JPH09169055A - Heat lamination method of crystalline thermoplastic resin sheet - Google Patents
Heat lamination method of crystalline thermoplastic resin sheetInfo
- Publication number
- JPH09169055A JPH09169055A JP7348193A JP34819395A JPH09169055A JP H09169055 A JPH09169055 A JP H09169055A JP 7348193 A JP7348193 A JP 7348193A JP 34819395 A JP34819395 A JP 34819395A JP H09169055 A JPH09169055 A JP H09169055A
- Authority
- JP
- Japan
- Prior art keywords
- resin sheet
- temperature
- resin
- sheet
- adhesive
- 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.)
- Granted
Links
Classifications
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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
- B29C66/40—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
- 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
- B29C65/1429—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 way of heating the interface
- B29C65/1432—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 way of heating the interface direct heating of the surfaces 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
- 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
- B29C65/1429—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 way of heating the interface
- B29C65/1445—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 way of heating the interface heating both sides of the joint
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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
- B29C65/1429—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 way of heating the interface
- B29C65/1464—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 way of heating the interface making use of several radiators
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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
- B29C65/1429—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 way of heating the interface
- B29C65/1464—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 way of heating the interface making use of several radiators
- B29C65/1467—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 way of heating the interface making use of several radiators at the same time, i.e. simultaneous welding
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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
- B29C65/78—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
- B29C66/02—Preparation of the material, in the area to be joined, prior to joining or welding
- B29C66/024—Thermal pre-treatments
- B29C66/0242—Heating, or preheating, e.g. drying
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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
- B29C66/03—After-treatments in the joint area
- B29C66/034—Thermal after-treatments
- B29C66/0342—Cooling, e.g. transporting through welding and cooling zone
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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
- B29C66/70—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
- B29C66/737—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 state of the material of the parts to be joined
- B29C66/7377—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 state of the material of the parts to be joined amorphous, semi-crystalline or crystalline
- B29C66/73775—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 state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being crystalline
- B29C66/73776—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 state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being crystalline the to-be-joined areas of both parts to be joined being crystalline
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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
- 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
- B29C66/83413—Roller, cylinder or drum types cooperating rollers, cylinders or drums
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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
- B29C66/83—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
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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
- B29C66/90—Measuring or controlling the joining process
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- B29C66/9141—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature
- B29C66/91411—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature of the parts to be joined, e.g. the joining process taking the temperature of the parts to be joined into account
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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
- B29C66/90—Measuring or controlling the joining process
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- B29C66/9141—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature
- B29C66/91421—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature of the joining 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
- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
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- B29C66/9141—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature
- B29C66/91441—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature the temperature being non-constant over time
- B29C66/91443—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature the temperature being non-constant over time following a temperature-time profile
- B29C66/91445—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the temperature the temperature being non-constant over time following a temperature-time profile by steps
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/90—Measuring or controlling the joining process
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- B29C66/91641—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the heat or the thermal flux, i.e. the heat flux the heat or the thermal flux being non-constant over time
- B29C66/91643—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux by controlling or regulating the temperature, the heat or the thermal flux by controlling or regulating the heat or the thermal flux, i.e. the heat flux the heat or the thermal flux being non-constant over time following a heat-time profile
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- B29C66/90—Measuring or controlling the joining process
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- B29C66/9192—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
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- B29C66/9192—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams
- B29C66/91921—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature
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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
- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
- B29C66/919—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges
- B29C66/9192—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams
- B29C66/91921—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature
- B29C66/91931—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature in explicit relation to the fusion temperature or melting point of the material of one of the parts to be joined
- B29C66/91933—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature in explicit relation to the fusion temperature or melting point of the material of one of the parts to be joined higher than said fusion temperature
-
- 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
- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
- B29C66/919—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges
- B29C66/9192—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams
- B29C66/91921—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature
- B29C66/91931—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature in explicit relation to the fusion temperature or melting point of the material of one of the parts to be joined
- B29C66/91935—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges in explicit relation to another variable, e.g. temperature diagrams in explicit relation to another temperature, e.g. to the softening temperature or softening point, to the thermal degradation temperature or to the ambient temperature in explicit relation to the fusion temperature or melting point of the material of one of the parts to be joined lower than said fusion temperature
-
- 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
-
- 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
- B29C65/1416—Near-infrared radiation [NIR]
-
- 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
- B29C65/1422—Far-infrared radiation [FIR]
-
- 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
- B29C65/16—Laser beams
- B29C65/1603—Laser beams characterised by the type of electromagnetic radiation
- B29C65/1612—Infrared [IR] radiation, e.g. by infrared lasers
-
- 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
- B29C65/16—Laser beams
- B29C65/1603—Laser beams characterised by the type of electromagnetic radiation
- B29C65/1612—Infrared [IR] radiation, e.g. by infrared lasers
- B29C65/1616—Near infrared radiation [NIR], e.g. by YAG lasers
-
- 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
- B29C65/16—Laser beams
- B29C65/1603—Laser beams characterised by the type of electromagnetic radiation
- B29C65/1612—Infrared [IR] radiation, e.g. by infrared lasers
- B29C65/1619—Mid infrared radiation [MIR], e.g. by CO or CO2 lasers
-
- 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
- B29C65/72—Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by combined operations or combined techniques, e.g. welding and stitching
-
- 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
-
- 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
- B29C66/737—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 state of the material of the parts to be joined
- B29C66/7377—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 state of the material of the parts to be joined amorphous, semi-crystalline or crystalline
- B29C66/73771—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 state of the material of the parts to be joined amorphous, semi-crystalline or crystalline the to-be-joined area of at least one of the parts to be joined being amorphous
-
- 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
- B29C66/90—Measuring or controlling the joining process
- B29C66/91—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux
- B29C66/919—Measuring or controlling the joining process by measuring or controlling the temperature, the heat or the thermal flux characterised by specific temperature, heat or thermal flux values or ranges
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Health & Medical Sciences (AREA)
- Electromagnetism (AREA)
- Toxicology (AREA)
- High Energy & Nuclear Physics (AREA)
- Crystallography & Structural Chemistry (AREA)
- Chemical & Material Sciences (AREA)
- Plasma & Fusion (AREA)
- Laminated Bodies (AREA)
- Lining Or Joining Of Plastics Or The Like (AREA)
Abstract
Description
【0001】[0001]
【発明の属する技術分野】本発明は、プラスチックの熱
融着ラミネート方法で、特に結晶性のあるポリオレフィ
ン系素材の樹脂シートに適した熱ラミネート方法に関す
る。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a heat fusion laminating method for plastics, and more particularly to a heat laminating method suitable for a resin sheet of a crystalline polyolefin material.
【0002】[0002]
【従来の技術】従来より、可塑剤を含んだ塩化ビニル樹
脂シート等の熱可塑性樹脂シートを熱ラミネートする方
法が知られている。例えば、「特許庁公報 周知・慣用
技術集」(日本国特許庁、昭和59年6月15日発行、
第163頁)には、熱可塑性樹脂フィルムの熱融着接着
方法として、2層の樹脂フィルムを連続的に熱圧着する
か、又は加熱プレスで熱圧着することにより接着一体化
する方法が挙げられている。また、接着一体化と樹脂フ
ィルムの表面への賦形をするエンボス処理を同時に行
う、いわゆるダブリングエンボス法が挙げられている。
この方法によれば、対象とする樹脂フィルムは、塩化ビ
ニル樹脂、アクリル樹脂、アクリロニトリル−ブタジエ
ン−スチレン共重合体フィルム等であるが、又、一般的
に熱接着が困難なオレフィン系樹脂フィルム、ポリエス
テルフィルム等も、あらかじめヒートシール剤をフィル
ムにコーティングしておく事により同様に熱接着する事
が出来ると説明している。2. Description of the Related Art Conventionally, a method of thermally laminating a thermoplastic resin sheet such as a vinyl chloride resin sheet containing a plasticizer has been known. For example, "Public Office Official Notices and Common Techniques" (Japanese Patent Office, published June 15, 1984,
(P. 163), as a method for heat-sealing and adhering a thermoplastic resin film, there is a method in which two layers of resin films are continuously thermocompression bonded or thermocompression-bonded by a heat press for adhesion and integration. ing. Further, there is a so-called doubling embossing method in which the bonding and integration and the embossing treatment for shaping the surface of the resin film are simultaneously performed.
According to this method, the target resin film is a vinyl chloride resin, an acrylic resin, an acrylonitrile-butadiene-styrene copolymer film, or the like, but, in general, it is difficult to thermally bond the olefin resin film and the polyester. It is explained that a film or the like can be similarly heat-bonded by coating the film with a heat sealing agent in advance.
【0003】図3は、この様な方法によるエンボス装置
を兼ねた従来の熱ラミネート装置(すなわちダブリング
エンボス装置)の装置構成を示す概念図である。同図を
説明すれば、2層の樹脂シートS1及びS2は各々巻取
ロール91a及び91bから供給され、予熱ロール92
a及び92bで各々予熱されてからヒートドラム93部
分で重ね合わされつつヒートドラム93で加熱されると
共に、予熱用パネルヒータ94aでも非接触による輻射
熱でも加熱され、次いで、予熱用パネルヒータ94b及
び94cで輻射加熱されつつ、表面をテフロン製として
非粘着化した予熱ロール95a〜95cでさらに加熱さ
れて、エンボスロール96と圧胴97の間に導かれて、
加圧されてエンボス処理と2層のシートの積層・接着に
よる一体化が行われ、その後、冷却ロール98で冷却さ
れて巻取ロール91cで巻き取られるというものであ
る。FIG. 3 is a conceptual diagram showing a device configuration of a conventional thermal laminating device (that is, a doubling embossing device) which also serves as an embossing device by such a method. Referring to the figure, the two-layer resin sheets S1 and S2 are supplied from the winding rolls 91a and 91b, respectively, and the preheating roll 92 is supplied.
a and 92b, respectively, and then heated by the heat drum 93 while being superposed on the heat drum 93 portion, and also heated by the preheat panel heater 94a and radiant heat by non-contact, and then by the preheat panel heaters 94b and 94c. While being radiantly heated, it is further heated by preheating rolls 95a to 95c whose surface is made of Teflon and made non-adhesive, and is guided between the embossing roll 96 and the impression cylinder 97,
The sheet is pressurized, embossed and integrated by laminating and adhering the two layers of sheets, and then cooled by the cooling roll 98 and wound by the winding roll 91c.
【0004】この様な構造の熱ラミネート装置には他に
も各種あり、例えば特開昭57−157756号公報で
は、可塑剤を含有する塩化ビニル樹脂シートについて、
積層後に上側となる上台シートのみを熱ドラムで加熱
後、さらにヒータによる非接触加熱でシートが軟化する
温度まで加熱し、一方、積層後に下側となる下台シート
の方は予め施されているエンボスが戻らない程度にまで
抑えて予備加熱して、これら両シートを重ね合わせて加
圧して、2層のシート間にエンボスがある構造の積層シ
ートを製造する熱ラミネート方法が開示されている。There are various other types of thermal laminating apparatus having such a structure. For example, in JP-A-57-157756, a vinyl chloride resin sheet containing a plasticizer is disclosed.
After heating only the upper base sheet after lamination with a heating drum, it is further heated to a temperature that softens the sheet by non-contact heating with a heater, while the lower base sheet after lamination is pre-embossed. There is disclosed a thermal laminating method for producing a laminated sheet having a structure in which two sheets are superposed with each other by pressurizing them so as not to return to each other and preheating them.
【0005】また、特公平42−551号公報では、赤
外線による輻射加熱装置及び加熱ドラムにより塩化ビニ
ルレーザの樹脂シートAを軟化させ、これにポリエステ
ルフィルム等の耐熱性で強靱屈曲性に富みかつ剥離しや
すい薄いフィルムBを重ね合わせて状態で、エンボスロ
ールと圧胴との間を通すことで、エンボスと共に積層し
て熱ラミネートを行った後、フィルムBをシートAから
剥離することで、エンボスロールの凹凸をフィルムBを
通してシートAの表面に間接的にエンボス形成するとい
う、熱ラミネート方法を応用した薄いぼかした紋模様を
形成する方法等も提案されている。In Japanese Patent Publication No. 42-551, a resin sheet A of a vinyl chloride laser is softened by an infrared radiation heating device and a heating drum, and a polyester film or the like is heat-resistant and has high toughness and flexibility and is peeled off. The thin film B, which is easy to be laminated, is passed between the embossing roll and the impression cylinder so that the thin film B is laminated with the embossing to perform thermal lamination, and then the film B is peeled from the sheet A. There is also proposed a method of forming a thin blurred pattern by applying a thermal laminating method, such as indirectly embossing the unevenness of No. 2 on the surface of the sheet A through the film B.
【0006】また、特公平2−61378号公報では、
一対の熱ラミネートロールに積層すべき2層の樹脂シー
トを重ね合わせて通す前に、予備熱処理ロールでより厚
みの大きい方の樹脂シートを予熱処理しながら行う熱ラ
ミネート方法が提案されている。また、同号公報ではこ
の方法が適用できる樹脂として、ポリスチレン系樹脂等
と共に、ポリエチレン、ポリプロピレン等の結晶性熱可
塑性樹脂等も挙げている。In Japanese Patent Publication No. 2-61378,
A thermal laminating method has been proposed in which a two-layer resin sheet to be laminated is passed through a pair of thermal laminating rolls while the resin sheet having a larger thickness is preheated by a preliminary heat treatment roll before being passed through. In addition, in the same publication, as a resin to which this method can be applied, a crystalline thermoplastic resin such as polyethylene or polypropylene is cited as well as a polystyrene resin.
【0007】[0007]
【発明が解決しようとする課題】しかしながら、上述し
た従来の熱ラミネート方法では、可塑剤含有の塩化ビニ
ル樹脂シートや非晶性熱可塑性樹脂シート等では熱ラミ
ネートの適正温度範囲が広く製造は容易だが、特にポリ
エチレン、ポリプロピレン等のポリオレフィン系樹脂等
による結晶性熱可塑性樹脂シートの場合には適正温度範
囲が狭く熱ラミネートに問題があった。それは、結晶性
熱可塑性樹脂シートでは、シートの樹脂の融点近傍にお
いて、急激にシートが軟化して強度が低下する熱−機械
的特性がある為に温度制御が難しく、加熱過多の場合、
シートが溶融し、切断又は歪みや伸びを生じてしまうか
らであった。そして、シート表面が粘着性をおびて、加
熱ローラから剥離しない等の問題が生じた。また、加熱
が少な過ぎると、2層の樹脂シート同士の接着力が不足
してラミネート強度が出ず、またエンボスも施す場合に
はエンボスの入りが甘く、エンボスの耐熱性が低くてラ
ミネート時の残留応力や歪みの解放も不充分であった。
なお、ポリエチレン、ポリプロピレン等のポリオレフィ
ン系樹脂のシートの場合には、得られた積層シートの表
面の接着性を改善する為に、コロナ処理等を熱ラミネー
ト前に施しておいたとしても、加熱によりその効果が薄
れてしまうという問題もあった。However, in the above-mentioned conventional thermal laminating method, a plasticizer-containing vinyl chloride resin sheet, an amorphous thermoplastic resin sheet or the like has a wide suitable temperature range for thermal laminating and is easy to manufacture. In particular, in the case of a crystalline thermoplastic resin sheet made of a polyolefin resin such as polyethylene or polypropylene, the proper temperature range is narrow and there is a problem in thermal lamination. That is, in the crystalline thermoplastic resin sheet, in the vicinity of the melting point of the resin of the sheet, it is difficult to control the temperature because of the thermo-mechanical characteristics that the sheet suddenly softens and the strength decreases, and in the case of excessive heating,
This is because the sheet melts and causes cutting or distortion or elongation. Then, there arises a problem that the surface of the sheet becomes tacky and is not separated from the heating roller. Also, if the heating is too low, the adhesive strength between the two layers of resin sheets will be insufficient and the laminating strength will not be obtained, and if embossing is also applied, the embossing will not be easy and the heat resistance of the embossing will be low and the laminating strength will be low. Relief of residual stress and strain was also insufficient.
In the case of a sheet of a polyolefin resin such as polyethylene or polypropylene, in order to improve the adhesiveness of the surface of the obtained laminated sheet, even if corona treatment or the like is performed before thermal lamination, it is still heated. There was also a problem that the effect diminished.
【0008】[0008]
【課題を解決するための手段】そこで上記課題を解決す
る為に、本発明の熱ラミネート方法では、2層の結晶性
熱可塑性樹脂シートの樹脂の結晶融解温度に注目しつ
つ、加圧積層を主として仮ラミネートとしての第1の加
圧積層(各請求項の工程(b) )の工程と、本ラミネート
としての第2の加圧積層(各請求項の工程(d) )の工程
との2段階に分けて行い、最初の仮ラミネート工程で
は、両シートの接着面表面近傍のみ接着性を発現させる
ために結晶融解温度以上に加熱し、それ以外の部分は結
晶融解温度未満に保つことでこの部分でシートの強度を
確保した状態で仮接着を行い、次いで本ラミネート工程
で、両シート表面を所望の表面状態(平滑又は凹凸)に
する為、及び両シート内の残留応力を除く為、更により
接着力を高くする為に両シートを結晶融解温度以上で融
点迄未満の温度まで加熱した状態で接着し、その後、結
晶融解温度以下に、さらに室温まで冷却する様にして、
熱可塑性樹脂シートが結晶性であっても熱ラミネートを
行える様にした。この結果、両シートの熱変形、歪み、
破断、ガイドローラ等接触部分との粘着防止を企てつ
つ、両シートを積層できる様にした。In order to solve the above problems, in the thermal laminating method of the present invention, pressure lamination is performed while paying attention to the crystal melting temperature of the resin of the two-layer crystalline thermoplastic resin sheet. Mainly, a first pressure laminating step (step (b) in each claim) as a temporary laminate and a second pressure laminating step (step (d) in each claim) as a main laminate. In the first temporary laminating step, heating is performed above the crystal melting temperature in order to develop adhesiveness only in the vicinity of the bonding surface of both sheets, and the other parts are kept below the crystal melting temperature by this step. Temporary bonding is performed while ensuring the strength of the sheet at the part, and then in the present laminating process, both sheet surfaces are made to have a desired surface state (smooth or uneven) and residual stress in both sheets is removed. To increase the adhesive strength Bonding the over bets while heating a crystalline melting temperature above to a temperature below up to the melting point, then, the following crystalline melting temperature, in the manner further cooling to room temperature,
Even if the thermoplastic resin sheet is crystalline, thermal lamination can be performed. As a result, thermal deformation and distortion of both sheets,
Both sheets can be laminated while attempting to prevent breakage and adhesion to contact parts such as guide rollers.
【0009】また、上記の方法は、両シートに予め接着
剤を施したものを使う場合は、該接着剤としてその接着
力発現温度を両シートの結晶融解温度未満のものが施さ
れているものを用意し、仮ラミネート工程は前記接着力
発現温度以上で且つ上記結晶融解温度未満の温度で接着
を行い、後は前述同様に本ラミネート工程は両シートを
結晶融解温度以上で融点迄未満の温度まで加熱した状態
で接着する様にして、熱可塑性樹脂シートが結晶性であ
っても熱ラミネートを行える様にした。この場合も前述
同様に、両シートの熱変形、歪み、破断、ガイドローラ
等接触部分との粘着防止を企てつつ、両シートを積層で
きることとなる。Further, in the above method, when both sheets are preliminarily coated with an adhesive, the one whose adhesive strength expression temperature is lower than the crystal melting temperature of both sheets is used as the adhesive. In the temporary laminating step, the bonding is performed at a temperature which is equal to or higher than the adhesive strength developing temperature and lower than the crystal melting temperature. The thermoplastic resin sheet was bonded so that it could be thermally laminated even if it was crystalline. In this case as well, both sheets can be laminated while attempting to prevent thermal deformation, distortion, breakage, and adhesion to the contact portion such as the guide roller in the same manner as described above.
【0010】[0010]
【発明の実施の形態】以下、図面を参照しながら本発明
の結晶性熱可塑性樹脂シートの熱ラミネート方法を説明
する。BEST MODE FOR CARRYING OUT THE INVENTION A method for thermally laminating a crystalline thermoplastic resin sheet according to the present invention will be described below with reference to the drawings.
【0011】先ず、図1は本発明の結晶性熱可塑性樹脂
シートの熱ラミネート方法を実現する為の熱ラミネート
装置の装置構成を示す概念図である。同図に示す如く、
本発明を実現し得る熱ラミネート装置の加圧積層部分
は、第1の加圧積層を行う仮ラミネート部分と、第2の
加圧積層を行う本ラミネート部分とを有する。仮ラミネ
ート部分は圧着ロール31及び32で加圧され、本ラミ
ネート部分はラミネートロール5及び圧胴6により加圧
される。樹脂シートS1及びS2は、各々巻取ロール1
1及び12から対を成す供給側ニップロール81a及び
81bによりニップされつつ送り出されて仮ラミネート
部分に供給されていく。そして、仮ラミネート部分で
は、両シートS1及びS2は、その接着面側を各々、加
熱ロール21及び22により加熱れさ、さらに加熱ロー
ルから離れて表面が低温の圧着ロール31及び32によ
り挟まれて加圧積層されるまでの間に冷えない様に、予
熱用パネルヒータ41及び42による赤外線輻射により
加熱されて、圧着ロール31及び32により両樹脂シー
ト同士の仮ラミネートが行われる。そして、本発明の熱
ラミネート方法では、この仮ラミネートの際に、両樹脂
シートの接着面側の表面近傍の温度と、非接着面側の表
面近傍の温度を、所定の温度に制御することになる。First, FIG. 1 is a conceptual diagram showing an apparatus configuration of a thermal laminating apparatus for realizing the method for thermally laminating a crystalline thermoplastic resin sheet of the present invention. As shown in FIG.
The pressure laminating portion of the thermal laminating apparatus that can realize the present invention has a temporary laminating portion for performing the first pressure laminating and a main laminating portion for performing the second pressure laminating. The temporary laminated portion is pressed by the pressure bonding rolls 31 and 32, and the main laminated portion is pressed by the laminating roll 5 and the impression cylinder 6. The resin sheets S1 and S2 are the winding roll 1 respectively.
The supply side nip rolls 81a and 81b, which are paired with 1 and 12, feed the nip rolls 81a and 81b while feeding the nip rolls 81a and 81b. Then, in the temporary laminating portion, both the sheets S1 and S2 are heated by the heating rolls 21 and 22, respectively, on the bonding surface side thereof, and further separated from the heating rolls and the surfaces are sandwiched by the pressure bonding rolls 31 and 32 having a low temperature. The resin sheets are preliminarily laminated by the pressure rolls 31 and 32 by being heated by infrared radiation from the preheating panel heaters 41 and 42 so as not to cool before being pressure-laminated. Then, in the thermal laminating method of the present invention, during this temporary lamination, the temperature near the surface on the adhesive surface side of both resin sheets and the temperature near the surface on the non-adhesive surface side are controlled to a predetermined temperature. Become.
【0012】以上の様にして2層の樹脂シートは、仮ラ
ミネートにより一応積層されて積層シートとなるが、次
にこの積層シートを最終的な温度まで加熱して本ラミネ
ートを行う。そこで、圧着ロールから出た積層シート
は、圧着ロールから垂直にほぼ自重により落下させて、
ラミネートロール5及び圧胴6に至る直前で予熱用パネ
ルヒータ43及び44によって、本発明が規定する所定
の温度まで積層シートに接触することなく非接触で加熱
して、ラミネートロール5及び圧胴6によって、加圧し
積層、接着して一体化する。従って、本ラミネートのラ
ミネートロール5及び圧胴6(のニップ面)は、仮ラミ
ネートの圧着ロール31及び32(のニップ面)の真下
に位置する構造である。即ち、シートの自重(重力)の
方向はシートの搬送方向の成分のみ有し、シートと直交
しそれを変形させる成分を持たない。又、ローラ等から
力を受ける事もない。これによって、本ラミネート直前
に結晶融解温度以上且つ融点未満の温度まで加熱されて
弾性率が低下して不安定な状態の仮接着した積層シート
であっても、安定的に仮ラミネート部分から本ラミネー
ト部分に搬送移入できることとなる。これに対して、例
えば図3に示す従来の熱ラミネート装置では、接触加熱
による予熱ロール95a〜c等により蛇行したり、張力
によって伸ばされたりする等して、この点でも結晶性熱
可塑性樹脂シートの加工は不可能な構造であった。As described above, the two-layer resin sheet is tentatively laminated to form a laminated sheet. Next, this laminated sheet is heated to the final temperature for main lamination. Therefore, the laminated sheet discharged from the pressure bonding roll is dropped vertically from the pressure bonding roll almost by its own weight,
Immediately before reaching the laminating roll 5 and the impression cylinder 6, the preheating panel heaters 43 and 44 heat the laminated sheet to a predetermined temperature defined by the present invention without contacting the laminated sheet, and the laminating roll 5 and the impression cylinder 6 are heated. By applying pressure, stacking, and adhering to integrate. Therefore, the laminate roll 5 and the impression cylinder 6 (nip surface thereof) of the main laminate have a structure located directly below (the nip surface of) the pressure rolls 31 and 32 of the temporary laminate. That is, the direction of the sheet's own weight (gravity) has only a component in the sheet conveying direction, and has no component orthogonal to the sheet and deforming it. Also, it does not receive any force from the rollers or the like. As a result, even if the laminated sheet is temporarily adhered in a unstable state due to a decrease in elastic modulus due to being heated to a temperature higher than or equal to the crystal melting temperature and lower than the melting point immediately before the main lamination, the main lamination can be stably performed from the temporary lamination part. It will be possible to transfer and transfer to the part. On the other hand, for example, in the conventional thermal laminating apparatus shown in FIG. 3, the crystalline thermoplastic resin sheet is meandered by the preheating rolls 95a to 95c by contact heating or stretched by the tension, and in this respect as well. The structure was impossible to process.
【0013】その後、剥離ロール83により積層シート
をラミネートロール5から剥離して、クーリングロール
71〜73によって段階的に冷やした後、対を成す排紙
側ニップロール82でニップされつつ引き出されて巻取
ロール13に巻き取られる。After that, the laminated sheet is peeled off from the laminating roll 5 by the peeling roll 83, and is gradually cooled by the cooling rolls 71 to 73, and is then drawn out and wound while being nipped by the pair of discharge side nip rolls 82. It is wound up on a roll 13.
【0014】以上は本発明の熱ラミネート方法で用い得
る熱ラミネート装置の一例であるが、この装置では、従
来の熱ラミネート装置と異なり、積層する樹脂シートの
接着面側と非接着面側との両方の表面を別々に加熱制御
でき、また、2段階の加圧積層部分がある点が大きく異
なる。例えば、図3に示した従来の熱ラミネート装置で
は、各種予熱ロール及び予熱用パネルヒータのシートに
対する加熱面は、特に接着面側を加熱するというもので
はなく、装置的構造の容易性から、主として積層後のシ
ートの表側面(例えば、シートS1に対する予熱ロール
92a、予熱用パネルヒータ94a〜94c、予熱ロー
ル95a〜95c)である。ただ一つ接着面側に有るも
のはシートS2に対する予熱ロール92bである。The above is an example of a thermal laminating apparatus that can be used in the thermal laminating method of the present invention. In this apparatus, unlike the conventional thermal laminating apparatus, the adhesive surface side and the non-adhesive surface side of the resin sheet to be laminated are Both surfaces can be separately heated and controlled, and there is a large difference in that there is a two-stage pressure laminated portion. For example, in the conventional thermal laminating apparatus shown in FIG. 3, the heating surfaces of the various preheating rolls and preheating panel heaters for the sheets are not those for heating the bonding surface side in particular, and mainly because of the ease of the apparatus structure. It is the front surface of the laminated sheets (for example, the preheating roll 92a for the sheet S1, the preheating panel heaters 94a to 94c, and the preheating rolls 95a to 95c). The only one on the adhesive surface side is the preheating roll 92b for the sheet S2.
【0015】また、図1の熱ラミネート装置で、加熱ロ
ール21及び22は、内部が中空になった鉄、銅等の金
属製ロールで空芯内に油、水(水蒸気)等の伝熱媒体を
循環させたり、誘電加熱で温度制御を行う。ロール表面
は耐蝕性を考慮したクロムメッキ或いは剥離性を考慮し
たフッ素樹脂コートがされていても良い。この加熱ロー
ル21及び22は、積層すべき2層の樹脂シートの接着
面に接触して接着面側を非接着面側に対してより高い温
度に加熱する。なお、この様な接触による伝導加熱によ
らずに次に説明する非接触加熱のヒータに置き換えるこ
ともできる。予熱用パネルヒータ41及び42、さらに
予熱用パネルヒータ43及び44は、近赤外線〜遠赤外
線を輻射する電熱線ヒータ、セラミックヒータ等の電熱
式赤外線輻射ヒータ、或いは高周波交流電場を用いた誘
電加熱、或いは熱風の吹き付け、或いはYAGレーザ、
炭酸ガスレーザ等の赤外線レーザ光の照射等の非接触で
加熱して加熱調整が容易にできるものとする。シートの
接着面側表面近傍のみを加熱するという点から仮ラミネ
ート直前のヒータ41、42は電熱線輻射ヒータ、或い
は熱風の吹き付け、或いは赤外レーザのパルス照射が好
ましい。又、本ラミネート直前のヒータ43、44はシ
ート厚み方向全体を均一に加熱するという点から、遠赤
外線を輻射するセラミック電熱ヒータ、誘電加熱が好ま
しい。圧着ロール31及び32も、加熱ロール21及び
22と同様に内部が中空の金属製ロールで空芯内に油、
水(水蒸気)等の伝熱媒体を循環させたり、誘電加熱で
温度制御を行う。但し、一方のロールの表面にはシリー
コンゴム等のゴム状弾性体を被覆しておくことが好まし
い。In the thermal laminating apparatus shown in FIG. 1, the heating rolls 21 and 22 are metal rolls having hollow interiors, such as iron and copper, and heat transfer media such as oil and water (steam) in the air core. Temperature is controlled by circulating or by dielectric heating. The roll surface may be chromium-plated in consideration of corrosion resistance or may be coated with a fluororesin in consideration of releasability. The heating rolls 21 and 22 contact the adhesive surfaces of the two-layer resin sheets to be laminated and heat the adhesive surface side to a higher temperature than the non-adhesive surface side. Note that a non-contact heating heater described below can be used instead of such conductive heating by contact. The preheating panel heaters 41 and 42, and further the preheating panel heaters 43 and 44 are heating wire heaters that radiate near infrared rays to far infrared rays, electrothermal infrared radiation heaters such as ceramic heaters, or dielectric heating using a high frequency AC electric field. Or blowing hot air, or YAG laser,
The heating and adjustment can be easily performed by heating without contact such as irradiation with an infrared laser beam such as a carbon dioxide gas laser. It is preferable that the heaters 41 and 42 immediately before the temporary lamination are heating wire radiant heaters, hot air blowing, or infrared laser pulse irradiation from the viewpoint of heating only the vicinity of the adhesive side surface of the sheet. Further, the heaters 43 and 44 immediately before the main lamination are preferably a ceramic electric heater that radiates far infrared rays and a dielectric heater from the viewpoint of uniformly heating the entire sheet thickness direction. Similarly to the heating rolls 21 and 22, the pressure bonding rolls 31 and 32 are metal rolls having a hollow interior, and oil inside the air core,
A heat transfer medium such as water (water vapor) is circulated, or the temperature is controlled by dielectric heating. However, it is preferable to coat the surface of one roll with a rubber-like elastic material such as silicone rubber.
【0016】ラミネートロール5は中空の金属製ロール
で、表面はエンボスをしない場合にはクロムメッキ等で
鏡面平滑に仕上げてある。また、エンボスをする場合
は、すなわちエンボスロールの場合は銅メッキを介し
て、或いは介さずにエッチング、彫刻等の手法により表
面に所望の凹凸模様を施したものを使う。或いはエンボ
スロールとしては、ロール表層を樹脂或いはセラミック
スにしてレーザ彫刻を行ったもの、或いは電鋳法によっ
て所望の凹凸模様の母型上に銅等の金属をメッキして作
ったもの等も使用できる。なお、凹凸模様は木目導管、
皮紋、砂目、梨地、ヘアライン、布目等である。圧胴6
は中空の金属製ロールでその表面をシリコーンゴム層等
のゴム状弾性体で被覆し、空芯内には温水を循環させて
温度制御したロールである。そして冷却ロール71〜7
3は、金属等の熱伝導率の高い材質の中空ロール内に冷
水等の低温の伝熱媒体を流通された構成のロールであ
る。冷却は或いはヒートパイプに接触させたりしても良
い。また、冷風の吹付けを併用しても良い。The laminating roll 5 is a hollow metal roll, and its surface is mirror-finished by chrome plating or the like when it is not embossed. In the case of embossing, that is, in the case of an embossing roll, a surface having a desired uneven pattern is used by a method such as etching or engraving with or without copper plating. Alternatively, as the embossing roll, a roll surface layer made of resin or ceramics and subjected to laser engraving, or a plate made by plating a metal such as copper on a mold having a desired uneven pattern by electroforming can be used. . In addition, the uneven pattern is a wood grain conduit,
Examples include skin prints, grain, satin, hairline, and cloth. Impression cylinder 6
Is a hollow metal roll whose surface is covered with a rubber-like elastic material such as a silicone rubber layer and whose temperature is controlled by circulating hot water in the air core. And the cooling rolls 71 to 7
3 is a roll having a structure in which a low-temperature heat transfer medium such as cold water is circulated in a hollow roll made of a material having a high thermal conductivity such as metal. Alternatively, cooling may be performed by contact with a heat pipe. Further, cold air may be blown together.
【0017】なお、上述の熱ラミネート装置で冷却ロー
ルで冷却されてから巻取ロールで巻き取る迄の間に塗工
装置を設ければ、オンラインで熱ラミネートと塗工とを
同時に行うこともできる。塗工装置としては、例えば、
グラビアコーター、ロールコーター、コンマコーター等
の各種のウェブ用コーターで良く、また必要に応じて乾
燥ゾーンを併設する。また、塗工装置の前に、或いは塗
工装置が設けない場合でも、適宜、水濡れ性、接着性能
の向上を図る為にコロナ処理でラミネート後の積層フィ
ルムの表面を改質しても良い。If a coating device is provided between the cooling with the cooling roll in the thermal laminating device and the winding with the winding roll, the thermal laminating and the coating can be simultaneously performed online. . As the coating device, for example,
Various web coaters such as a gravure coater, a roll coater, and a comma coater may be used, and a drying zone may be provided if necessary. In addition, before the coating device, or even when the coating device is not provided, the surface of the laminated film after lamination may be modified by corona treatment in order to improve water wettability and adhesion performance. .
【0018】次に、本発明の熱ラミネート方法に適する
樹脂シートとしては、熱可塑性樹脂からなるものである
が、特に結晶性の熱可塑性樹脂からなるシートにおい
て、優れた適性を発揮する。これらの結晶性熱可塑性樹
脂としては、例えば、ポリエチレン、ポリプロピレン、
ポリブテン、ポリメチルペンテン等のポリオレフィン系
樹脂、或いは、ナイロン6、ナイロン66等の線状ポリ
アミド、ポリエチレンテレフタレート、ポリブチレンテ
レフタレート等のポリエステル系樹脂等に有効である。
また、この他、ポリ塩化ビニル樹脂、アクリル樹脂等で
も有効である。また、樹脂シートの厚みは、通常10〜
500μm程度である。Next, the resin sheet suitable for the thermal laminating method of the present invention is made of a thermoplastic resin, and particularly a sheet made of a crystalline thermoplastic resin exhibits excellent suitability. Examples of these crystalline thermoplastic resins include polyethylene, polypropylene,
It is effective for polyolefin resins such as polybutene and polymethylpentene, linear polyamides such as nylon 6 and nylon 66, and polyester resins such as polyethylene terephthalate and polybutylene terephthalate.
In addition, polyvinyl chloride resin, acrylic resin, etc. are also effective. The thickness of the resin sheet is usually 10
It is about 500 μm.
【0019】そして、本発明の結晶性熱可塑性樹脂シー
トの熱ラミネート方法でいうところの、結晶融解温度に
ついて説明する。一般に純粋な結晶の場合は、固体状態
から液体状態に変化する結晶融解温度は、融点として一
義的に定義される得る物理量である。ところが、柔軟な
分子鎖からなる通常の結晶性の高分子物質の場合には、
固体状態は無定形領域と結晶領域(微結晶)とからなっ
ており、この微結晶は種々の大きさ、種々の内部欠陥等
により安定状態の異なった種々の集合状態になってお
り、その結果、結晶性(熱可塑性)高分子では、純粋結
晶の様な明確な融点はなく、或る広がりを持った融点を
示す。従って、示差熱分析(DTA)や示差走査熱分析
(DSC)等による熱分析の際のピーク温度が融点とな
る。また、ピークが複数でる事も有るが、この場合、本
発明の方法では主ピークを融点として扱えば良い。そし
て、ピークにはすそ野があり、これは試料中の微結晶の
中には主ピークの温度以下の温度で結晶の融解が起こる
ものを示すものだが、このすそ野の開始地点の温度がい
ずれかの微結晶の融解が開始する温度であり、すなわち
補外融解開始温度を、本発明では結晶融解温度として捉
える。The crystal melting temperature, which is the term used in the method for thermally laminating the crystalline thermoplastic resin sheet of the present invention, will be described. Generally in the case of pure crystals, the crystal melting temperature at which the solid state changes to the liquid state is a physical quantity that can be uniquely defined as the melting point. However, in the case of an ordinary crystalline polymer substance composed of a flexible molecular chain,
The solid state consists of an amorphous region and a crystalline region (microcrystal), and these microcrystals are in various aggregate states with different stable states due to various sizes, various internal defects, etc. , A crystalline (thermoplastic) polymer does not have a clear melting point like pure crystals, but shows a melting point with a certain spread. Therefore, the peak temperature during thermal analysis such as differential thermal analysis (DTA) or differential scanning calorimetry (DSC) is the melting point. Further, although there may be a plurality of peaks, in this case, the main peak may be treated as the melting point in the method of the present invention. And, there is a skirt area in the peak, which shows that some of the microcrystals in the sample cause melting of the crystal at a temperature below the temperature of the main peak. The temperature at which the melting of the microcrystals starts, that is, the extrapolation melting start temperature is regarded as the crystal melting temperature in the present invention.
【0020】以上は熱分析を前提とした話であったが、
これは温度−機械的特性(例えば弾性率E)との関係で
も同様なことが言える。これを図示したのが図2であ
る。図2は、樹脂シートの温度制御を結晶融解温度等に
注目して行う本発明の熱ラミネート方法と従来の熱ラミ
ネート方法を、樹脂の弾性率と温度との関係で対比した
説明図である。同図で横軸は温度T、縦軸は弾性率Eで
あり、Ccrysで指示される曲線が結晶性熱可塑性樹
脂の曲線を、Camorで指示される曲線が非晶性熱可
塑性樹脂の曲線を概念的に示したものである。非晶性の
熱可塑性樹脂では、弾性率は温度が上昇するにつれてガ
ラス転移点Tg付近で段差が生じて低下し、その後、徐
々に低下しながら、弾性率の低下度合いが増して融点T
m又は流動点(Tm)で急激に低下する。そして、樹脂
シートが熱ラミネートされるには、適度な粘着性と機械
的強度が必要であり、この結果、弾性率には加工適正上
限弾性率Euと加工適正下限弾性率Elとの間に、適正
加工弾性率範囲ΔEが存在する。一方、結晶性熱可塑性
樹脂Ccrysの場合には、弾性率は温度の上昇ととも
に、ガラス転移点Tgで若干の段差をともなって低下
し、その後、徐々に減少して、微結晶が融解が進行する
と共に弾性率の低下が激しくなり、融点で最も弾性率の
低下が激しくなり、その後、流動化していく。適正加工
弾性率範囲ΔEにおける弾性率の低下の度合いは、結晶
性熱可塑性樹脂は非晶性熱可塑性樹脂に比べて急峻であ
る為に、結晶性熱可塑性樹脂の適正加工温度範囲ΔTc
rysは非晶性熱可塑性樹脂の適正加工温度範囲ΔTa
morに比べて狭く、これが従来の熱ラミネート装置で
は結晶性熱可塑性樹脂シートを加工できない理由であ
る。The above is a premise of thermal analysis.
The same can be said with respect to the relationship between temperature and mechanical properties (for example, elastic modulus E). This is illustrated in FIG. FIG. 2 is an explanatory diagram comparing the thermal lamination method of the present invention in which the temperature control of the resin sheet is focused on the crystal melting temperature and the like with the conventional thermal lamination method in terms of the elastic modulus of the resin and the temperature. In the figure, the horizontal axis is temperature T and the vertical axis is elastic modulus E. The curve designated by Ccrys is the curve of the crystalline thermoplastic resin, and the curve designated by Camor is the curve of the amorphous thermoplastic resin. It is shown conceptually. In the amorphous thermoplastic resin, the elastic modulus decreases as a temperature rises due to a step near the glass transition point Tg, and then gradually decreases, and the degree of decrease of the elastic modulus increases and the melting point T increases.
m or pour point (Tm) drops sharply. In order for the resin sheet to be heat-laminated, appropriate adhesiveness and mechanical strength are required. As a result, the elastic modulus is between the proper upper limit elastic modulus of processing Eu and the proper lower limit elastic modulus of processing El. There is a proper processing elastic modulus range ΔE. On the other hand, in the case of the crystalline thermoplastic resin Ccrys, the elastic modulus decreases with a rise in temperature with a slight step at the glass transition point Tg, and then gradually decreases, and the fine crystals progress to melt. At the same time, the elastic modulus drops sharply, and the elastic modulus drops most at the melting point, and then fluidizes. The degree of decrease in the elastic modulus in the proper processing elastic modulus range ΔE is steeper than that of the amorphous thermoplastic resin, so that the appropriate processing temperature range ΔTc of the crystalline thermoplastic resin is
rys is a proper processing temperature range ΔTa of the amorphous thermoplastic resin.
It is narrower than mor, and this is the reason why the crystalline thermoplastic resin sheet cannot be processed by the conventional thermal laminating apparatus.
【0021】そこで、本発明の結晶性熱可塑性樹脂シー
トの熱ラミネート方法では、適正加工温度範囲ΔEを実
現する結晶性熱可塑性樹脂の適正加工温度範囲ΔTcr
ysから逸脱しても問題無く熱ラミネートを行うべく、
少なくとも2層の樹脂シートが粘着を発現して仮固定で
きるまで(最終的なラミネート接着力がなくてもまだ良
い)に加熱するために、微結晶が融解を開始しだす温度
として前記結晶融解温度以上に、接着面表面近傍側のみ
を加熱して仮ラミネートを行う。そして、接着とは関係
ない非接着面近傍側は温度を上げずに結晶融解温度未満
として、こちらの方で樹脂シートの強度を保たせる様に
するのである。従って接着面表面近傍の温度が例えば融
点以上に上昇し流動性が出たとしても、非接着面(裏
面)は結晶融解温度未満であり十分な強度を有し、又、
2層複合されている為、シートが大きく変形する事は無
い。一方、接着面表面近傍が例えば結晶融解温度未満に
下降しても、後の本ラミネート工程で接着力不足等は解
消される。その結果、ラミネートの適正加工温度範囲は
実質上大幅に拡大する。また、非接着面表面近傍を結晶
融解温度未満であるが加熱しておくのは、接着面側の加
熱を助ける為、また次の本ラミネートの予熱も兼ねてい
る。Therefore, in the method for thermally laminating a crystalline thermoplastic resin sheet according to the present invention, an appropriate processing temperature range ΔTcr of a crystalline thermoplastic resin that realizes an appropriate processing temperature range ΔE is obtained.
Even if it deviates from ys, in order to perform thermal lamination without problems,
In order to heat the resin sheet of at least two layers until it develops tackiness and can be temporarily fixed (it is not necessary to have the final laminating adhesive strength), the temperature at which the microcrystals start melting is equal to or higher than the crystal melting temperature. Then, only the surface near the bonding surface is heated to perform temporary lamination. The temperature on the non-bonding surface side, which is not related to bonding, is kept below the crystal melting temperature without raising the temperature so that the strength of the resin sheet can be maintained. Therefore, even if the temperature in the vicinity of the surface of the adhesive surface rises above the melting point and fluidity appears, the non-adhesive surface (rear surface) is below the crystal melting temperature and has sufficient strength.
Because it is a two-layer composite, the sheet does not deform significantly. On the other hand, even if the vicinity of the surface of the adhesive surface is lowered below the crystal melting temperature, for example, the insufficient adhesive force is eliminated in the subsequent main laminating step. As a result, the proper processing temperature range of the laminate is substantially expanded. In addition, heating the vicinity of the surface of the non-adhesive surface, which is lower than the crystal melting temperature, assists heating on the adhesive surface side, and also serves as preheating for the next main laminate.
【0022】そして、以上の様にして仮ラミネートが済
めば、後は、積層されたシート全体の熱歪み等を除去す
る為に、また、最終的なラミネート強度を出す為に、
(さらにエンボスの場合はエンボスする為に)、積層シ
ート全体を結晶融解温度以上に加熱する。この時も融点
未満の温度として積層シート全体の破断、変形、ガイド
ローラへの粘着を防止する。その後は、従来公知の熱ラ
ミネート同様に室温まで冷却することとなる。Then, after the temporary lamination is completed as described above, after that, in order to remove the thermal strain and the like of the entire laminated sheets and to obtain the final lamination strength,
(For embossing in the case of embossing), the entire laminated sheet is heated to the crystal melting temperature or higher. Also at this time, the temperature is lower than the melting point to prevent the entire laminated sheet from breaking, deforming, and sticking to the guide roller. After that, it is cooled to room temperature as in the conventionally known thermal lamination.
【0023】以上の様に、加圧積層を2段階に分けて行
う事で1段階で行う事に比べて、安定的に製造できる利
点がある。もしも、一段階で行おうとすれば、例えば図
1において、ラミネートロール5と圧胴6との間に、予
熱された2層の樹脂シートを供給する際に、他方のシー
トは右側から、もう片方のシートは左側からと斜めに供
給しなければならない。しかし、予熱された結晶性熱可
塑性樹脂シートの機械的強度は弱く不安定なので、斜め
からの供給ではシートを張力を与えて供給しないと自重
でたるみが生じるし、また張力を与えて供給すると延び
て破断が生じる。結局、真上から2層のシートを供給す
ることが必要となり、また2層のシートを隣接して供給
すれば、シートのバタツキにより予熱されたシートが粘
着により不意に接着したりして安定しない。従って、意
識的に且つ安定的に2層のシートを(仮)接着させてか
ら、ラミネートロールと圧胴との間に供給することが必
要となる。As described above, performing pressure lamination in two stages has the advantage that it can be manufactured more stably than performing it in one stage. If one step is to be performed, for example, in FIG. 1, when the preheated two-layer resin sheet is supplied between the laminating roll 5 and the impression cylinder 6, the other sheet is transferred from the right side to the other side. Sheets must be fed from the left and diagonally. However, the mechanical strength of the preheated crystalline thermoplastic resin sheet is weak and unstable, so if the sheet is fed obliquely, it will sag due to its own weight unless it is fed with tension, and if it is fed with tension, it stretches. Breaks. After all, it is necessary to supply a two-layer sheet from directly above, and if two-layer sheets are adjacently supplied, the sheet preheated due to the flapping of the sheet may be abruptly adhered due to adhesion, which is not stable. . Therefore, it is necessary to consciously and stably adhere the two layers of sheets (temporarily) and then supply the sheets between the laminating roll and the impression cylinder.
【0024】また、本発明の結晶性熱可塑性樹脂シート
の熱ラミネート方法は、積層する2層の樹脂シートの接
着面に熱融着性接着剤層が形成されていなくても、熱ラ
ミネートが可能であるが、熱融着性接着剤層が形成され
ている場合でも、上述の本発明の方法は拡張できる。そ
れは、熱融着性接着剤層の接着力発現温度と、熱融着性
接着剤層以外の樹脂シート部分の樹脂の結晶融解温度に
注目して、接着面側の表面近傍は前者の接着力発現温度
以上にして、非接着面側の表面近傍は後者の結晶融解温
度未満になる様にして最初の仮ラミネートを行う様にす
る。後の本ラミネートは前述と同様に、樹脂シートの樹
脂の結晶融解温度以上且つ融点以下の温度に積層された
両シートの両層を加熱して行えば良い。この場合、熱融
着性接着剤は熱で融着性を発現する接着剤であれば、ド
ライラミネート用接着剤等、従来公知のもので良く、特
に限定されない。また、接着力発現温度は、両シートの
結晶融解温度以上であっても、未満であっても支障は無
い。この様に、熱融着性接着剤層が形成された結晶性熱
可塑性樹脂シートは、単層ではなく最初から2層構成の
結晶性熱可塑性樹脂シートとして捉えることができ、こ
れら各層の、結晶融解温度、融点等の熱特性に注目して
熱ラミネートを行えば良いことになる。Further, according to the method for thermally laminating a crystalline thermoplastic resin sheet of the present invention, thermal lamination is possible even if a heat-fusible adhesive layer is not formed on the adhesive surfaces of the two layers of resin sheets to be laminated. However, the method of the present invention described above can be extended even when the heat-fusible adhesive layer is formed. That is, paying attention to the adhesive force expression temperature of the heat-fusible adhesive layer and the crystal melting temperature of the resin of the resin sheet portion other than the heat-fusible adhesive layer, the vicinity of the surface on the adhesive side is the adhesive force of the former. At the temperature above the expression temperature, the vicinity of the surface on the non-adhesive surface side is set below the crystal melting temperature of the latter so that the first temporary lamination is performed. The subsequent main lamination may be carried out by heating both layers of both sheets laminated at a temperature not lower than the crystal melting temperature of the resin of the resin sheet and not higher than the melting point, as in the above. In this case, the heat-fusible adhesive may be any conventionally known adhesive such as an adhesive for dry lamination as long as it is an adhesive that exhibits heat-fusible properties and is not particularly limited. Further, there is no problem if the adhesive force expression temperature is higher than or lower than the crystal melting temperature of both sheets. Thus, the crystalline thermoplastic resin sheet on which the heat-fusible adhesive layer is formed can be regarded as a crystalline thermoplastic resin sheet having a two-layer structure from the beginning, instead of a single layer. It suffices to perform thermal lamination by paying attention to thermal characteristics such as melting temperature and melting point.
【0025】[0025]
【実施例】以下、本発明の結晶性熱可塑性樹脂シートの
熱ラミネート方法を実施例で説明する。EXAMPLES The thermal laminating method for the crystalline thermoplastic resin sheet of the present invention will be described below with reference to examples.
【0026】図1に示す様な構成の熱ラミネート装置
で、ポリプロピレン製で厚さ100μmの樹脂シート
(結晶融解温度130℃、融点176℃)を2層用意
し、巻取から帯状連続シートとして供給して、熱ラミネ
ートを行った。加熱ロール21及び22の表面温度は1
40℃として結晶融解温度よりも高く設定し、また、圧
着ロール31及び32の表面温度は95℃として結晶融
解温度よりも低く設定し、さらに予熱用パネルヒータ4
1及び42により適量の赤外線を輻射し、加熱ロールの
接触を離れてから圧着ロールで2層のシートが圧着され
る迄の間の冷却を防止する。そして圧着ロール31及び
32による圧着直前の両シートの接着面の表面温度を1
40℃、非接触面の表面温度を95℃に保つ。以上の様
にして仮ラミネート工程が終了した積層シートは、圧着
ロール31及び32の間から垂直に下方に落として次の
本ラミネートの為の圧胴5及びラミネートロール6の間
に導かれる。その際、仮接着が行われた積層シートを両
面から別の予熱用パネルヒータ43及び44によって赤
外線輻射で加熱し、今度は両面の表面温度を、結晶融解
温度以上で融点よりも低い170℃に調整し、加熱直後
にラミネートロール5と圧胴6との間に積層シートが入
る様にして、本ラミネートを行う。ラミネートロール及
び圧胴は表面温度を60℃に設定し、その後、冷却ロー
ル71、72及び73により室温まで冷却する。冷却ロ
ールの表面温度は、ラミネートロールに近い方の上流側
から順に、40℃、30℃、25℃とする。なお、シー
トの送り速度は25m/minとした。Using a thermal laminator having a structure as shown in FIG. 1, two layers of polypropylene resin sheet (crystal melting temperature 130 ° C., melting point 176 ° C.) made of polypropylene are prepared and supplied as a strip-shaped continuous sheet from winding. Then, thermal lamination was performed. The surface temperature of the heating rolls 21 and 22 is 1
40 ° C. is set higher than the crystal melting temperature, the surface temperature of the pressure bonding rolls 31 and 32 is set to 95 ° C. lower than the crystal melting temperature, and the preheating panel heater 4 is used.
1 and 42 radiate an appropriate amount of infrared rays to prevent cooling from leaving the contact of the heating roll until the two-layer sheet is pressure-bonded by the pressure roll. The surface temperature of the adhesive surface of both sheets immediately before pressure bonding by the pressure rollers 31 and 32 is set to 1
The surface temperature of the non-contact surface is kept at 40 ° C and 95 ° C. The laminated sheet having undergone the temporary laminating step as described above is dropped vertically between the pressure bonding rolls 31 and 32 and guided between the impression cylinder 5 and the laminating roll 6 for the next main lamination. At that time, the laminated sheets that have been temporarily adhered are heated from both sides by infrared radiation by different preheating panel heaters 43 and 44, and this time the surface temperature of both sides is set to 170 ° C. which is higher than the crystal melting temperature and lower than the melting point. After the adjustment, the laminated sheet is inserted between the laminating roll 5 and the impression cylinder 6 immediately after heating, and the main lamination is performed. The surface temperature of the laminating roll and the impression cylinder is set to 60 ° C., and then cooled to room temperature by the cooling rolls 71, 72 and 73. The surface temperature of the cooling roll is 40 ° C., 30 ° C., and 25 ° C. from the upstream side closer to the laminating roll. The sheet feeding speed was 25 m / min.
【0027】また、上記で用いる熱ラミネート装置の各
構成要素は次の様なものである。加熱ロール21及び2
2は表面をクロムメッキした中空の鉄製ロールで空芯内
を高圧蒸気を通して加熱する。圧着ロール31及び32
は、片方は表面クロムメッキの中空鉄製ロールで空芯を
熱水を通して加熱し、もう片方は中空鉄製ロール表面を
シリコーンゴム層で被覆し、空芯内を熱水を通して加熱
する構造である。次に、予熱用パネルヒータ41、42
はニクロム線条電熱ヒータを、又、予熱パネルヒータ4
3、44は電熱加熱式のセラミックス面輻射ヒータをそ
れぞれ用いたもので輻射熱により加熱するものである。
また、ラミネートロール5は空芯の鉄製ロールで表面は
クロムメッキを行い鏡面平滑に仕上げてある。空芯内に
温水を循環させて加熱する。また、圧胴6は空芯鉄製ロ
ールの表面を硬度50°のシリコーンゴム層で被覆し、
空芯内には温水を循環させて加熱する構造である。そし
て、冷却ロール71〜73は空芯鉄製ロールで表面をク
ロムメッキで鏡面仕上げしたもので、空芯内を冷水を通
して冷却する構造である。The components of the thermal laminator used above are as follows. Heating rolls 21 and 2
2 is a hollow iron roll whose surface is chrome-plated, and heats the inside of the air core through high-pressure steam. Crimping rolls 31 and 32
One has a structure in which a hollow iron roll with a surface chrome plating heats the air core through hot water, and the other one coats the surface of the hollow iron roll with a silicone rubber layer and heats the inside of the air core through hot water. Next, the preheating panel heaters 41 and 42
Is a Nichrome wire electric heater, and is also a preheat panel heater 4
Reference numerals 3 and 44 respectively use electric heating type ceramic surface radiant heaters, which are heated by radiant heat.
Further, the laminating roll 5 is an iron core roll having an air core, and the surface thereof is plated with chrome and finished to have a mirror surface. Heat by circulating hot water in the air core. Further, the impression cylinder 6 covers the surface of an air-core iron roll with a silicone rubber layer having a hardness of 50 °,
The air core has a structure in which hot water is circulated for heating. The cooling rolls 71 to 73 are air-core iron rolls whose surfaces are mirror-finished by chrome plating, and have a structure for cooling the inside of the air-core by passing cold water.
【0028】[0028]
【発明の効果】本発明によれば、ポリオレフィン系素材
の様な結晶性を有する熱可塑性樹脂シートを、、熱融着
性接着剤を該樹脂シートに施すこと無く、充分な接着力
で効率良く、高速でなお且つシートの歪み、変形、破
断、ガイドローラとの粘着を防ぎつつ、ラミネート(ま
た、必要に応じてエンボスも)する事ができる。また、
加工条件、特にシート加熱条件のバラツキによる影響を
受けにくい。また、樹脂シートに熱融着性接着剤を施し
てある樹脂シートを用いる場合に於いても、該接着剤の
接着力発現温度如何にかかわらず樹脂シートの非接着面
近傍が結晶融解温度未満で仮ラミネート工程が行われる
為、シートの歪み、変形、破断、ガイドローラ等への粘
着の防止効果が特に高い。また、本ラミネート工程で結
晶融解温度以上に加熱して加圧圧接される為、両樹脂シ
ートの接着力の低下、残留応力(歪み)の発生は生じな
い。EFFECTS OF THE INVENTION According to the present invention, a thermoplastic resin sheet having crystallinity such as a polyolefin material can be efficiently provided with sufficient adhesive force without applying a heat-fusible adhesive to the resin sheet. It is possible to carry out lamination (and embossing if necessary) at high speed while preventing distortion, deformation, breakage of the sheet and adhesion with the guide roller. Also,
Less affected by variations in processing conditions, especially sheet heating conditions. Further, even when a resin sheet having a heat-fusible adhesive applied to the resin sheet is used, the temperature in the vicinity of the non-adhesive surface of the resin sheet is below the crystal melting temperature regardless of the adhesive force expression temperature of the adhesive. Since the temporary laminating step is performed, the effect of preventing distortion, deformation, breakage of the sheet, and adhesion to the guide roller and the like is particularly high. Further, in the present laminating step, since heating is performed at a temperature higher than the crystal melting temperature and pressure is applied, the adhesive force between both resin sheets is not reduced and residual stress (strain) does not occur.
【図1】本発明の結晶性熱可塑性樹脂シートの熱ラミネ
ート方法を実現し得る熱ラミネート装置の装置構成の一
例を示す概念図。FIG. 1 is a conceptual diagram showing an example of a device configuration of a thermal laminating device capable of realizing a thermal laminating method for a crystalline thermoplastic resin sheet of the present invention.
【図2】樹脂シートの温度制御を結晶融解温度等に注目
して行う本発明の熱ラミネート方法と従来の熱ラミネー
ト方法を、樹脂の弾性率と温度との関係で対比した説明
図。FIG. 2 is an explanatory diagram comparing the thermal laminating method of the present invention in which the temperature of a resin sheet is controlled by paying attention to the crystal melting temperature and the like and the conventional thermal laminating method in terms of the relationship between the elastic modulus of the resin and the temperature.
【図3】従来の熱可塑性樹脂シートの熱ラミネート方法
を行う熱ラミネート装置の装置構成の一例を示す概念
図。FIG. 3 is a conceptual diagram showing an example of a device configuration of a thermal laminating device for performing a conventional method for thermally laminating a thermoplastic resin sheet.
11〜13 巻取ロール 21、22 加熱ロール 31、32 圧着ロール 41〜44 予熱用パネルヒータ(非接触加熱) 5 ラミネートロール(又はエンボスロール) 6 圧胴 71〜73 冷却ロール 81a,81b 給紙側ニップロール(対) 82 排紙側ニップロール(対) 83 剥離ロール 91a〜91c 巻取ロール 92a、92b 予熱ロール 93 ヒートドラム 94a〜94c 予熱用パネルヒータ(非接触加熱) 95a〜95c 予熱ロール 96 エンボスロール 97 圧胴 98 冷却ロール Ccrys 結晶性熱可塑性樹脂 Camor 非晶性熱可塑性樹脂 E 弾性率 Eu 加工適正上限弾性率 El 加工適正下限弾性率 ΔE 適性加工弾性率範囲 Tc 結晶融解温度 Tg ガラス転移温度 Tm 融点又は流動温度 ΔTcrys 結晶性熱可塑性樹脂の適正加工温度範囲 ΔTamor 非晶性熱可塑性樹脂の適正加工温度範囲 S1 シート1 S2 シート2 11-13 Winding roll 21, 22 Heating roll 31, 32 Pressure bonding roll 41-44 Preheating panel heater (non-contact heating) 5 Laminating roll (or embossing roll) 6 Impression drum 71-73 Cooling roll 81a, 81b Paper feeding side Nip roll (pair) 82 Paper discharge side nip roll (pair) 83 Peeling roll 91a to 91c Winding roll 92a, 92b Preheating roll 93 Heat drum 94a to 94c Preheating panel heater (non-contact heating) 95a to 95c Preheating roll 96 Embossing roll 97 Impression cylinder 98 Cooling roll Ccrys Crystalline thermoplastic resin Camor Amorphous thermoplastic resin E Elastic modulus Eu Machining appropriate upper limit elastic modulus El Machining proper lower limit elastic modulus ΔE Suitable machining elastic modulus range Tc Crystal melting temperature Tg Glass transition temperature Tm Melting point or Flow temperature ΔTcrys Crystalline thermoplastic Proper processing temperature range of proper processing temperature range ΔTamor amorphous thermoplastic resin of the resin S1 sheet 1 S2 sheet 2
Claims (2)
着により積層、接着する熱ラミネート方法であって、 (a) 該樹脂シートの各々の接着面に熱融着性接着剤層を
形成せずに、該2層の樹脂シートを、各々の接着面表面
近傍が該樹脂シートの樹脂の結晶融解温度以上に、また
各々の非接着面の表面近傍が該樹脂シートの樹脂の結晶
融解温度未満になる様に加熱し、 (b) 次いで、該2層の樹脂シートを、その接着面同士が
対面するような向きで両面から加圧積層し、 (c) 次いで、該2層の樹脂シートの両層を共に、該樹脂
シートの樹脂の結晶融解温度以上で且つ融点未満にまで
加熱させ、 (d) 次いで、該2層の樹脂シートを両面から加圧し、そ
して該2層の樹脂シートを結晶融解温度未満にまで冷却
し、 (e) 次いで、該2層の樹脂シートを室温にまで冷却す
る、工程からなることを特徴とする、結晶性熱可塑性樹
脂シートの熱ラミネート方法。1. A thermal laminating method for laminating and adhering two layers of crystalline thermoplastic resin sheets by thermal fusion bonding, comprising: (a) forming a thermally fusible adhesive layer on each adhesive surface of the resin sheet. Without forming the two-layer resin sheet, the vicinity of the surface of each adhesive surface is above the crystal melting temperature of the resin of the resin sheet, and the vicinity of the surface of each non-adhesive surface is the crystal melting of the resin of the resin sheet. (B) Next, the two-layer resin sheet is pressure-laminated from both sides in such a direction that the adhesive surfaces face each other, and (c) then the two-layer resin sheet is heated. Both layers of the sheet are heated together to above the crystal melting temperature of the resin of the resin sheet and below the melting point, (d) then the two-layer resin sheet is pressed from both sides, and the two-layer resin sheet Is cooled to below the crystal melting temperature, and (e) then the two-layer resin sheet is brought to room temperature. In cooling, characterized by comprising the steps, the crystalline thermoplastic resin sheets thermally laminated methods.
着により積層、接着する熱ラミネート方法であって、 (a) 該樹脂シートの各々の接着面に接着力発現温度が該
樹脂シートの樹脂の結晶融解温度未満である熱融着性接
着剤層を形成したものを用意し、該2層の樹脂シート
を、各々の接着面表面近傍が上記接着剤の接着力発現温
度以上に、また各々の非接着面の表面近傍が該樹脂シー
トの樹脂の結晶融解温度未満になる様に加熱し、 (b) 次いで、該2層の樹脂シートを、その接着面同士が
対面するような向きで両面から加圧積層し、 (c) 次いで、該2層の樹脂シートの両層を共に、該樹脂
シートの樹脂の結晶融解温度以上で且つ融点未満にまで
加熱させ、 (d) 次いで、該2層の樹脂シートを両面から加圧し、そ
して該2層の樹脂シートを結晶融解温度未満にまで冷却
し、 (e) 次いで、該2層の樹脂シートを室温にまで冷却す
る、工程からなることを特徴とする、結晶性熱可塑性樹
脂シートの熱ラミネート方法。2. A thermal laminating method for laminating and adhering two layers of crystalline thermoplastic resin sheets by heat fusion, which comprises: (a) the resin sheet having an adhesive force developing temperature on each adhesive surface of the resin sheet. A resin having a heat-fusible adhesive layer having a temperature lower than the crystal melting temperature of the resin is prepared, and the resin sheet of the two layers is formed such that the adhesive surface temperature of each adhesive surface is equal to or higher than the adhesive force expression temperature of the adhesive. Also, heating is performed so that the vicinity of the surface of each non-adhesive surface becomes lower than the crystal melting temperature of the resin of the resin sheet, and (b) then, the two-layer resin sheet is oriented so that the adhesive surfaces face each other. (C) Next, both layers of the two-layer resin sheet are heated to above the crystal melting temperature of the resin of the resin sheet and below the melting point, and (d) The two-layer resin sheet is pressed from both sides, and the two-layer resin sheet is crystallized. Cooled to below the temperature, (e) Next, the resin sheet of the second layer is cooled to room temperature, characterized by comprising the steps, the crystalline thermoplastic resin sheets thermally laminated methods.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP34819395A JP3813223B2 (en) | 1995-12-19 | 1995-12-19 | Thermal lamination method for crystalline thermoplastic resin sheet |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP34819395A JP3813223B2 (en) | 1995-12-19 | 1995-12-19 | Thermal lamination method for crystalline thermoplastic resin sheet |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH09169055A true JPH09169055A (en) | 1997-06-30 |
JP3813223B2 JP3813223B2 (en) | 2006-08-23 |
Family
ID=18395379
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP34819395A Expired - Fee Related JP3813223B2 (en) | 1995-12-19 | 1995-12-19 | Thermal lamination method for crystalline thermoplastic resin sheet |
Country Status (1)
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JP (1) | JP3813223B2 (en) |
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