DE10132196B4 - A method of making a product having a perforated thermoplastic structure and perforating means for carrying out the method - Google Patents
A method of making a product having a perforated thermoplastic structure and perforating means for carrying out the method Download PDFInfo
- Publication number
- DE10132196B4 DE10132196B4 DE10132196A DE10132196A DE10132196B4 DE 10132196 B4 DE10132196 B4 DE 10132196B4 DE 10132196 A DE10132196 A DE 10132196A DE 10132196 A DE10132196 A DE 10132196A DE 10132196 B4 DE10132196 B4 DE 10132196B4
- Authority
- DE
- Germany
- Prior art keywords
- layer
- roller
- perforating
- perforated
- thermoplastic
- 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.)
- Expired - Fee Related
Links
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
- B32B7/00—Layered products characterised by the relation between layers; Layered products characterised by the relative orientation of features between layers, or by the relative values of a measurable parameter between layers, i.e. products comprising layers having different physical, chemical or physicochemical properties; Layered products characterised by the interconnection of layers
- B32B7/02—Physical, chemical or physicochemical properties
- B32B7/027—Thermal properties
-
- 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
- B32B27/08—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 synthetic resin
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B26—HAND CUTTING TOOLS; CUTTING; SEVERING
- B26F—PERFORATING; PUNCHING; CUTTING-OUT; STAMPING-OUT; SEVERING BY MEANS OTHER THAN CUTTING
- B26F1/00—Perforating; Punching; Cutting-out; Stamping-out; Apparatus therefor
- B26F1/24—Perforating by needles or pins
-
- 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
- B29C65/10—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using hot gases (e.g. combustion gases) or flames coming in contact with at least one of the 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
- 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
-
- 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
- B29C65/74—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area
- B29C65/743—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc
- B29C65/7435—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc the tool being a roller
-
- 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
- B29C65/74—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area
- B29C65/743—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc
- B29C65/7437—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc the tool being a perforating tool
-
- 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
- B29C65/78—Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus
- B29C65/7858—Means for handling the parts to be joined, e.g. for making containers or hollow articles, e.g. means for handling sheets, plates, web-like materials, tubular articles, hollow articles or elements to be joined therewith; Means for discharging the joined articles from the joining apparatus characterised by the feeding movement of the parts to be joined
- B29C65/7888—Means for handling of moving sheets or webs
- B29C65/7894—Means for handling of moving sheets or webs of continuously moving sheets or webs
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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
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/10—Particular design of joint configurations particular design of the joint cross-sections
- B29C66/11—Joint cross-sections comprising a single joint-segment, i.e. one of the parts to be joined comprising a single joint-segment in the joint cross-section
- B29C66/112—Single lapped joints
- B29C66/1122—Single lap to lap joints, i.e. overlap joints
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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
- B29C66/01—General aspects dealing with the joint area or with the area to be joined
- B29C66/05—Particular design of joint configurations
- B29C66/20—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
- B29C66/21—Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
- B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/40—General aspects of joining substantially flat articles, e.g. plates, sheets or web-like materials; Making flat seams in tubular or hollow articles; Joining single elements to substantially flat surfaces
- B29C66/41—Joining substantially flat articles ; Making flat seams in tubular or hollow articles
- B29C66/45—Joining of substantially the whole surface of the articles
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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
- B29C66/731—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 intensive physical properties of the material of the parts to be joined
- B29C66/7311—Thermal properties
- B29C66/73115—Melting point
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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
- B29C66/731—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 intensive physical properties of the material of the parts to be joined
- B29C66/7311—Thermal properties
- B29C66/73115—Melting point
- B29C66/73116—Melting point of different melting point, i.e. the melting point of one of the parts to be joined being different from the melting point of the other part
-
- 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
- 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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/81—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
- B29C66/814—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
- B29C66/8141—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined
- B29C66/81433—General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined being toothed, i.e. comprising several teeth or pins, or being patterned
-
- 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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/834—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools moving with the parts to be joined
- B29C66/8341—Roller, cylinder or drum types; Band or belt types; Ball types
- B29C66/83411—Roller, cylinder or drum types
- B29C66/83415—Roller, cylinder or drum types the contact angle between said rollers, cylinders or drums and said parts to be joined being a non-zero angle
-
- 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
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/834—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools moving with the parts to be joined
- B29C66/8351—Jaws mounted on rollers, cylinders, drums, bands, belts or chains; Flying jaws
- B29C66/83511—Jaws mounted on rollers, cylinders, drums, bands, belts or chains; Flying jaws jaws mounted on rollers, cylinders or drums
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/00—General aspects of processes or apparatus for joining preformed parts
- B29C66/80—General aspects of machine operations or constructions and parts thereof
- B29C66/83—General aspects of machine operations or constructions and parts thereof characterised by the movement of the joining or pressing tools
- B29C66/836—Moving relative to and tangentially to the parts to be joined, e.g. transversely to the displacement of the parts to be joined, e.g. using a X-Y table
-
- 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
- B32B27/12—Layered products comprising a layer of synthetic resin next to a fibrous or filamentary layer
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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
- B32B3/26—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 particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer
- B32B3/266—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 particular shape of the outline of the cross-section of a continuous layer; characterised by a layer with cavities or internal voids ; characterised by an apertured layer characterised by an apertured layer, the apertures going through the whole thickness of the layer, e.g. expanded metal, perforated layer, slit layer regular cells B32B3/12
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- B32—LAYERED PRODUCTS
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- 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
- B32B5/022—Non-woven fabric
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- 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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- 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
- B29C66/729—Textile or other fibrous material made from plastics
- B29C66/7294—Non woven mats, e.g. felt
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- B—PERFORMING OPERATIONS; TRANSPORTING
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- B29L—INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES
- B29L2009/00—Layered products
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- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/04—Punching, slitting or perforating
- B32B2038/047—Perforating
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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
- B32B2398/00—Unspecified macromolecular compounds
- B32B2398/20—Thermoplastics
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- B32B38/00—Ancillary operations in connection with laminating processes
- B32B38/0036—Heat treatment
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Forests & Forestry (AREA)
- Textile Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Nonwoven Fabrics (AREA)
- Laminated Bodies (AREA)
- Paper (AREA)
Abstract
Verfahren zur Herstellung eines Produktes mit einer perforierten thermoplastischen Struktur (7), welches zumindest eine erste (8) und eine zweite Lage (9) aufweist, wobei ein thermoplastisches Material der ersten Lage (8) einen niedrigeren Schmelzpunkt aufweist als ein thermoplastisches Material der zweiten Lage (9), wobei die erste (8) und die zweite Lage (9) zusammen über eine Zuführung einer beheizten Perforierungseinrichtung (1) mit einem Perforierkalander (6) über einen Umschlingungswinkel von über 180°, vorzugsweise zwischen 190° und 220°, entlang der Gegenwalze (3) zugeführt werden, wobei im Perforierkalander (6) Erhebungen (5) von einer Perforierungswalze (2) die erste (8) und die zweite Lage (9) durchdringen und teilweise in die Gegenwalze (3) eingreifen, wobei die zweite Lage (9) vor der ersten Lage (8) mit den Erhebungen (5) in Kontakt kommt und dass im Bereich der Perforationen die zweite Lage (9) ungeschmolzen bleibt, und eine Innenfläche (20) einer kegelförmigen oder zylinderförmigen Gestalt (18) bildet, während die erste Lage...method for producing a product with a perforated thermoplastic Structure (7) comprising at least a first (8) and a second layer (9) wherein a thermoplastic material of the first layer (8) has a lower melting point than a thermoplastic Material of the second layer (9), wherein the first (8) and the second Location (9) together over a feeder a heated perforating device (1) with a perforating calender (6) about a wrap angle of about 180 °, preferably between 190 ° and 220 °, along fed to the counter-roller (3) are in the Perforierkalander (6) surveys (5) of a Perforation roller (2) penetrate the first (8) and the second layer (9) and partially engage the counter roll (3), wherein the second Position (9) in front of the first layer (8) with the elevations (5) in contact comes and that in the area of the perforations the second layer (9) remains unmelted, and an inner surface (20) of a conical or cylindrical Form (18) forms while the first location ...
Description
Die vorliegende Erfindung betrifft ein Verfahren und eine Vorrichtung zur Herstellung eines Produktes mit einer perforierten thermoplastischen Struktur.The The present invention relates to a method and an apparatus for producing a product with a perforated thermoplastic Structure.
Ein
perforiertes Material geht beispielsweise aus der
In
Aus
Die vorliegende Erfindung hat nun zur Aufgabe, ein Verfahren zur Herstellung eines Produktes mit einer perforierten thermoplastischen Struktur mit einer dreidimensionalen Gestalt zu schaffen, die über eine gewisse Druckunempfindlichkeit in Bezug auf ihre Gestalt verfügt.The It is an object of the present invention to provide a process for the production a product with a perforated thermoplastic structure to create with a three-dimensional shape that over one has certain pressure insensitivity with regard to its shape.
Diese Aufgabe wird mit einem Verfahren zur Herstellung eines perforierten Laminates mit den Merkmalen des Anspruches 1 und einer Perforierungsvorrichtung mit den Merkmalen des Anspruchs 5 gelöst. Vorteilhafte Weiterbildungen sind in den jeweiligen Unteransprüchen angegeben, wobei weitere Ausgestaltungen in der nachfolgenden Beschreibung beschrieben sind.These Task is using a method of making a perforated Laminates with the features of claim 1 and a perforating device solved with the features of claim 5. Advantageous developments are given in the respective subclaims, wherein more Embodiments are described in the following description.
Die Erfindung weist ein Verfahren zur Herstellung eines Produktes mit einer perforierten thermoplastischen Struktur mit zumindest einer ersten Lage und mit einer Vielzahl von Perforationen auf. Die Perforationen erstrecken sich durch die erste Lage, wobei die Perforationen eine dreidimensionale, etwa kegelförmige oder zylinderförmige Gestalt aufweisen. Mit der ersten Lage ist zumindest eine zweite Lage zumindest teilweise verbunden. Die Perforationen erstrecken sich auch durch die zweite Lage. Die zweite Lage bildet eine Innenfläche der Gestalt, während die erste Lage eine Außenfläche der Gestalt bildet. Die erste Lage weist weiterhin ein thermoplastisches Material auf, dessen Schmelzpunkt niedriger ist als der Schmelzpunkt des thermoplastischen Materials der zweiten Lage.The The invention has a method for producing a product a perforated thermoplastic structure having at least one first location and with a variety of perforations on. The perforations extend through the first layer, the perforations being a three-dimensional, about conical or cylindrical Have shape. With the first layer is at least a second Location at least partially connected. The perforations extend also through the second location. The second layer forms an inner surface of the Shape, while the first layer has an outer surface of Form forms. The first layer also has a thermoplastic Material whose melting point is lower than the melting point the thermoplastic material of the second layer.
Die erste Lage ist zumindest teilweise im Bereich der Perforationen geschmolzen und stabilisiert dadurch die Gestalt, während die zweite Lage im Bereich der Perforierung ungeschmolzen ist.The first position is at least partially in the area of the perforations thereby melted and stabilized the shape, while the second layer in the perforation is unmelted.
Die Auswahl unterschiedlicher Schmelzpunkte von unterschiedlichen thermoplastischen Materialien erlaubt, den jeweiligen Lagen unterschiedliche Eigenschaften zuzuweisen. Vorzugsweise bildet die zweite Lage, die unbeeinflusst von dem Energieeintrag beim Umformvorgang ist, in einem Produkt zumindest teilweise eine Außenfläche. Die Schmelztemperatur der zweiten Lage ist insbesondere so gewählt, dass Oberflächeneigenschaften in der zweiten Lage unverändert bleiben. Dieses ist insbesondere im Hinblick auf Verwendung von Fasern, insbesondere Vliesfasern, beispielsweise in der Anwendung für Hygieneprodukte, aber auch bei Industrieprodukten und Bekleidungsprodukten von Bedeutung. So liegt ein verhärtetes Material vorzugsweise in der ersten Lage vor, während die zweite Lage vom Energieeintrag unbeeinflusst bleibt und damit eine unveränderte Weichheit besitzt. Neben einem Energieeintrag während des Umformvorganges besteht weiterhin die Möglichkeit, den Energieeintrag im Anschluss an den Umformvorgang durchzuführen. Beispielsweise ist dieses mittels Ultraschall, Wärmestrahlung oder auch durch chemische Reaktionen möglich. Letzteres erfolgt beispielsweise durch ein Aufbringen einer Chemikalie, ein Aktivieren einer Chemikalie oder ein Herauslösen einer Chemikalie aus der ersten Lage, wodurch eine zumindest partielle Verhärtung des thermoplastischen Materials der ersten Lage erfolgt. Beispielsweise wird dazu zumindest im Bereich der Perforierungen vorzugsweise über eine Sprüheinrichtung ein Verhärtungsmittel direkt auf die erste Lage aufgetragen. Die zweite Lage bleibt davon im wesentlichen unbeeinflusst. Ein Auftrag des Mittels kann vor oder auch nach dem Umformvorgang erfolgen.The selection of different melting points of different thermoplastic materials allows to assign different properties to the respective layers. Preferably, the second La forms ge, which is unaffected by the energy input during the forming process, in a product at least partially an outer surface. The melting temperature of the second layer is chosen in particular so that surface properties remain unchanged in the second layer. This is of particular importance with regard to the use of fibers, in particular nonwoven fibers, for example in the application for hygiene products, but also in industrial products and clothing products. Thus, a hardened material is preferably present in the first layer, while the second layer is unaffected by the energy input and thus has an unchanged softness. In addition to an energy input during the forming process, it is still possible to carry out the energy input following the forming process. For example, this is possible by means of ultrasound, heat radiation or by chemical reactions. The latter takes place, for example, by applying a chemical, activating a chemical or dissolving out a chemical from the first layer, which results in at least partial hardening of the thermoplastic material of the first layer. For example, at least in the region of the perforations, a hardening agent is preferably applied directly to the first layer via a spraying device. The second layer remains essentially unaffected. An order of the agent can be made before or after the forming process.
Gemäß einer weiteren Ausgestaltung kann auch ein Mittel zwischen die erste und die zweite Lage aufgetragen werden. Während des Umformvorganges wird beispielsweise Energie der Struktur zugeführt, wodurch das Mittel chemisch reagiert, z. B. bei Latex, und/oder physikalisch reagiert, z. B. Hotmelt. Die Reaktion führt vorzugsweise zu einem Aushärten des Mittels selbst, wodurch die erste und die zweite Lage stabilisiert werden. Weiterhin kann das Mittel so geartet sein, dass es als Kleber dient. Dadurch wird nicht nur der unmittelbar um die Perforation herum liegende Bereich, sondern auch der übrige Bereich der Struktur stabilisiert.According to one Another embodiment can also be a means between the first and the second layer can be applied. During the forming process is For example, energy is supplied to the structure, whereby the agent chemically reacts, z. As in latex, and / or physically reacted, for. B. Hotmelt. The reaction leads preferably to a curing of the agent itself, whereby the first and second layers are stabilized. Furthermore, the agent may be such that it serves as an adhesive. This will not just be around the perforation lying area, but also the remaining area of the structure stabilized.
Beispiele
für vorteilhafte
thermoplastische Materialkombinationen ergeben sich aus der nachfolgenden
Tabelle:
Getestet
wurden Flächengewichte
wie folgt:
Vorzugsweise hat die erste Lage ein Flächengewicht, das höher ist als das Flächengewicht der zweiten Lage.Preferably the first layer has a basis weight, the higher is the basis weight the second location.
Versuchergebnisse
waren wie folgt:
Muster A ist ein Spinnvlies aus PP und dient als Vergleichsmaterial. Muster B weist in der zweiten Lage ein Spinnvlies und in der ersten Lage ein cardiertes Bico-Material auf. Muster C weist in der zweiten Lage ein Spinnvlies und in der ersten Lage ein kardiertes Material auf. Muster D weist in der zweiten Lage ein BICO-Spinnvlies und in der ersten Lage ein kardiertes Bico-Vlies auf. Muster E weist in der zweiten Lage ein HDPE-Spinnvlies und in der ersten Lageein kardiertes Bico-Material auf. Alle Muster waren vor der Perforierung jeweils als einzelne Lage bondiert.template A is a spunbond of PP and serves as a reference material. template B has a spunbonded fabric in the second layer and in the first layer a carded bico material on. Pattern C points in the second Location a spunbonded and in the first layer of a carded material on. Pattern D has in the second layer a BICO spunbond and in the first layer a carded bico fleece. Pattern E points in the second layer, a HDPE spunbonded web and in the first layer a carded bico material. All patterns were each bonded as a single layer before the perforation.
Wie insbesondere der Vergleich zwischen der gemessenen und der theoretischen offenen Fläche sowie vorzugsweise das Verhältnis der Lochgröße MD/CD zeigt, gelingt es auch, besonders runde Öffnungen der Perforierungen zu stabilisieren. Die Lochdurchmesser betragen in MD zwischen 1 und 1,8 mm und in CD zwischen 0,8 und 1,7 mm.As in particular the comparison between the measured and the theoretical open area and preferably the ratio hole size MD / CD shows, it also succeeds, especially round openings of the perforations to stabilize. The hole diameters in MD are between 1 and 1.8 mm and in CD between 0.8 and 1.7 mm.
Einen weiteren Einfluss auf die Lochgrößen hat die Geschwindigkeit, mit der die Struktur durch die Perforierungseinrichtung hindurchläuft. Die Struktur wurde mit Geschwindigkeiten zwischen 5 m/s bis zu 130 m/s hindurchgeführt. Als vorteilhaft haben sich Geschwindigkeiten zwischen 45 m/s und 120 m/s, insbesondere zwischen 60 m/s und 95 m/s zur Herstellung einer stabilen Perforierung herausgestellt. Bei Lochdurchmessern, die sich in einem Bereich von unter 0,5 mm bewegen, ist eine höhere Betriebsgeschwindigkeit einstellbar. Hier sind Geschwindigkeiten bis 200 m/s einstellbar, vorzugsweise Geschwindigkeiten über 150 m/s. Die Lochdurchmesser sind beispielsweise dann in einem Bereich zwischen 0,5 und 0,1 mm. Die Perforierungswalze weist je nach Material vorzugsweise eine Temperatur zwischen etwa 100° und 160°C an einem Walzengrund auf. Eine Öltemperatur bei der Beheizung wird beispielsweise zwischen 135°C und 180°C eingestellt, während die Gegenwalze vorzugsweise eine Temperatur zwischen 45°C und 95°C, insbesondere zwischen 55°C und 75°C hat.a has further influence on the hole sizes the speed with which the structure passes through the perforating device passes. The structure was at speeds between 5 m / s up to 130 m / s passed. As advantageous speeds have between 45 m / s and 120 m / s, in particular between 60 m / s and 95 m / s for the production a stable perforation exposed. For hole diameters, moving in a range of less than 0.5 mm is a higher operating speed adjustable. Here speeds up to 200 m / s are adjustable, preferably speeds above 150 m / s. The hole diameters are then in an area, for example between 0.5 and 0.1 mm. The perforating roller shows depending on the material preferably a temperature between about 100 ° and 160 ° C on a roll base. An oil temperature when heating is set, for example, between 135 ° C and 180 ° C, while the Counter roll preferably a temperature between 45 ° C and 95 ° C, in particular between 55 ° C and 75 ° C Has.
Gemäß einem weiteren Gedanken weist eine Perforierungseinrichtung eine Zuführung für eine zu perforierende Struktur auf, die so angeordnet ist, dass die Struktur über einen Umschlingungswinkel von über 120°, vorzugsweise über 150° entlang der Gegenwalze geführt wird, bevor eine Perforierung durchführbar ist. Dadurch gelingt es insbesondere, dass bei einer erwärmten Gegenwalze die Struktur angewärmt der Perforierungswalze zugeführt wird. Darüber hinaus wird aufgrund der Umschlingung eine Spannung im Material, das sich in Kontakt mit der Gegenwalze befindet, abgesenkt. Dadurch gelingt eine besonders stabile Perforierung.According to another idea, a perforating device has a feed for a structure to be perforated, which is arranged such that the structure is guided over an angle of wrap of more than 120 °, preferably over 150 °, along the counter-roller before a perforation can be carried out. This makes it possible, in particular, that warmed in a heated counter-roller, the structure of the perforation ing roller is supplied. In addition, due to the wrap, a tension in the material in contact with the backing roll is lowered. This creates a particularly stable perforation.
Gemäß einer weiteren Ausbildung weist die Gegenwalze eine Beschichtung auf, vorzugsweise eine Gummierung. Die Beschichtung ist insbesondere zwischen 1,5 mm und 15 mm dick, insbesondere mindestens 4 mm. Die Erhebungen der Perforierungswalze können in die Beschichtung eingreifen. Vorzugsweise greifen diese in eine Tiefe von etwa 2,5 bis etwa 6 mm ein.According to one further embodiment, the counter-roller has a coating, preferably a gum. The coating is particular between 1.5 mm and 15 mm thick, in particular at least 4 mm. The Elevations of the perforating roller can interfere with the coating. Preferably, these grip to a depth of about 2.5 to about 6 mm.
Eine zweilagige zu perforierende Struktur wird gemäß einer Ausgestaltung in einem integrierten Herstellungsverfahren produziert. Beispielsweise wird bei einer Vliesherstellung eine Spinnvliesmaschine mit einem oder mehreren Balken zur Verfügung gestellt. Mittels eines der Balken wird beispielsweise eine Polymer-Mischung mit niedrigem Schmelzpunkt und mittels eines zweiten Balkens ein BICO PP/PE-Vlies hergestellt. Weiterhin kann auch auf ein vorgefertigtes Material eine zweite Lage aufgebracht und dann anschließend perforiert werden. Weiterhin besteht die Möglichkeit, die erste und die zweite Lage inline herzustellen und in einem davon getrennten Arbeitsvorgang zu perforieren. Wie am Beispiel von Vliesstoff dargestellt, besteht weiterhin die Möglichkeit, Kombinationen von Film und Vliesstoff zu verwenden. Beispielsweise kann ein Film auf ein beispielsweise kardiertes Vlies extrudiert werden und anschließend einer Perforierungseinheit zugeführt werden.A two-layer structure to be perforated according to an embodiment in a produced integrated manufacturing process. For example in a nonwoven production a spunbonding machine with one or several bars available posed. By means of one of the bars, for example, a polymer mixture with a low melting point and by means of a second bar BICO PP / PE nonwoven produced. Furthermore, can also be on a ready-made Material applied a second layer and then perforated become. It is also possible to produce the first and the second layer inline and in one of them to perforate separate operation. As with the example of nonwoven fabric shown, there is still the possibility of combinations of To use film and nonwoven fabric. For example, a movie on a For example, carded nonwoven be extruded and then a Perforation unit are supplied.
Wird gemäß einer Ausgestaltung ein Vliesmaterial als erste Lage verwendet, gelingt es dadurch, dass Vliesfasern partiell angeschmolzen werden können und auf diese Weise die Geometrie der Gestalt stabilisieren. Die Vliesfasern können dabei beispielsweise zumindest teilweise ihre Form verlieren. Gemäß einer weiteren Ausgestaltung behalten die Vliesfasern zum überwiegenden Teil ihre Form und werden adhäsiv. Gemäß einer weiteren Ausgestaltung sind die Fasern der ersten Lage zumindest teilweise mit Fasern eines Vlieses der zweiten Lage vermengt, insbesondere in Form eines Ineinandergreifens. Während beispielsweise zwei getrennt voneinander hergestellte Vlieslagen zwischen sich eine Materialgrenze aufweisen können, weisen die beiden zum Teil miteinander vermengten Vlieslagen einen Materialübergang auf. Außerhalb des Materialüberganges weisen die eine wie die andere Lage jeweils nur ein thermoplastisches Material auf. Ein derartiger Aufbau wird insbesondere mittels eines Inlineverfahrens hergestellt. Vorzugsweise weist die perforierte Struktur einen Phasenübergang oder gemäß einer weiteren Ausgestaltung eine beispielsweise vollständige Vermischung der Fasern zumindest teilweise im Bereich der Perforierung auf. Vorzugsweise werden die erste und die zweite Lage auf gleiche Weise hergestellt. Beide Lagen sind beispielsweise extrudierte Vliese, die auf der gleichen Maschine hergestellt werden. Auch besteht die Möglichkeit, unterschiedliche Materialien mit jeweils unterschiedlichen Eigenschaften zu einer perforierten Struktur bilden zu können. Während das eine Vlies PP zumindest zum überwiegenden Teil aufweist, ist das andere Vlies zum überwiegenden Teil aus HDPE oder DAPP bestehend. Darüber hinaus bestehen Kombinationsmöglichkeiten von verschiedenen Herstellungsweisen von Vliesen, insbesondere Verwendung von hochvoluminösen Stapelfaservliesen mit Spinnvliesen oder auch schmelzgeblasenes Vlies mit Spinnvlies sowie weitere Kombinationen.Becomes according to a Design a nonwoven material used as the first layer succeeds it by the fact that nonwoven fibers can be partially melted and in this way stabilize the geometry of the shape. The fleece fibers can thereby, for example, at least partially lose their shape. According to one In another embodiment, the nonwoven fibers remain predominantly Part of their form and become adhesive. According to one In another embodiment, the fibers of the first layer are at least partially mixed with fibers of a web of the second layer, in particular in the form of a mesh. For example, while two are separated fabric layers made of each other between them a material limit can have have the two partially mixed together fleece layers one Material transition on. Outside the material transition the one and the other position each have only one thermoplastic Material on. Such a construction is in particular by means of a Inline method produced. Preferably, the perforated Structure a phase transition or according to one Another embodiment, for example, complete mixing the fibers at least partially in the region of the perforation. Preferably, the first and second layers become the same produced. Both layers are for example extruded nonwovens, which are manufactured on the same machine. Also exists the Possibility, different materials, each with different properties to be able to form a perforated structure. While that one fleece PP at least for the most part Part, the other fleece is for the most part made of HDPE or DAPP. About that There are also possible combinations of different production methods of nonwovens, in particular use of high volume Staple fiber webs with spunbonded nonwovens or also meltblown Nonwoven with spunbonded fabric and other combinations.
Gemäß einer weiteren Ausgestaltung ist die erste Lage mit einer dritten Lage verbunden. Die dritte Lage weist ein thermoplastisches Material auf, dessen Schmelzpunkt höher ist als der Schmelzpunkt des thermoplastischen Materials der ersten Lage. Dadurch gelingt es, eine Art „Sandwich" zu produzieren, wobei die mittlere Lage für die Stabilität der in den drei Lagen vorhandenen dreidimensionalen Gestalt sorgt.According to one Another embodiment is the first layer with a third layer connected. The third layer has a thermoplastic material on, whose melting point higher is the melting point of the thermoplastic material of the first Location. This makes it possible to produce a kind of "sandwich", with the middle Location for the stability which provides in the three layers existing three-dimensional shape.
Gemäß einem weiteren Gedanken der Erfindung wird ein Verfahren zur Herstellung eines perforierten Laminates zur Verfügung gestellt, welches zumindest eine erste und eine zweite Lage aufweist. Ein thermoplastisches Material der ersten Lage weist einen niedrigeren Schmelzpunkt auf als das thermoplastische Material der zweiten Lage. Die erste und die zweite Lage werden zusammen in einen Perforierkalander geführt, wobei im Perforierkalander Erhebungen von einer Kalanderwalze, vorzugsweise zumindest nadelähnliche Vorsprünge, die erste und die zweite Lage durchdringen und die Erhebungen vorzugsweise beheizt sind, wobei die zweite Lage vor der ersten Lage mit den Erhebungen in Kontakt kommt.According to one Another idea of the invention is a process for the production a perforated laminate provided, which at least having a first and a second layer. A thermoplastic Material of the first layer has a lower melting point as the thermoplastic material of the second layer. The first and the second layer are passed together in a Perforierkalander, wherein in Perforierkalander elevations of a calender roll, preferably at least needle-like projections the first and the second layer penetrate and the elevations preferably are heated, wherein the second layer before the first layer with the Surveys comes into contact.
Gemäß einer Weiterbildung wird durch den Kontakt mit den Erhebungen die zweite Lage nicht angeschmolzen, während die erste Lage zumindest teilweise klebrig wird. Gemäß einem weiteren Verfahren wird die zweite Lage in einem ungeschmolzenen Zustand durch den Kalander geführt, während die erste Lage jedoch zumindest teilweise schmilzt. Gemäß einer Weiterbildung kann jedoch auch vorgesehen werden, dass die Temperatur bzw. der Energieeintrag so hoch ist, dass das thermoplastische Material der ersten Lage zumindest teilweise die Ursprungsgestalt verliert und bei Abkühlung wieder verfestigt wird. Bei entsprechender Temperatureinstellung besteht weiterhin die Möglichkeit, dass Filamente in der ersten Lage angeschmolzen werden und dabei ihre Filamentgestalt bewahren.According to one Continuing education becomes the second through contact with the surveys Location not melted while the first layer becomes at least partially sticky. According to one Another method is the second layer in an unmelted Condition passed through the calender, while however, the first layer at least partially melts. According to one However, further education can also be provided that the temperature or the energy input is so high that the thermoplastic material the first layer at least partially loses its original shape and when cooled is solidified again. With appropriate temperature setting there is still the possibility that filaments are melted in the first layer and thereby preserve their filament shape.
Weitere vorteilhafte Merkmale, Ausgestaltungen sowie Weiterbildungen werden anhand der nachfolgenden Zeichnung näher erläutert. Die dort beschriebenen Merkmale sind mit den oben beschriebenen zu weiteren Ausführungen kombinierbar. Es zeigenFurther advantageous features, refinements and developments are explained in more detail with reference to the following drawings. The ones described there Features are with the above described to further embodiments combined. Show it
Die
in
Wie
aus
Die
in
Beispiele für eine Anwendung des Laminats bzw. der Struktur in einem Produkt sind Hygieneartikel, Sanitär- und Haushaltsartikel, insbesondere Wischtücher, medizinische Produkte, Oberflächenanwendungen bei Produkten, Filtermaterialien, Schutzbekleidungen, Geotextilien, Wegwerfprodukte.Examples for one Application of the laminate or the structure in a product are sanitary articles, sanitary and household articles, especially wipes, medical products, surface applications at Products, filter materials, protective clothing, geotextiles, Disposable products.
Claims (6)
Priority Applications (2)
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DE20121445U DE20121445U1 (en) | 2001-07-03 | 2001-07-03 | Perforated laminate |
DE10132196A DE10132196B4 (en) | 2001-07-03 | 2001-07-03 | A method of making a product having a perforated thermoplastic structure and perforating means for carrying out the method |
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DE10132196A DE10132196B4 (en) | 2001-07-03 | 2001-07-03 | A method of making a product having a perforated thermoplastic structure and perforating means for carrying out the method |
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DE20121445U Expired - Lifetime DE20121445U1 (en) | 2001-07-03 | 2001-07-03 | Perforated laminate |
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DE20311313U1 (en) | 2003-07-23 | 2003-10-02 | RKW AG Rheinische Kunststoffwerke, 67547 Worms | Perforated film with a textured surface |
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DE102007063784B3 (en) * | 2007-04-18 | 2013-06-27 | Abts- Advanced Bag Technology & Service Gmbh | Flexible building material bag e.g. cement bag, has laminate comprising layers connected with each other, and inner and outer layers permeable to air, where laminate is permeable to air, and is perforated |
DE102007063783B3 (en) * | 2007-04-18 | 2013-06-27 | Abts- Advanced Bag Technology & Service Gmbh | Flexible building material bag e.g. cement bag, has laminate comprising layers connected with each other, and inner and outer layers permeable to air, where laminate is permeable to air, and is perforated |
DE102007018579B4 (en) | 2007-04-18 | 2012-03-15 | Abts- Advanced Bag Technology & Service Gmbh | Cement bag and manufacturing process |
US8460778B2 (en) * | 2008-12-15 | 2013-06-11 | Tredegar Film Products Corporation | Forming screens |
CN106738022A (en) * | 2017-03-20 | 2017-05-31 | 安徽金春无纺布股份有限公司 | A kind of tapered bore type hot-wind nonwoven cloth automatic assembly line |
DE102024117660B3 (en) * | 2024-06-21 | 2025-06-18 | tambula GmbH | Device and method for perforating web-shaped films, in particular plastic films |
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US4758297A (en) * | 1986-06-03 | 1988-07-19 | Fmc Corporation | Hot pin laminated fabric |
GB2267680A (en) * | 1992-06-02 | 1993-12-15 | Kimberly Clark Ltd | Absorbent,abrasive composite non-woven web |
JPH06280150A (en) * | 1993-03-29 | 1994-10-04 | Mitsui Petrochem Ind Ltd | Perforated laminated sheet and manufacturing method thereof |
EP0472992B1 (en) * | 1990-08-10 | 1996-05-22 | Kimberly-Clark Corporation | A nonwoven wiper and method of making same |
US5830555A (en) * | 1994-06-15 | 1998-11-03 | International Paper Company | Thermally apertured nonwoven product and process for making same |
WO1999065673A1 (en) * | 1998-06-19 | 1999-12-23 | Bba Nonwovens Simpsonville, Inc. | Thermally apertured nonwoven laminates for wipes and coverstock for hygenic articles |
-
2001
- 2001-07-03 DE DE10132196A patent/DE10132196B4/en not_active Expired - Fee Related
- 2001-07-03 DE DE20121445U patent/DE20121445U1/en not_active Expired - Lifetime
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4758297A (en) * | 1986-06-03 | 1988-07-19 | Fmc Corporation | Hot pin laminated fabric |
EP0472992B1 (en) * | 1990-08-10 | 1996-05-22 | Kimberly-Clark Corporation | A nonwoven wiper and method of making same |
GB2267680A (en) * | 1992-06-02 | 1993-12-15 | Kimberly Clark Ltd | Absorbent,abrasive composite non-woven web |
JPH06280150A (en) * | 1993-03-29 | 1994-10-04 | Mitsui Petrochem Ind Ltd | Perforated laminated sheet and manufacturing method thereof |
US5830555A (en) * | 1994-06-15 | 1998-11-03 | International Paper Company | Thermally apertured nonwoven product and process for making same |
WO1999065673A1 (en) * | 1998-06-19 | 1999-12-23 | Bba Nonwovens Simpsonville, Inc. | Thermally apertured nonwoven laminates for wipes and coverstock for hygenic articles |
Non-Patent Citations (2)
Title |
---|
Pat. Abstr. of Jp., JP 06280150 A |
Patent Abstracts of Japan & JP 06280150 A * |
Also Published As
Publication number | Publication date |
---|---|
DE20121445U1 (en) | 2002-10-17 |
DE10132196A1 (en) | 2003-01-30 |
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