.
- In spite of their low weight, sandwich composite elements with structural elements according to the invention exhibit a high degree of stiffness and excellent shear and compressive strength. Such sandwich structures are therefore suitable especially for applications which require components which are light in eight but structurally high load bearing.
- Sandwich-type composite elements with structural elements according to the invention as core layer may e.g. be employed as construction elements in the building industry.
- Examples of such construction elements are walls, floors, ceilings, doors, dividing walls or cladding elements.
- Sandwich composite elements with structural elements according to the invention as core layer also find preferred application in transportation on land (e.g. road or railway vehicle manufacture), on water (e.g. ship and boat building, equipment for water sports) or in the air (e.g. aircraft construction). This may be e.g. sandwich composite elements according to the invention for trunk structures, loading platforms, walls, ceilings, floors, lids, cladding or parts thereof, on or as part of lorries or railway trucks for goods transport, or walls, ceilings, floors, intermediate walls, cladding elements, doors, lids or parts hereof, on vehicles for public transport such as omnibusses, trams, railway carriages or on ships such as passenger ships, ferries, pleasure steamers or boots.
- The sandwich composite elements according to the invention may also find application in sports articles for use on land, water or air.
- Sandwich composite elements with structural elements as core layer according to the invention are highly preferred for application as vanes or rotor-blades for wind powered generating units.
- The invention is described in greater detail in the following by way of example and with reference to the accompanying drawings. These show in:
-
FIG. 1 : an explosive view of a sandwich composite with a structural element according to the invention as core layer; -
FIG. 2 : a cross-section through a sandwich composite with a structural element according to the invention as core layer; -
FIG. 3 : plan view of a first version of structural element according to the invention; -
FIG. 4 : plan view of a second version of structural element according to the invention; -
FIG. 5 : plan view of a third version of structural element according to the invention; -
FIG. 6 : plan view of a fourth version of structural element according to the invention; -
FIG. 7 : plan view of a fifth version of structural element according to the invention; -
FIG. 8 : plan view of a sixth version of structural element according to the invention; -
FIG. 9 : perspective view of a plastic block for manufacturing structural elements according to the invention as shown inFIG. 5 . -
FIG. 1 shows a sandwich composite element 1 with a core layer of structural element according to the invention, which is in the form of a plastic sheet 10 (see alsoFIG. 3 ). Theplastic sheet 10 is made up of block-shapedbody segments 11 which are joined together at their touching side faces 17 via longitudinal and transverse weld seams 12, 13 that extend over the said side faces 17. The weld seams 12, 13 form thereby (as seen in plan view) a network-like, stiff structure of struts. Provided on each side of the core layer on the outer faces 16 of thebody segments 11 is anouter layer outer layers -
FIG. 2 shows a cross-sectional view of a sandwich composite element 1 as inFIG. 1 . Theouter layers -
FIGS. 3 to 7 show various versions of structural elements according to the invention in the form ofplastic sheets body segments - The
plastic sheets FIGS. 3 and 4 containbody segments body segments 11 as shown inFIG. 3 are arranged in a plane next to each other inseveral rows 14 andcolumns 15, whereby the weld joints between thebody segments 11 form a network-like structure of intersecting longitudinal and transverse weld seams 12, 13. - The
body segments 21 shown inFIG. 4 are arranged in a plane next to each other inseveral rows 24 that are offset with respect to each other, whereby the weld joints form a structure that has the appearance of a brick wall with uninterrupted transverse weld seams 23 and longitudinal weld seams 22 that are offset with respect to each other. - The
plastic sheets FIGS. 5 and 6 containbody segments body segments 31 shown inFIG. 5 are arranged next to each other in a plane inseveral rows 34 andcolumns 35, whereby the weld joins form a network-like structure with intersecting longitudinal and transverse weld seams 32, 33. - The
body segments 41 shown inFIG. 6 are arranged in a plane next to each other in offsetrows 44, whereby the weld joins form uninterrupted transverse weld seams 43 and longitudinal weld seams 42 that are offset with respect to each other. -
FIG. 7 shows a further version of aplastic sheet 50 having—as viewed in plan view—hexagonal i.e. web-shapedbody segments 51 which are arranged on a plane next to each other and are welded together forming weld seams 52. -
FIG. 8 shows another version of aplastic sheet 60 according to the invention having—as viewed in plan view—triangular body segments 61 which are arranged on a plane next to each other and are welded together forming weld seams 62. -
FIG. 9 shows aplastic block 5 made up of column-shaped or rod-shapedfoam bodies 7, whereby thefoam bodies 7 are manufactured e.g. by means of extrusion or by dividing a homogeneous block of foam. Theindividual foam bodies 7 are, according to the invention, joined together along their long sides 8 by plastic welding, forming longitudinal and transverse weld seams 32, 33 respectively. - By sawing or thermally cutting the
plastic block 5 is divided intoindividual plastic sheets 30 according to the invention as shown inFIG. 5 , whereby theplastic sheets 30 are made up ofbody segments 31 that are arranged next to each other on a plane.
Claims (12)
1-20. (canceled)
21. A structural element, comprising: a block which comprises a plurality of body segments of a foamed, thermoplastic material having a stretched polymer structure in one direction, the body segments being arranged next to each other and joined together on a plane defining foam sheets running transverse or perpendicular to the one direction of the stretched polymer structure, wherein the structural element is a plastic sheet having opposed relatively large area sides, and relatively small area edges, and where the stretched polymer structure is in a direction perpendicular to the relatively large area sides, wherein the structural element is made wholly of plastic and the body segments are welded together at abutting side faces forming weld seams, whereby the weld seams form a substantially pore-free intermediate plastic layer in the form of a network of stiffening struts defined by intersecting weld seams, wherein each of the weld seams have a thickness such that a network strut structure is formed by the weld seams which increases the compressive strength of the structural element with respect to surface pressure wherein the structural element has a specific weight less than 130 kg/m3.
22. The structural element of claim 21 , wherein the specific weight is between 20 kg/m3 and 130 kg/m3.
23. The structural element of claim 21 , wherein the body segments are made of a closed-cell foam material.
24. The structural element of claim 21 , wherein the thermoplastic material is polyethylene-terephthalate (PET) or styrene/acrylnitrile-copolymer (SAN).
25. The structural element of claim 21 , wherein the weld seams comprises melted plastic of the body segments.
26. The structural element of claim 21 , wherein the body segments are formed from lengths cut from rod-shaped or column-shaped foam bodies.
27. The structural element of claim 26 , wherein the rod-shaped or column-shaped foam bodies are formed by means of extrusion, and the direction of extrusion in the body segments manufactured from the foam bodies lies substantially parallel to a line of intersection of two intersecting weld seams.
28. The structural element of claim 21 , wherein the body segments have a polygonal shape.
29. The structural element of claim 21 , wherein the structural element (10) is a plastic sheet.
30. The structural element of claim 21 , wherein the weld seams form a structure with uninterrupted transverse weld seams and longitudinal weld seams that are offset with respect to each other.
31. The structural element of claim 21 , wherein the body segments are arranged on a plane next to each other and are welded together forming the weld seams.
Priority Applications (1)
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US12/947,190 US20110091715A1 (en) | 2002-08-29 | 2010-11-16 | Foamed plastic sheet |
Applications Claiming Priority (6)
Application Number | Priority Date | Filing Date | Title |
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EP20020405739 EP1393892A1 (en) | 2002-08-29 | 2002-08-29 | Foamed plastic plate |
US10/524,987 US20060257612A1 (en) | 2002-08-29 | 2003-08-16 | Foamed plastic sheet |
PCT/EP2003/009090 WO2004024434A1 (en) | 2002-08-29 | 2003-08-16 | Foamed plastic sheet |
US12/757,376 US7857596B2 (en) | 2002-08-29 | 2010-04-09 | Vane or rotor blade |
US12/947,190 US20110091715A1 (en) | 2002-08-29 | 2010-11-16 | Foamed plastic sheet |
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US12/757,376 Continuation US7857596B2 (en) | 2002-08-29 | 2010-04-09 | Vane or rotor blade |
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US20110091715A1 true US20110091715A1 (en) | 2011-04-21 |
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US11/971,930 Expired - Lifetime US7988805B2 (en) | 2002-08-29 | 2008-01-10 | Foamed plastic sheet |
US12/757,376 Expired - Lifetime US7857596B2 (en) | 2002-08-29 | 2010-04-09 | Vane or rotor blade |
US12/947,190 Abandoned US20110091715A1 (en) | 2002-08-29 | 2010-11-16 | Foamed plastic sheet |
US13/196,242 Abandoned US20110287248A1 (en) | 2002-08-29 | 2011-08-02 | Foamed plastic sheet |
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US12/757,376 Expired - Lifetime US7857596B2 (en) | 2002-08-29 | 2010-04-09 | Vane or rotor blade |
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US13/196,242 Abandoned US20110287248A1 (en) | 2002-08-29 | 2011-08-02 | Foamed plastic sheet |
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EP (2) | EP1393892A1 (en) |
AT (1) | ATE330787T1 (en) |
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CA (1) | CA2496492C (en) |
CY (1) | CY1107471T1 (en) |
DE (1) | DE50303984D1 (en) |
DK (1) | DK1536944T4 (en) |
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US10183464B2 (en) | 2014-09-18 | 2019-01-22 | Basf Se | Composite article |
WO2016041836A1 (en) * | 2014-09-18 | 2016-03-24 | Basf Se | New composite article |
US10556732B2 (en) | 2015-03-03 | 2020-02-11 | Selig Sealing Products, Inc. | Tabbed seal concepts |
US11059644B2 (en) | 2015-03-03 | 2021-07-13 | Selig Sealing Products, Inc. | Tabbed seal concepts |
US10899506B2 (en) | 2016-10-28 | 2021-01-26 | Selig Sealing Products, Inc. | Single aluminum tamper indicating tabbed sealing member |
US10934069B2 (en) | 2016-10-28 | 2021-03-02 | Selig Sealing Products, Inc. | Sealing member for use with fat containing compositions |
US11401080B2 (en) | 2016-10-28 | 2022-08-02 | Selig Sealing Products, Inc. | Single aluminum tamper indicating tabbed sealing member |
US11866242B2 (en) | 2016-10-31 | 2024-01-09 | Selig Sealing Products, Inc. | Tabbed inner seal |
US11708198B2 (en) | 2018-07-09 | 2023-07-25 | Selig Sealing Products, Inc. | Grip enhancements for tabbed seal |
US11724863B2 (en) | 2018-07-09 | 2023-08-15 | Selig Sealing Products, Inc. | Tabbed seal with oversized tab |
US11254481B2 (en) | 2018-09-11 | 2022-02-22 | Selig Sealing Products, Inc. | Enhancements for tabbed seal |
EP3944944B1 (en) | 2020-07-29 | 2024-04-24 | Airex AG | Contoured structural element and manufacture of the contoured structural element |
Also Published As
Publication number | Publication date |
---|---|
PT1536944E (en) | 2006-11-30 |
DE50303984D1 (en) | 2006-08-03 |
SI1536944T2 (en) | 2012-03-31 |
ES2265599T3 (en) | 2007-02-16 |
US20110287248A1 (en) | 2011-11-24 |
US20100254819A1 (en) | 2010-10-07 |
DK1536944T3 (en) | 2006-10-23 |
EP1393892A1 (en) | 2004-03-03 |
US20060257612A1 (en) | 2006-11-16 |
EP1536944A1 (en) | 2005-06-08 |
ES2265599T5 (en) | 2012-02-15 |
US20080105991A1 (en) | 2008-05-08 |
US7857596B2 (en) | 2010-12-28 |
EP1536944B2 (en) | 2011-10-05 |
DK1536944T4 (en) | 2012-01-30 |
CA2496492C (en) | 2009-10-27 |
CY1107471T1 (en) | 2013-03-13 |
EP1536944B1 (en) | 2006-06-21 |
WO2004024434A1 (en) | 2004-03-25 |
CA2496492A1 (en) | 2004-03-25 |
SI1536944T1 (en) | 2006-12-31 |
US7988805B2 (en) | 2011-08-02 |
ATE330787T1 (en) | 2006-07-15 |
AU2003258619A1 (en) | 2004-04-30 |
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STCB | Information on status: application discontinuation |
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