TW201827233A - Composite sheet manufacturing method and manufacturing apparatus - Google Patents

Composite sheet manufacturing method and manufacturing apparatus Download PDF

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Publication number
TW201827233A
TW201827233A TW106144542A TW106144542A TW201827233A TW 201827233 A TW201827233 A TW 201827233A TW 106144542 A TW106144542 A TW 106144542A TW 106144542 A TW106144542 A TW 106144542A TW 201827233 A TW201827233 A TW 201827233A
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TW
Taiwan
Prior art keywords
sheet
manufacturing
composite sheet
ultrasonic
sheet according
Prior art date
Application number
TW106144542A
Other languages
Chinese (zh)
Other versions
TWI742214B (en
Inventor
黑目圭介
松永竜二
森田進之介
齊藤数馬
Original Assignee
日商花王股份有限公司
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority claimed from JP2017237899A external-priority patent/JP7084130B2/en
Application filed by 日商花王股份有限公司 filed Critical 日商花王股份有限公司
Publication of TW201827233A publication Critical patent/TW201827233A/en
Application granted granted Critical
Publication of TWI742214B publication Critical patent/TWI742214B/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/08Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
    • B29C65/083Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations using a rotary sonotrode or a rotary anvil
    • B29C65/086Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations using a rotary sonotrode or a rotary anvil using a rotary anvil
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61FFILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
    • A61F13/00Bandages or dressings; Absorbent pads
    • A61F13/15Absorbent pads, e.g. sanitary towels, swabs or tampons for external or internal application to the body; Supporting or fastening means therefor; Tampon applicators
    • A61F13/15577Apparatus or processes for manufacturing
    • A61F13/15699Forming webs by bringing together several webs, e.g. by laminating or folding several webs, with or without additional treatment of the webs
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61FFILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
    • A61F13/00Bandages or dressings; Absorbent pads
    • A61F13/15Absorbent pads, e.g. sanitary towels, swabs or tampons for external or internal application to the body; Supporting or fastening means therefor; Tampon applicators
    • A61F13/51Absorbent pads, e.g. sanitary towels, swabs or tampons for external or internal application to the body; Supporting or fastening means therefor; Tampon applicators characterised by the outer layers
    • A61F13/511Topsheet, i.e. the permeable cover or layer facing the skin
    • A61F13/51104Topsheet, i.e. the permeable cover or layer facing the skin the top sheet having a three-dimensional cross-section, e.g. corrugations, embossments, recesses or projections
    • AHUMAN NECESSITIES
    • A61MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • A61FFILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; DEVICES PROVIDING PATENCY TO, OR PREVENTING COLLAPSING OF, TUBULAR STRUCTURES OF THE BODY, e.g. STENTS; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS
    • A61F13/00Bandages or dressings; Absorbent pads
    • A61F13/15Absorbent pads, e.g. sanitary towels, swabs or tampons for external or internal application to the body; Supporting or fastening means therefor; Tampon applicators
    • A61F13/51Absorbent pads, e.g. sanitary towels, swabs or tampons for external or internal application to the body; Supporting or fastening means therefor; Tampon applicators characterised by the outer layers
    • A61F13/511Topsheet, i.e. the permeable cover or layer facing the skin
    • A61F13/5116Topsheet, i.e. the permeable cover or layer facing the skin being formed of multiple layers
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00Shaping by thermoforming, i.e. shaping sheets or sheet like preforms after heating, e.g. shaping sheets in matched moulds or by deep-drawing; Apparatus therefor
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/08Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using ultrasonic vibrations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/02Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure
    • B29C65/18Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by heating, with or without pressure using heated tools
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/72Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by combined operations or combined techniques, e.g. welding and stitching
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/74Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area
    • B29C65/743Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc
    • B29C65/7437Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc the tool being a perforating tool
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/74Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area
    • B29C65/743Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc
    • B29C65/7443Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor by welding and severing, or by joining and severing, the severing being performed in the area to be joined, next to the area to be joined, in the joint area or next to the joint area using the same tool for both joining and severing, said tool being monobloc or formed by several parts mounted together and forming a monobloc by means of ultrasonic vibrations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C65/00Joining or sealing of preformed parts, e.g. welding of plastics materials; Apparatus therefor
    • B29C65/78Means 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
    • B29C65/7841Holding or clamping means for handling purposes
    • B29C65/7847Holding or clamping means for handling purposes using vacuum to hold at least one of the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/004Preventing sticking together, e.g. of some areas of the parts to be joined
    • B29C66/0042Preventing sticking together, e.g. of some areas of the parts to be joined of the joining tool and the parts to be joined
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/006Preventing damaging, e.g. of the parts to be joined
    • B29C66/0062Preventing damaging, e.g. of the parts to be joined of the joining tool, e.g. avoiding wear of the joining tool
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/02Preparation of the material, in the area to be joined, prior to joining or welding
    • B29C66/024Thermal pre-treatments
    • B29C66/0242Heating, or preheating, e.g. drying
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/11Joint 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
    • B29C66/112Single lapped joints
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/10Particular design of joint configurations particular design of the joint cross-sections
    • B29C66/13Single flanged joints; Fin-type joints; Single hem joints; Edge joints; Interpenetrating fingered joints; Other specific particular designs of joint cross-sections not provided for in groups B29C66/11 - B29C66/12
    • B29C66/131Single flanged joints, i.e. one of the parts to be joined being rigid and flanged in the joint area
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/01General aspects dealing with the joint area or with the area to be joined
    • B29C66/05Particular design of joint configurations
    • B29C66/20Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines
    • B29C66/21Particular design of joint configurations particular design of the joint lines, e.g. of the weld lines said joint lines being formed by a single dot or dash or by several dots or dashes, i.e. spot joining or spot welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/50General aspects of joining tubular articles; General aspects of joining long products, i.e. bars or profiled elements; General aspects of joining single elements to tubular articles, hollow articles or bars; General aspects of joining several hollow-preforms to form hollow or tubular articles
    • B29C66/51Joining tubular articles, profiled elements or bars; Joining single elements to tubular articles, hollow articles or bars; Joining several hollow-preforms to form hollow or tubular articles
    • B29C66/53Joining single elements to tubular articles, hollow articles or bars
    • B29C66/534Joining single elements to open ends of tubular or hollow articles or to the ends of bars
    • B29C66/5346Joining single elements to open ends of tubular or hollow articles or to the ends of bars said single elements being substantially flat
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/70General 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
    • B29C66/73General 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
    • B29C66/739General 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
    • B29C66/7392General 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
    • B29C66/73921General 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/812General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • B29C66/8122General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps characterised by the composition of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/812General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • B29C66/8126General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps characterised by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • B29C66/81261Thermal properties, e.g. thermal conductivity, thermal expansion coefficient
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/812General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • B29C66/8126General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the composition, by the structure, by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps characterised by the intensive physical properties or by the optical properties of the material constituting the pressing elements, e.g. constituting the welding jaws or clamps
    • B29C66/81264Mechanical properties, e.g. hardness
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/814General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps
    • B29C66/8141General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined
    • B29C66/81433General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the design of the pressing elements, e.g. of the welding jaws or clamps characterised by the surface geometry of the part of the pressing elements, e.g. welding jaws or clamps, coming into contact with the parts to be joined being toothed, i.e. comprising several teeth or pins, or being patterned
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B29WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29CSHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C66/00General aspects of processes or apparatus for joining preformed parts
    • B29C66/80General aspects of machine operations or constructions and parts thereof
    • B29C66/81General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps
    • B29C66/818General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the cooling constructional aspects, or by the thermal or electrical insulating or conducting constructional aspects of the welding jaws or of the clamps ; comprising means for compensating for the thermal expansion of the welding jaws or of the clamps
    • B29C66/8183General aspects of the pressing elements, i.e. the elements applying pressure on the parts to be joined in the area to be joined, e.g. the welding jaws or clamps characterised by the cooling constructional aspects, or by the thermal or electrical insulating or conducting constructional aspects of the welding jaws or of the clamps ; comprising means for compensating for the thermal expansion of the welding jaws or of the clamps characterised by the thermal conducting constructional aspects
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    • B29C66/91931Measuring 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
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    • B29K2105/00Condition, form or state of moulded material or of the material to be shaped
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    • B29L2031/00Other particular articles
    • B29L2031/48Wearing apparel
    • B29L2031/4871Underwear
    • B29L2031/4878Diapers, napkins

Abstract

A composite sheet manufacturing method is provided with: a step of introducing a first sheet (1) into a meshing part (33) and deforming the first sheet (1) into a concavo-convex shape while rotating a first roll (31) and a second roll (32) having meshing concavities and convexities on peripheral surface parts thereof; a step of conveying the first sheet (1), deformed into the concavo-convex shape, while carrying the same on the first roll (31), and overlapping a second sheet (2) with the first sheet (1) being conveyed; and a step of sandwiching the overlapped sheets (1 and 2) between a convex part (35) of the first roll (31) and an ultrasonic horn (42) of a ultrasonic welding machine, and applying ultrasonic vibrations. During the application of the ultrasonic vibrations in the ultrasonic treatment step, a welded part (4) having a through-hole (14) is formed.

Description

複合片材之製造方法及製造裝置Method and device for manufacturing composite sheet

本發明係關於一種複合片材之製造方法及製造裝置。The invention relates to a method and a device for manufacturing a composite sheet.

作為拋棄式尿布或經期衛生棉等吸收性物品之表面片材,已知有於與穿著者之肌膚抵接之面形成有凹凸者。 例如,本申請人提出一種複合片材,其具有第1及第2片材熔合之多個熔合部,且第1片材中之除熔合部以外之部分形成向與第2片材側為相反側突出的凸部。該複合片材由於在表面形成有凹凸,故而肌膚觸感或液體之擴散防止性優異。 又,亦已知有於此種複合片材中之熔合部形成貫通孔而提高液體之引入性等(參照專利文獻1、2)。於專利文獻2中,亦記載有為了形成具有貫通孔之熔合部,而於凹凸輥之凸部之前端部,設置有於與周圍之肩部之間具有階差之開孔形成用之小凸部,將2片片材夾於該小凸部與砧輥之間進行加熱而形成具有開孔之熔合部。 [先前技術文獻] [專利文獻] 專利文獻1:日本專利特開2006-175688號公報 專利文獻2:日本專利特開2006-175689號公報As a surface sheet of an absorbent article such as a disposable diaper or a menstrual tampon, it is known that an unevenness is formed on a surface abutting on the wearer's skin. For example, the present applicant proposes a composite sheet having a plurality of fused portions where the first and second sheets are fused, and a portion other than the fused portion of the first sheet is formed to be opposite to the second sheet side Projections protruding sideways. Since this composite sheet has irregularities formed on the surface, it has excellent skin feel and prevention of liquid diffusion. It is also known to form a through hole in a fused portion in such a composite sheet to improve liquid introduction properties and the like (see Patent Documents 1 and 2). In Patent Document 2, it is also described that in order to form a fused portion having a through hole, a small protrusion for forming an opening having a step difference from the surrounding shoulder portion is provided at the front end portion of the convex portion of the uneven roller. The two sheets are sandwiched between the small convex portion and the anvil roll and heated to form a fused portion having an opening. [Prior Art Literature] [Patent Literature] Patent Literature 1: Japanese Patent Laid-Open No. 2006-175688 Patent Literature 2: Japanese Patent Laid-Open No. 2006-175689

本發明為一種複合片材之製造方法,該複合片材具有第1片材及第2片材熔合之多個熔合部,且上述第1片材中之除上述熔合部以外之部分之至少一部分形成向與上述第2片材側為相反側突出之凸部。該複合片材之製造方法具備:賦形步驟,其一面使於周面部具有相互嚙合之凹凸之第1輥及第2輥旋轉,一面將上述第1片材導入至該等兩輥之嚙合部而使之變形為凹凸形狀;重疊步驟,其將變形為凹凸形狀之上述第1片材一面保持於上述第1輥上一面搬送,且使上述第2片材重疊於搬送中之上述第1片材;及超音波處理步驟,其將重疊之兩個片材夾於上述第1輥之凸部與超音波熔合機之超音波焊頭之間而施加超音波振動。於上述超音波處理步驟中,於該超音波振動之施加時,形成具有貫通孔之上述熔合部。 又,本發明為一種複合片材之製造裝置,該複合片材具有第1片材及第2片材熔合之多個熔合部,且上述第1片材中之除上述熔合部以外之部分之至少一部分形成向與上述第2片材側為相反側突出之凸部。該複合片材之製造裝置具備:凹凸賦形部,其具有於周面部具有相互嚙合之凹凸之第1輥及第2輥,且使導入至該等兩輥之嚙合部之上述第1片材變形為凹凸形狀;及超音波處理部,其具備超音波熔合機,且於使上述第2片材重疊於變形為凹凸形狀之狀態之上述第1片材上之後,將該等兩個片材夾於上述第1輥之凸部與上述超音波熔合機之超音波焊頭之間而局部地施加超音波振動,形成具有貫通孔之上述熔合部。The present invention is a method for manufacturing a composite sheet, the composite sheet having a plurality of fused portions where the first sheet and the second sheet are fused, and at least a part of the first sheet except for the fused portion A convex portion is formed to protrude to the side opposite to the second sheet side. The manufacturing method of the composite sheet is provided with a forming step of rotating the first roller and the second roller that have irregularities that engage with each other on the peripheral surface, and introducing the first sheet to the meshing portion of the two rollers while rotating. And deforming it into a concave-convex shape; in the overlapping step, the first sheet deformed into the concave-convex shape is conveyed while being held on the first roller, and the second sheet is superimposed on the first sheet being conveyed And an ultrasonic processing step of sandwiching the two overlapping sheets between the convex portion of the first roller and the ultrasonic welding head of the ultrasonic fusion machine to apply ultrasonic vibration. In the above-mentioned ultrasonic processing step, when the ultrasonic vibration is applied, the fused portion having a through hole is formed. In addition, the present invention is a device for manufacturing a composite sheet, the composite sheet having a plurality of fusion portions where the first sheet and the second sheet are fused, and a portion of the first sheet other than the fusion portion At least a part is formed with a convex portion protruding to a side opposite to the second sheet side. The manufacturing apparatus of this composite sheet is provided with a concave-convex forming portion having a first roller and a second roller having convex and concave portions that mesh with each other on a peripheral surface portion, and the first sheet introduced into the meshing portion of the two rollers. Deformed into a concave-convex shape; and an ultrasonic processing unit including an ultrasonic fusion machine, and after superimposing the second sheet on the first sheet deformed into a concave-convex shape, the two sheets It is sandwiched between the convex part of the said 1st roll and the ultrasonic welding head of the said ultrasonic fusion machine, and ultrasonic vibration is applied locally, and the said fusion | melting part which has a through-hole is formed.

於製造複合片材時,若利用不同之步驟進行熔合部之形成與貫通孔之形成,則有於熔合部之位置與貫通孔之位置之間產生位置偏移之情形,又,專利文獻2中所記載之於凸部之前端部設置小凸部之方法中,小凸部容易磨損,維護負擔較大等方面有改善之餘地。 因此,本發明係關於一種可消除先前技術所具有之解決問題之複合片材之製造方法及製造裝置。 以下,基於本發明之較佳之實施形態,一面參照圖式一面對本發明進行說明。 首先,一面參照圖1,一面對藉由本發明之複合片材之製造方法或製造裝置而製造之複合片材進行說明。 圖1所示之複合片材10係藉由本發明之複合片材之製造方法或製造裝置而製造之複合片材之一例,如圖1所示,具有第1片材1及第2片材2熔合之多個熔合部4,且第1片材1中之除熔合部4以外之部分之至少一部分形成向與第2片材2側為相反側突出之凸部5。 複合片材10較佳地用作吸收性物品之表面片材等。於用作吸收性物品之表面片材時,第1片材1形成朝向穿著者之肌膚側之面(以下,亦稱為肌膚對向面),第2片材2形成於穿著時朝向吸收體側之面(以下,亦稱為非肌膚對向面)。 凸部5及熔合部4於與複合片材10之面平行之一方向即圖1中之X方向,交替地且以形成一行之方式配置,此種行於與複合片材10之面平行且與上述一方向正交之方向即圖1中之Y方向形成為多行。相互鄰接之行中之凸部5及熔合部4分別於X方向偏移配置,更具體而言,偏移半個間距而配置。 於複合片材10中,上述Y方向與製造時之行進方向(MD,機械方向)一致,上述X方向與和製造時之行進方向正交之方向(CD)一致。 第1片材1及第2片材2包括片材材料。作為片材材料,例如可使用不織布、織布及針織布等纖維片材或膜等,自肌膚觸感等觀點而言,較佳為使用纖維片材,特佳為使用不織布。構成第1片材1與第2片材2之片材材料之種類既可相同,或者亦可不同。 作為使用不織布作為構成第1片材1及第2片材2之片材材料之情形時之不織布,例如,可列舉熱風不織布、紡黏不織布、水刺不織布、熔噴不織布、樹脂黏合劑不織布、針刺不織布等。亦可使用將該等不織布組合2種以上而成之積層體、或將該等不織布與膜等組合而成之積層體。用作構成第1片材1及第2片材2之片材材料之不織布之基重較佳為10 g/m2 以上,更佳為15 g/m2 以上,又較佳為40 g/m2 以下,更佳為35 g/m2 以下。不織布之基重較佳為10 g/m2 以上且40 g/m2 以下,更佳為15 g/m2 以上且35 g/m2 以下。 作為構成不織布之纖維,可使用包括各種熱塑性樹脂之纖維。作為不織布以外之片材材料,構成纖維或構成樹脂亦可較佳地使用包括各種熱塑性樹脂者。 作為熱塑性樹脂,可列舉聚乙烯、聚丙烯、聚丁烯等聚烯烴、聚對苯二甲酸乙二酯、聚對苯二甲酸丁二酯等聚酯、尼龍6、尼龍66等聚醯胺、聚丙烯酸、聚甲基丙烯酸烷基酯、聚氯乙烯、聚偏二氯乙烯等。該等樹脂可將1種單獨使用或作為2種以上之摻合物使用。又,可以芯鞘型或並列型等複合纖維之形態使用。 複合片材10如圖1所示,於第1片材1側之面,於X方向及Y方向之兩個方向具有夾於凸部5之多個凹部3,於各個凹部3之底部,形成有具有貫通孔14之熔合部4。若整體觀察,則複合片材10於第1片材1側之面具有包含上述凹部3與上述凸部5之起伏較大之凹凸,第2片材2側之面平坦,或成為相對於第1片材1側之面而起伏相對較小之大致平坦面。 複合片材10中之各個熔合部4如圖2所示,具有於上述Y方向較長之大致長方形狀之俯視形狀,於各者之內側,形成有俯視形狀為大致長方形狀之貫通孔14。換言之,各個熔合部4形成為包圍貫通孔14之環狀。貫通孔14較佳為於一個熔合部4僅形成有一個,且較佳為形成於在與熔合部4之位置之關係中預先決定之特定位置。又,貫通孔14係俯視形狀既可與熔合部4之外周緣之俯視形狀為相似形亦可為不相似形,但較佳為相似形。 於熔合部4中,藉由構成第1片材1及第2片材2之至少一者之熱熔合性樹脂熔融固化而使第1片材1與第2片材2結合。於第1片材1及第2片材2包括不織布等纖維片材之情形時,於熔合部4中,第1片材1及第2片材2之構成纖維較佳為熔融或埋沒至熔融之樹脂,無法利用目視觀察纖維狀之形態,即成為外觀上膜化之狀態。 其次,對本發明之複合片材之製造方法之第1實施態樣進行說明。 於第1實施態樣中,使用圖3所示之第1實施形態之複合片材之製造裝置20,製造上述複合片材10。 若對圖3所示之複合片材之製造裝置20進行說明,則複合片材之製造裝置20具備凹凸賦形部30、超音波處理部40、及預熱機構6,該預熱機構6將施加超音波振動之前之片材預熱至所控制之特定溫度。 凹凸賦形部30如圖3所示,具有於周面部具有相互嚙合之凹凸之第1及第2輥31、32,且藉由一面使兩輥31、32旋轉,一面將第1片材1導入至該等兩輥31、32之嚙合部33,而將第1片材1變形為沿著第1輥31之周面部之凹凸之形狀之凹凸形狀。 圖4係將第1輥31之主要部分放大表示之立體圖。於圖4中表示了第1輥31之周面部之一部分。 第1輥31係將具有特定齒寬之正齒輪31a、31b、・・組合複數片而形成為輥狀者。各齒輪之齒形成第1輥31之周面部中之凹凸形狀之凸部35,該凸部35之前端面35c成為於與下述超音波熔合機41之超音波焊頭42之前端面42t之間,對作為熔合對象之第1及第2片材1、2進行加壓之加壓面。 各齒輪之齒寬(齒輪之軸向之長度)決定複合片材10之凸部5中之上述X方向之尺寸,各齒輪之齒之厚度(齒輪之旋轉方向之長度)決定複合片材10之凸部5中之上述Y方向之尺寸。相鄰之齒輪係以其齒之間距分別偏移半個間距之方式組合。其結果,第1輥31之周面部成為凹凸形狀。於本實施形態中,各凸部35之前端面35c成為第1輥31之旋轉方向為長邊、軸向為短邊之矩形狀。若前端面35c為旋轉方向較長之形狀,則可使第1輥31之凸部35之一者與超音波焊頭42之前端面42t之接觸時間變長而容易提高溫度,故而較佳。 第1輥31中之各齒輪之齒槽部形成第1輥31之周面上之凹凸之凹部。於各齒輪之齒槽部之底部形成有抽吸孔34。抽吸孔34連通於鼓風機或真空泵等抽吸源(未圖示),以於自第1輥31與第2輥32之嚙合部33至第1片材1與第2片材2之合流部為止之間進行抽吸的方式被控制。因此,藉由第1輥31與第2輥32之嚙合而變形為凹凸形狀之第1片材1,以藉由抽吸孔34之抽吸力而維持於變形為沿著第1輥31之凹凸之形狀之狀態的狀態,搬送至第1片材1與第2片材2之合流部及利用超音波熔合機之超音波振動之施加部36。 於該情形時,如圖4所示,若於相鄰之齒輪間設置有特定空隙G,則可抑制對第1片材1施加過度之伸長力,或因兩輥31、32之嚙合部33而將第1片材1切斷,從而可使第1片材1變形為沿著第1輥31之周面之形狀,故而較佳。 第2輥32於周面部具有與第1輥31之周面部之凹凸相互嚙合之凹凸形狀。第2輥32除了不具有抽吸孔34以外,具有與第1輥31相同之構成。而且,一面使具有相互嚙合之凹凸之第1及第2輥31、32旋轉,一面將第1片材1導入至兩輥31、32之嚙合部33,藉此可使第1片材1變形為凹凸形狀。於嚙合部33中,第1片材1之複數個部位被第2輥32之凸部壓入至第1輥31之周面部之凹部,該被壓入之部分成為所製造之複合片材10之凸部5。於第2輥32之周面部,形成有插入至第1輥31之凹部之複數個凸部,但並非必須於第2輥32形成有與第1輥31之凹部全部對應之凸部。 超音波處理部40如圖3所示,具備有具備超音波焊頭42之超音波熔合機41,使第2片材2重疊於變形為凹凸形狀之狀態之第1片材1上之後,將該等兩個片材夾於第1輥31之凸部與超音波焊頭42之間而局部地施加超音波振動,形成具有貫通孔14之熔合部4。 超音波熔合機41如圖3及圖5所示,具備超音波振盪器(未圖示)、轉換器43、加速器44及超音波焊頭42。超音波振盪器(未圖示)與轉換器43電性地連接,藉由超音波振盪器而產生之頻率15 kHz~50 kHz左右之波長的高電壓之電信號輸入至轉換器43。超音波振盪器(未圖示)設置於可動台45上或可動台45外。 轉換器43內置壓電元件等壓電元件,將自超音波振盪器輸入之電信號藉由壓電元件而轉換為機械性振動。加速器44對自轉換器43發出之機械性振動之振幅調整,較佳為加以放大並傳遞至超音波焊頭42。超音波焊頭42由鋁合金或鈦合金等金屬塊形成,且以按照所使用之頻率正確地共振之方式設計。自加速器44傳遞至超音波焊頭42之超音波振動於超音波焊頭42之內部放大或衰減後,施加至作為熔合對象之第1及第2片材1、2。作為該超音波熔合機41,可將市售之超音波焊頭、轉換器、加速器、超音波振盪器組合使用。 超音波熔合機41固定於可動台45上,藉由使可動台45之位置朝向接近於第1輥31之周面之方向進退,能夠調節超音波焊頭42之前端面42t與第1輥31之凸部35之前端面35c之間之間隙、及對積層之第1及第2片材1、2之加壓力。 而且,藉由一面夾於第1輥31之凸部35之前端面35c與超音波熔合機41之超音波焊頭42之前端面42t之間而加壓,一面對作為熔合對象之第1及第2片材1、2施加超音波振動,而第1片材1中之位於凸部35之前端面35c上之部分之各者熔合於第2片材2,形成熔合部4,並且將貫通兩個片材1、2之貫通孔14形成為由熔融部分包圍之狀態。 於較佳之實施形態中,複合片材之製造裝置20具備具有配置於第1輥31內之加熱器61之預熱機構6。更具體而言,具備配置於第1輥31內之加熱器61等加熱機構、能夠測量施加超音波振動之前之片材之溫度的測溫機構(未圖示)、及基於測溫機構之測定值控制加熱器61之溫度之溫度控制部(未圖示)。藉由基於測溫機構之測定值,控制由加熱器61進行之第1輥31之周面部之加熱溫度,可將即將施加超音波振動之前之第1片材1之溫度高精度地控制為所期望之溫度。 於較佳之實施形態中,加熱器61沿著其軸長方向嵌入至第1輥31。又,加熱器61係於第1輥31之旋轉軸之周圍中之外周部之附近,於圓周方向設置間隔而配置有複數個。由加熱器61進行之第1輥31之周面部之加熱溫度藉由未圖示之溫度控制部而控制,可將複合片材之製造裝置20之運轉中導入至超音波振動之施加部36的第1片材1之溫度維持為特定範圍之溫度。 預熱機構6較佳為具備自外部對加熱對象物施加熱能而加熱之加熱機構。作為加熱機構,例如,可列舉使用電熱線之匣式加熱器等,但並不限定於此,可無特別限制地使用各種公知之加熱機構。 超音波熔合機係對熔合對象物施加超音波振動,由此使熔合對象物發熱及熔融而熔合者,不包含此處所言及之加熱機構。 於本發明之第1實施形態之製造方法中,如圖3所示,一面使第1及第2輥31、32旋轉,一面將自原料片輥(未圖示)捲出之第1片材1導入至該等兩輥31、32之嚙合部33而使之變形為凹凸形狀(賦形步驟)。然後,將變形為凹凸形狀之第1片材1一面保持於第1輥31上一面搬送,使自與第1片材1不同之原料片輥(未圖示)捲出之第2片材2重疊於搬送中之第1片材1(重疊步驟)。然後,將該重疊之兩個片材1、2夾於第1輥31之凸部35與超音波熔合機之超音波焊頭42之間而施加超音波振動(超音波處理步驟)。於超音波處理步驟中,於超音波振動之施加時,形成具有貫通孔14之熔合部4。 於第1實施形態之製造方法中,較佳為,於該超音波振動之施加之前,將第1片材1及第2片材2之至少一者預先加熱至未達該片材之熔點、且較該熔點低50℃之溫度以上。即,較佳為,於超音波振動之施加之前,進行以下之(1)及(2)之任一者或兩者。 (1)將第1片材1預先加熱至未達該第1片材之熔點、且較該熔點低50℃之溫度以上。 (2)將第2片材2預先加熱至未達該第2片材之熔點、且較該熔點低50℃之溫度以上。 較佳為,將第1片材1預先加熱至未達該第1片材之熔點、且較該熔點低50℃之溫度以上,並且將第2片材2預先加熱至未達該第2片材之熔點、且較該熔點低50℃之溫度以上。 作為使第1片材1為未達第1片材1之熔點、且較該熔點低50℃之溫度以上之方法,例如,於第1及第2輥31、32之嚙合部33與由超音波熔合機進行之超音波振動之施加部36之間,測定第1輥31上之第1片材1之溫度,且以其測定值成為上述特定範圍內之方式,控制第1輥31之周面部之溫度。作為使第1片材1預熱至特定範圍之溫度之方法,可代替以使第1片材1成為特定範圍之溫度之方式,利用配置於第1輥31內之加熱器控制第1輥31之周面部之溫度的方法,使用各種方法。例如,可列舉:於第1輥31之周面部之附近設置加熱器或熱風之吹出口、遠紅外線之照射裝置,藉由該等而控制沿著第1片材1之前或之後之第1輥31之周面部之溫度的方法;於嚙合部33中將接觸於第1片材1之第2輥32加熱,藉由其周面部之溫度控制而控制第1片材1之溫度之方法;及對沿著第1輥31之前之第1片材1,使之接觸於加熱輥或通過維持於高溫之空間,或吹送熱風之方法等。 另一方面,作為使第2片材2為未達第2片材之熔點、且較該熔點低50℃之溫度以上之方法,較佳為,將與第1片材1合流之前之第2片材之溫度利用配置於第2片材之搬送路中之測溫機構測量,以其測定值成為上述特定範圍內之方式,控制配置於第2片材之搬送路中之第2片材之加熱機構(未圖示)之溫度。第2片材之加熱機構既可為使經加熱之輥等接觸等之接觸方式,亦可為通過維持於高溫之空間、或吹送熱風或貫通或照射孔外線等非接觸式。 第1片材1及第2片材2之熔點係藉由以下之方法而測定。 例如,使用Perkin-Elmer公司製造之示差掃描熱量測定裝置(DSC,Differential scanning calorimetry)PYRIS Diamond DSC來測定。根據測定資料之峰值算出熔點。於第1片材1或第2片材2為不織布等纖維片材,且其構成纖維為包括芯鞘型、並列型等複數個成分之複合纖維之情形時,該片材之熔點係將藉由DSC而測定出之複數個熔點中最低溫度之熔點設為複合纖維片材之熔點。 於第1實施形態之複合片材之製造方法中,如此,將重疊之第1及第2片材1、2夾於第1輥31之凸部與超音波熔合機之超音波焊頭42之間而施加超音波振動,形成具有貫通孔14之熔合部4。於第1實施形態之複合片材之製造方法中,較佳為,將第1及第2片材1、2之至少一者預先預熱至該片材不熔融之上述特定範圍之溫度,然後,對一者或兩者被預熱之狀態之兩個片材1、2施加超音波振動。此時,調節施加超音波振動時之條件,例如,施加之超音波振動之波長、強度、對兩個片材1、2進行加壓之壓力等,利用超音波振動,將兩個片材1、2熔融而形成熔合部4,並且將貫通兩個片材1、2之貫通孔14形成為由熔融部分包圍之狀態。 根據第1實施形態之複合片材之製造方法,如此,將第1片材1及第2片材2之至少一者,較佳為兩者藉由加熱器等加熱機構而預先加熱至片材不熔融之程度之高溫,然後,於第1輥31之凸部35與超音波熔合機之超音波焊頭42之間一面加壓一面施加超音波振動,形成具有貫通孔14之熔合部4,藉此,與不將兩個片材1、2預熱之情形相比,可更確實地形成具有貫通孔14之熔合部4,並且不易產生於將兩個片材1、2預熱至超過熔點之溫度之情形時容易產生之不良情況,例如,熔融樹脂向搬送機構之附著或片材向搬送輥之捲繞等不良情況,故而裝置之維護負擔亦較小。 又,藉由於第1輥31之凸部35與超音波熔合機之超音波焊頭42之間,同時地進行熔合部4之形成與貫通孔14之形成,而於熔合部4之位置與貫通孔14之位置之間亦不產生位置偏移。 藉由第1實施形態之複合片材之製造方法而獲得之複合片材10具有凹凸,而且於凹部之底部具有熔合部4,該熔合部4具有貫通孔14,故而肌膚觸感或平面方向上之液體之擴散防止性優異,又透氣性或液體之引入性亦優異。 複合片材10發揮該特性,較佳地用作吸收性物品之表面片材,但複合片材10之用途並不限定於此。 自更確實地發揮上述一個或兩個以上之效果之觀點而言,本案發明之製造方法及製造裝置較佳為具有以下之構成。 (1)第1片材1較佳為預熱至較第1片材1之熔點低50℃之溫度以上、且未達該熔點,更佳為預熱至較第1片材1之熔點低20℃之溫度以上、且較該熔點低5℃之溫度以下。 (2)第2片材2較佳為預熱至較第2片材2之熔點低50℃之溫度以上、且未達該熔點,更佳為預熱至較第2片材2之熔點低20℃之溫度以上、且較該熔點低5℃之溫度以下之溫度。 第1片材1及第2片材2各者之預熱溫度自容易形成貫通孔14之觀點而言,較佳為100℃以上,更佳為130℃以上,又,自防止向搬送機構之附著或防止向搬送輥之捲繞之觀點而言,較佳為150℃以下,更佳為145℃以下。 又,自容易形成熔合部4、貫通孔14之觀點而言,夾於第1輥31之凸部35之前端面35c與超音波焊頭42之前端面42t之間而施加至第1及第2片材1、2之加壓力較佳為10 N/mm以上,更佳為15 N/mm以上,又,較佳為150 N/mm以下,更佳為120 N/mm以下,又,較佳為10 N/mm以上且150 N/mm以下,更佳為15 N/mm以上且120 N/mm以下。 此處所言及之加壓力係所謂線壓,由將超音波焊頭42之加壓力(N)除以與超音波焊頭42接觸之凸部35之齒寬(X方向)之合計(不包含第1輥31之凹部)之長度所得的值(每單位長度之壓力)來表示。 又,自容易形成熔合部4、貫通孔14之觀點而言,施加之超音波振動之頻率較佳為15 kHz以上,更佳為20 kHz以上,又,較佳為50 kHz以下,更佳為40 kHz以下,又,較佳為15 kHz以上且50 kHz以下,更佳為20 kHz以上且40 kHz以下。 〔頻率之測定方法〕 利用雷射移位計等測量喇叭前端之位移。藉由設為採樣頻率200 kHz以上,精度1 μm以上而測定頻率。 又,自容易形成熔合部、貫通孔之觀點而言,施加之超音波振動之振幅較佳為20 μm以上,更佳為25 μm以上,又,較佳為50 μm以下,更佳為40 μm以下,又,較佳為20 μm以上且50 μm以下,更佳為25 μm以上且40 μm以下。 〔振幅之測定方法〕 利用雷射移位計等測量喇叭前端之位移。藉由設為採樣頻率200 kHz以上,精度1 μm以上而測定振幅。 其次,對本發明之複合片材之製造方法之第2及第3實施態樣進行說明。 於第2實施態樣,使用圖6表示主要部分之第2實施形態之複合片材之製造裝置,製造上述複合片材10。 第2實施態樣之複合片材之製造裝置僅於具備加熱超音波熔合機41之超音波焊頭42之機構來代替配置於第1輥31內之加熱器61(預熱機構)之方面,與上述複合片材之製造裝置20不同。更具體而言,第2實施態樣之複合片材之製造裝置具備安裝於超音波焊頭42之加熱器62來作為加熱超音波焊頭42之機構。 於第2實施態樣之複合片材之製造方法中,藉由控制由加熱器62加熱之超音波焊頭42之溫度,而將即將施加超音波振動之前之第2片材2之溫度預先加熱至未達該片材2之熔點、且較該熔點低50℃之溫度以上,於該狀態下,對夾於第1輥31之凸部35與超音波熔合機之超音波焊頭42之間的第1及第2片材1、2施加超音波振動。 於藉由加熱器62等加熱機構而加熱超音波焊頭42之情形時,於藉由超音波熔合機而施加超音波振動之狀態下,第1及第2片材1、2發熱,難以測定由預熱機構加熱之片材之溫度。因此,於經由經加熱之超音波焊頭42而將第1及第2片材1、2之一者或兩者預熱之情形時,不產生超音波振動僅將加熱進行30分鐘之後測定該超音波焊頭之前端面42t之溫度,將該測定值設為由預熱機構加熱之片材之溫度。 關於第2實施態樣未特別說明之方面與第1實施形態相同,適當應用關於第1實施態樣之說明。 於第3實施態樣中,使用圖7表示主要部分之第3實施形態之複合片材之製造裝置,製造上述複合片材10。 第3實施態樣之複合片材之製造裝置不具備於施加超音波振動之前,將第1片材及第2片材之至少一者加熱至特定溫度之預熱機構,另一方面,於超音波焊頭42之前端部,配置有具有蓄熱性之構件7(以下亦稱為「蓄熱材」)。 於第3實施態樣之製造方法中,與第1實施形態之製造方法相同地,將第1片材1導入至第1及第2輥31、32之嚙合部33而使之變形為凹凸形狀之後,將該變形為凹凸形狀之第1片材1一面保持於第1輥31上一面朝向超音波振動之施加部36搬送,使第2片材2重疊於搬送中之第1片材1之後,將該重疊之兩個片材1、2夾於第1輥31之凸部35與超音波熔合機之超音波焊頭42之前端面42t之間而於超音波振動之施加部36施加超音波振動。 於第3實施態樣之製造方法中,該超音波振動之施加如圖7所示,於在超音波焊頭42之前端部配置有蓄熱材7之狀態下進行。 根據第3實施態樣之製造方法,於複合片材之製造裝置之運轉剛開始之後,包括蓄熱材7之超音波焊頭42之前端部之溫度為第1及第2片材1、2之熔點以下,但若繼續運轉,則藉由超音波振動而發熱之第1及第2片材1、2之熱蓄積於蓄熱材7,蓄熱材7之溫度上升成為第1片材1及第2片材2之熔點以上。然後,於蓄熱材7之溫度成為第1片材1及第2片材2各者之熔點以上之狀態下,調節施加超音波振動時之條件,例如,超音波振動之波長、強度、對兩個片材1、2進行加壓之壓力等,於施加超音波振動時,兩個片材1、2熔融,並且若貫通兩個片材1、2之貫通孔14形成為由熔融部分包圍之狀態,則可確實地形成具有貫通孔14之熔合部4,並且亦不易產生片材熔融而產生之熔融樹脂向搬送機構之附著或片材向搬送輥之捲繞等不良情況,故而裝置之維護負擔亦較小。 又,藉由於第1輥31之凸部35與超音波熔合機之超音波焊頭42之間,同時地進行熔合部4之形成與貫通孔14之形成,而於熔合部4之位置與貫通孔14之位置之間亦不會產生位置偏移。 蓄熱材7與至少構成超音波焊頭42之金屬相比,熱導率較低。 蓄熱材7較佳為藉由下述方法而測定出之熱導率為2.0 W/mK以下。蓄熱材之熱導率自不易向超音波焊頭或大氣放熱之觀點而言,較佳為2.0 W/mK以下,更佳為1.0 W/mK以下,又,自有效率地加熱片材之觀點而言,較佳為0.1 W/mK以上,更佳為0.5 W/mK以上,又,較佳為0.1 W/mK以上且2.0 W/mK以下,更佳為0.5 W/mK以上且1.0 W/mK以下。 〔熱導率之測定方法〕 蓄熱材7之熱導率使用熱導率測定裝置來測定。 蓄熱材7較佳地使用具有耐熱性者。蓄熱材7之耐熱溫度較佳為150℃以上,更佳為200℃以上,進而較佳為250℃以上。無特別之耐熱溫度之上限,例如為1500℃以下。 蓄熱材7亦可使用包括具有蓄熱性之本體部分及用以將該本體接著於超音波焊頭之接著劑層者,該情形時之熱導率係將接著劑部分除外而進行測定。作為該蓄熱材,例如,亦可使用日東電工製造之「玻璃布膠帶」、日東電工製造之「耐熱絕緣用聚醯亞胺膠帶」等市售品。 作為蓄熱材7之具有蓄熱性之本體部分之材質,可列舉玻璃、聚醯亞胺等,自具有適度之蓄熱性且耐熱性較高之觀點而言,較佳為聚醯亞胺等。蓄熱材7既可為單層構造之片材,亦可為包括相同或不同之材質之2個以上之片材等積層體。 又,蓄熱材7較佳為具有相對於在第1輥31之軸長方向較長之形狀之超音波焊頭42的前端面而於相同方向較長之形狀。又,自防止超音波施加時之卡住之觀點而言,蓄熱材7較佳為如圖7所示,除了被覆超音波焊頭42之前端面之部分以外,還具有被覆超音波焊頭42之前端面42t之片材行進方向上游側(圖7中左側)之角部42a之部分,又,較佳為具有被覆超音波焊頭42之前端面42t之片材行進方向下游側(圖7中右側)之角部42b之部分。 用於蓄熱材7之本體部分之聚醯亞胺於如下方面亦較佳,即耐磨損性及耐熱性優異,而且為合成樹脂,具有接受超音波振動則其本身亦發熱之性能。 自相同之觀點而言,蓄熱材7之本體部分或圖8(a)所示之超音波焊頭42上所設置之合成樹脂層42h較佳為包括聚醯亞胺或聚苯并咪唑、聚醚乙基酮、聚苯硫醚、聚醚醯亞胺、聚醯胺醯亞胺等洛氏硬度為R120以上且R140以下、耐熱溫度為150℃以上且500℃以下之合成樹脂,更佳為包括聚醯亞胺或聚苯并咪唑等洛氏硬度為R125以上且R140以下、耐熱溫度為280℃以上且400℃以下之合成樹脂。 此處,洛氏硬度係根據ASTM D785而測定出之值,耐熱溫度係根據ASTM D648而測定出之值。 設置於超音波焊頭42之前端部之合成樹脂層之耐熱溫度較佳為150℃以上,更佳為280℃以上,又,較佳為500℃以下,更佳為400℃以下,又,較佳為150℃以上且500℃以下,更佳為280℃以上且400℃以下。 設置於超音波焊頭42之前端部之合成樹脂層之洛氏硬度較佳為R120以上,更佳為R125以上,又,較佳為R140以下,又,較佳為R120以上且R140以下,更佳為R125以上且R140以下。 圖8(a)係表示於前端部設置有蓄熱材7之超音波焊頭42之另一例之圖。於圖8(a)中,圓C2部分係圓C1部分之放大剖視圖。 於圖8(a)所示之超音波焊頭42中,如圖8(b)所示,於包括鋁合金或鈦合金等金屬之超音波焊頭42之本體部分42c之前端面42t,藉由熔射形成具有自一面42d至內部之空隙42e之連接層42f之後,如圖8(a)所示,於該連接層42f之上述一面42d側,固定有作為具有蓄熱性之構件之合成樹脂層42h。所謂熔射係指使藉由加熱而熔融或接近熔融之狀態之金屬或陶瓷等熔射材料之粒子加速而以高速與基材面碰撞,於該基材面形成被膜之表面處理法。於包括鈦合金等金屬之超音波焊頭42之本體部分42c之前端面42t,經由藉由熔射形成之連接層42f,設置具有蓄熱性之合成樹脂層42h,藉此,作為具有蓄熱性之合成樹脂層42h之材料,耐磨損性或耐熱性等優異,另一方面,即便於使用在直接固定之情形時不易獲得充分之固定強度之聚醯亞胺等合成樹脂之情形時,亦可容易地獲得充分之固定強度。再者,若固定強度不充分,則於複合片材10之製造中,容易產生合成樹脂層42h剝離等不良情況。 作為用以形成連接層42f之熔射材料,可無特別限制地使用能夠熔射、且可有助於提高具有蓄熱性之合成樹脂層42h之固定強度者,但自相對於包括鈦合金等金屬之超音波焊頭42之本體部分42c之結合力優異、耐磨損性或耐熱性亦優異之觀點而言,較佳地使用碳化鎢、氧化鋯、碳化鉻等陶瓷、鋁鎂、鋅鋁等合金、鋁、不鏽鋼、鈦、鉬等金屬、作為金屬與陶瓷之複合材之金屬陶瓷等,自形成提高合成樹脂層42h之固定強度之空隙42e之觀點而言,更佳為陶瓷,進而較佳為使用碳化鎢。 又,連接層42f之形成材料與構成具有蓄熱性之合成樹脂層42h之合成樹脂相比熔點較高,且於形成合成樹脂42h時維持空隙42e之形狀自提高合成樹脂層42h之固定強度之觀點而言較佳。 作為將具有蓄熱性之合成樹脂層42h固定於連接層42f之方法,可列舉:將連接層42f浸漬於藉由加熱而熔融之合成樹脂之方法;將藉由加熱而熔融之合成樹脂塗佈於連接層42f之方法;將經軟化之合成樹脂之板狀體壓抵於連接層42f之方法等。 連接層42f之厚度Tf〔參照圖8(a)〕無特別限制,若列舉一例,則較佳為10 μm以上,更佳為20 μm以上,又,較佳為100 μm以下,更佳為50 μm以下,又,較佳為10 μm以上且100 μm以下,更佳為20 μm以上且50 μm以下。 具有蓄熱性之合成樹脂層42h之厚度Th〔參照圖8(a)〕無特別限制,若列舉一例,則較佳為5 μm以上,更佳為10 μm以上,又,較佳為100 μm以下,更佳為50 μm以下,又,較佳為5 μm以上且100 μm以下,更佳為10 μm以上且50 μm以下。 又,連接層42f之厚度Tf相對於該厚度Tf與合成樹脂層42h之厚度Th之合計厚度Tt的比率,自維持合成樹脂之固定強度且不阻礙超音波振動或發熱之觀點而言,較佳為30%以上,更佳為50%以上,又,較佳為85%以下,更佳為75%以下,又,較佳為30%以上且85%以下,更佳為50%以上且75%以下。 即便為如第3實施形態般具備蓄熱材7之複合片材之製造裝置,亦可具有第1實施形態之複合片材之製造裝置所具備之預熱機構6或將第2實施形態之複合片材之製造裝置所具備之超音波焊頭42加熱的機構。 於上述各實施形態中製造之複合片材10較佳為具有以下之構成。 凸部5之高度H(參照圖1)為1~10 mm,特佳為3~6 mm。複合片材10之每單位面積(1 cm2 )之凸部5之數量為1~20個,特佳為6~15個。凸部5之X方向之底部尺寸A(參照圖1)為0.5~5.0 mm,特佳為1.0~4.0 mm。凸部5之Y方向之底部尺寸B(參照圖1)為1.0~10 mm,特佳為2.0~7.0 mm。 X方向之底部尺寸A與Y方向之底部尺寸B之比(底部尺寸A:底部尺寸B)為1:1~1:10,特佳為1:2~2:5。凸部5之底部面積(底部尺寸A×底部尺寸B)為0.5~50 mm2 ,特佳為2~20 mm2 。 熔合部4係X方向之尺寸C(參照圖1)為0.5~2 mm,特佳為0.8~1.5 mm,Y方向之尺寸D(參照圖1)為1.0~5.0 mm,特佳為1.2~3.0 mm。X方向之尺寸C與Y方向之尺寸D之比(尺寸C:尺寸D)為1:1~1:3,特佳為2:3~2:5。 熔合部4之較外周緣靠內側之面積較佳為0.5 mm2 以上,更佳為1.0 mm2 以上,又,較佳為5.0 mm2 以下,更佳為4.0 mm2 以下,又,較佳為0.5 mm2 以上且5.0 mm2 以下,更佳為1.0 mm2 以上且4.0 mm2 以下。熔合部4之較外周緣靠內側之面積亦包含貫通孔14之面積。 貫通孔14之開口面積相對於熔合部4之較外周緣靠內側之面積,較佳為50%以上,更佳為80%以上,又,較佳為未達100%,更佳為95%以下,又,較佳為50%以上且100%未達,更佳為80%以上且95%以下。 上述複合片材10較佳地用作拋棄式尿布、經期衛生棉、衛生護墊、失禁護墊等吸收性物品之表面片材。 又,亦可使用於除吸收性物品之表面片材以外之用途。 例如,作為吸收性物品用之片材,可使用於配置於表面片材與吸收體之間之片材、立體褶皺(防漏壁)形成用之片材(尤其形成褶皺之內壁之片材)等,又,作為除吸收性物品以外之用途,可用作清掃片材、尤其以液體吸收為主之清掃片材或對人用之化妝片材等。於用於清掃片材之情形時,於凸部中,對並不平滑之被清掃面之追隨性良好,故而較佳為將第1不織布側朝向被清掃面使用。於用作化妝片材之情形時,於凸部中追隨對象者之肌膚,又,體現按摩效果,並且可進行多餘之化妝劑(另外使用)或汗之吸收,故而較佳為將第1不織布側朝向肌膚側使用。 本發明之複合片材之製造方法及製造裝置不受上述實施形態任何限制,能夠適當變更。 例如,上述複合片材10係於各個凹部形成有一個熔合部,但於本發明中製造之複合片材亦可為於一個凹部包含複數個熔合部者。又,複合片材10之凸部5為四角錐台形狀者,但亦可為半球狀者等。又,相互鄰接之行中之凸部5及熔合部4分別於X方向偏移之程度既可代替1/2間距,而為1/3間距、1/4間距等,進而亦可不於X方向偏移。 又,熔合部及貫通孔之俯視形狀可為橢圓形、圓形、將角部弄圓之多邊形(正方形、長方形、三角形、菱形等)等。 又,製造之複合片材10既可為以日本專利特開2016-116582之圖4或圖5所示之態樣形成有凸部及熔合部者,亦可為以日本專利特開2016-116583號公報之圖3所示之態樣形成有凸部及熔合部者。又,亦可代替將存在於複合片材之熔合部之全部設為具有貫通孔之熔合部,而將存在於複合片材之熔合部中之一部分設為具有貫通孔之熔合部。例如,亦可對帶狀之複合片材中之寬度方向之中央區域中之第1及第2片材之一者或兩者進行預熱,形成具有貫通孔之熔合部,另一方面,不對隔著中央區域之側區域中之第1及第2片材之兩者進行預熱,形成不具有貫通孔之熔合部。 關於上述本發明之實施形態(態樣),進而揭示以下之複合片材之製造方法及複合片材之製造裝置。 <1> 一種複合片材之製造方法,該複合片材具有第1片材及第2片材熔合之多個熔合部,且上述第1片材中之除上述熔合部以外之部分之至少一部分形成向與上述第2片材側為相反側突出之凸部,該複合片材之製造方法具備: 賦形步驟,其一面使於周面部具有相互嚙合之凹凸之第1輥及第2輥旋轉,一面將上述第1片材導入至該等兩輥之嚙合部而使之變形為凹凸形狀;重疊步驟,其將變形為凹凸形狀之上述第1片材一面保持於上述第1輥上一面搬送,且使上述第2片材重疊於搬送中之上述第1片材;及超音波處理步驟,其將重疊之兩個片材夾於上述第1輥之凸部與超音波熔合機之超音波焊頭之間而施加超音波振動; 於上述超音波處理步驟中,於該超音波振動之施加時,形成具有貫通孔之上述熔合部。 <2> 如上述<1>之複合片材之製造方法,其中將上述超音波焊頭加熱至特定溫度,於上述超音波處理步驟中,與上述超音波振動之施加一同地加熱上述第1片材及上述第2片材之至少一者。 <3> 如上述<1>或<2>之複合片材之製造方法,其中將上述第1輥加熱至特定溫度,於上述超音波振動之施加之前,預先加熱上述第1片材及上述第2片材之至少一者。 <4> 如上述<1>至<3>中任一項之複合片材之製造方法,其中於上述超音波振動之施加之前,將上述第1片材及上述第2片材之至少一者直接預先加熱至特定溫度。 <5> 如上述<2>至<4>中任一項之複合片材之製造方法,其中特定溫度未達加熱之上述第1片材或上述第2片材之熔點,且為較該熔點低50℃之溫度以上。 <6> 如上述<1>至<5>中任一項之複合片材之製造方法,其中於上述超音波處理步驟中,於在上述超音波焊頭之前端部配置有具有蓄熱性之構件的狀態下進行上述超音波振動之施加,於該超音波振動之施加時,形成具有貫通孔之上述熔合部。 <7> 如上述<6>之複合片材之製造方法,其中上述具有蓄熱性之構件與構成上述超音波焊頭之材料相比,熱導率較低。 <8> 如上述<6>或<7>之複合片材之製造方法,其中上述具有蓄熱性之構件之熱導率為2.0 W/mK以下,較佳為1.0 W/mK以下,又,為0.1 W/mK以上,較佳為0.5 W/mK以上,又,為0.1 W/mK以上且2.0 W/mK以下,較佳為0.5 W/mK以上且1.0 W/mK以下。 <9> 如上述<6>至<8>中任一項之複合片材之製造方法,其中上述具有蓄熱性之構件具有耐熱性, 上述具有蓄熱性之構件之耐熱溫度為150℃以上,較佳為200℃以上,更佳為250℃以上,上述具有蓄熱性之構件之耐熱溫度之上限為1500℃以下。 <10> 如上述<6>至<9>中任一項之複合片材之製造方法,其中上述具有蓄熱性之構件之材料為玻璃或聚醯亞胺。 <11> 如上述<6>至<10>中任一項之複合片材之製造方法,其中上述具有蓄熱性之構件除了被覆上述超音波焊頭之前端面之部分以外,還具有被覆該超音波焊頭之前端面之片材行進方向上游側的角部之部分。 <12> 如上述<11>之複合片材之製造方法,其中上述具有蓄熱性之構件進而具有被覆上述超音波焊頭之前端面之片材行進方向下游側的角部之部分。 <13> 如上述<1>至<12>中任一項之複合片材之製造方法,其中夾於上述第1輥之凸部之前端面與上述超音波焊頭之前端面之間而對上述第1片材及上述第2片材施加之加壓力為10 N/mm以上,較佳為15 N/mm以上,又,為150 N/mm以下,較佳為120 N/mm以下,又,為10 N/mm以上且150 N/mm以下,較佳為15 N/mm以上且120 N/mm以下。 <14> 如上述<1>至<13>中任一項之複合片材之製造方法,其中施加之上述超音波振動之頻率為15 kHz以上,較佳為20 kHz以上,又,為50 kHz以下,較佳為40 kHz以下,又,為15 kHz以上且50 kHz以下,較佳為20 kHz以上且40 kHz以下。 <15> 如上述<1>至<14>中任一項之複合片材之製造方法,其中施加之上述超音波振動之振幅為20 μm以上,較佳為25 μm以上,又,為50 μm以下,較佳為40 μm以下,又,為20 μm以上且50 μm以下,較佳為25 μm以上且40 μm以下。 <16> 如上述<1>至<15>中任一項之複合片材之製造方法,其中上述複合片材用作拋棄式尿布、經期衛生棉、衛生護墊、失禁護墊等吸收性物品之表面片材。 <17> 一種複合片材之製造裝置,該複合片材具有第1片材及第2片材熔合之多個熔合部,且上述第1片材中之除上述熔合部以外之部分之至少一部分形成向與上述第2片材側為相反側突出之凸部,該複合片材之製造裝置具備: 凹凸賦形部,其具有於周面部具有相互嚙合之凹凸之第1輥及第2輥,且使導入至該等兩輥之嚙合部之上述第1片材變形為凹凸形狀;及超音波處理部,其具備超音波熔合機,且於使上述第2片材重疊於變形為凹凸形狀之狀態之上述第1片材上之後,將該等兩個片材夾於上述第1輥之凸部與上述超音波熔合機之超音波焊頭之間而局部地施加超音波振動,形成具有貫通孔之上述熔合部。 <18> 如上述<17>之複合片材之製造裝置,其具備將上述超音波焊頭加熱之機構。 <19> 如上述<17>或<18>之複合片材之製造裝置,其具備預熱機構,該預熱機構將施加上述超音波振動之前之上述第1片材及上述第2片材之至少一者預熱至特定溫度。 <20> 如上述<19>之複合片材之製造裝置,其中上述預熱機構為配置於上述第1輥內之加熱器。 <21> 如上述<19>或<20>之複合片材之製造裝置,其中藉由上述預熱機構,而將上述第1片材加熱至未達該片材之熔點、且較該熔點低50℃之溫度以上。 <22> 如上述<19>至<21>中任一項之複合片材之製造裝置,其中藉由上述預熱機構,而預熱至較上述第1片材之熔點低20℃之溫度以上、且較該熔點低5℃之溫度以下。 <23> 如上述<17>至<22>中任一項之複合片材之製造裝置,其中於上述超音波焊頭之前端部,配置有具有蓄熱性之構件。 <24> 如上述<23>之複合片材之製造裝置,其中上述具有蓄熱性之構件與構成上述超音波焊頭之材料相比,熱導率較低。 <25> 如上述<23>或<24>之複合片材之製造裝置,其中上述具有蓄熱性之構件之熱導率為2.0 W/mK以下,較佳為1.0 W/mK以下,又,為0.1 W/mK以上,較佳為0.5 W/mK以上,又,為0.1 W/mK以上且2.0 W/mK以下,較佳為0.5 W/mK以上且1.0 W/mK以下。 <26> 如上述<23>至<25>中任一項之複合片材之製造裝置,其中上述具有蓄熱性之構件具有耐熱性, 上述具有蓄熱性之構件之耐熱溫度為150℃以上,較佳為200℃以上,更佳為250℃以上,上述具有蓄熱性之構件之耐熱溫度之上限為1500℃以下。 <27> 如上述<23>至<26>中任一項之複合片材之製造裝置,其中上述具有蓄熱性之構件除了被覆上述超音波焊頭之前端面之部分以外,還具有被覆該超音波焊頭之前端面之片材行進方向上游側的角部之部分。 <28> 如上述<27>之複合片材之製造裝置,其中上述具有蓄熱性之構件進而具有被覆上述超音波焊頭之前端面之片材行進方向下游側的角部之部分。 <29> 如上述<23>至<28>中任一項之複合片材之製造裝置,其中上述具有蓄熱性之構件之材料為玻璃或聚醯亞胺。 <30> 如上述<23>至<29>中任一項之複合片材之製造裝置,其中於上述超音波焊頭之前端部,作為具有蓄熱性之構件而設置有具有耐熱性之合成樹脂層。 <31> 如上述<30>之複合片材之製造裝置,其中上述合成樹脂層之耐熱溫度為150℃以上,較佳為280℃以上,又,為500℃以下,較佳為400℃以下,又,為150℃以上且500℃以下,較佳為280℃以上且400℃以下。 <32> 如上述<23>至<31>中任一項之複合片材之製造裝置,其中於上述超音波焊頭之前端部,作為具有蓄熱性之構件而設置有具有耐磨損性之合成樹脂層。 <33> 如上述<32>之複合片材之製造裝置,其中上述合成樹脂層之洛氏硬度為R120以上,較佳為R125以上,又,為R140以下,又,為R120以上且R140以下,較佳為R125以上且R140以下。 <34> 如上述<30>至<33>中任一項之複合片材之製造裝置,其中上述合成樹脂層係隔著藉由熔射形成之連接層而固定於上述超音波焊頭之包含金屬之本體部分之前端面。 <35> 如上述<17>至<34>中任一項之複合片材之製造裝置,其中夾於上述第1輥之凸部與上述超音波焊頭之間而對上述第1片材及上述第2片材施加之加壓力為10 N/mm以上,較佳為15 N/mm以上,又,為150 N/mm以下,較佳為120 N/mm以下,又,為10 N/mm以上且150 N/mm以下,較佳為15 N/mm以上且120 N/mm以下。 <36> 如上述<17>至<35>中任一項之複合片材之製造裝置,其中施加之上述超音波振動之頻率為15 kHz以上,較佳為20 kHz以上,又,為50 kHz以下,較佳為40 kHz以下,又,為15 kHz以上且50 kHz以下,較佳為20 kHz以上且40 kHz以下。 <37> 如上述<17>至<36>中任一項之複合片材之製造裝置,其中施加之上述超音波振動之振幅為20 μm以上,較佳為25 μm以上,又為50 μm以下,較佳為40 μm以下,又,為20 μm以上且50 μm以下,較佳為25 μm以上且40 μm以下。 <38> 如上述<17>至<37>中任一項之複合片材之製造裝置,其中上述複合片材用作拋棄式尿布、經期衛生棉、衛生護墊、失禁護墊等吸收性物品之表面片材。 [產業上之可利用性] 根據本發明之複合片材之製造方法,可容易地形成具有貫通孔之熔合部,於熔合部之位置與貫通孔之位置之間不易產生位置偏移,裝置之維護負擔亦較小。 根據本發明之複合片材之製造裝置,可容易地形成具有貫通孔之熔合部,於熔合部之位置與貫通孔之位置之間不易產生位置偏移,裝置之維護負擔亦較小。In the production of a composite sheet, if the formation of the fusion portion and the formation of the through-holes are performed by different steps, a positional shift may occur between the position of the fusion portion and the position of the through-hole. In addition, Patent Document 2 In the described method of providing a small convex part at the front end of the convex part, the small convex part is easy to wear, and there is room for improvement in terms of a large maintenance burden. Therefore, the present invention relates to a method and a device for manufacturing a composite sheet which can solve the problems of the prior art. Hereinafter, based on the preferred embodiment of the present invention, the present invention will be described with reference to the drawings. First, referring to FIG. 1, a composite sheet produced by the method or device for producing a composite sheet of the present invention will be described. The composite sheet 10 shown in FIG. 1 is an example of a composite sheet manufactured by the method or apparatus for manufacturing a composite sheet of the present invention. As shown in FIG. 1, the composite sheet 10 includes a first sheet 1 and a second sheet 2. The plurality of fused portions 4 are fused, and at least a part of the portion other than the fused portion 4 in the first sheet 1 is formed with a convex portion 5 protruding toward the opposite side from the second sheet 2 side. The composite sheet 10 is preferably used as a surface sheet or the like of an absorbent article. When used as a surface sheet of an absorbent article, the first sheet 1 forms a surface facing the wearer's skin side (hereinafter, also referred to as a skin-facing surface), and the second sheet 2 forms an absorbent body when worn. Side surface (hereinafter, also referred to as non-skin facing surface). The convex portions 5 and the fused portions 4 are arranged alternately and in a row in a direction parallel to the surface of the composite sheet 10, that is, in the X direction in FIG. 1. This line is parallel to the surface of the composite sheet 10 and The direction orthogonal to the above-mentioned one direction, that is, the Y direction in FIG. 1 is formed in a plurality of lines. The convex portions 5 and the fused portions 4 in the mutually adjacent rows are respectively arranged to be shifted in the X direction, and more specifically, they are arranged to be shifted by a half pitch. In the composite sheet 10, the Y direction is consistent with the traveling direction (MD, mechanical direction) during manufacturing, and the X direction is consistent with the direction (CD) orthogonal to the traveling direction during manufacturing. The first sheet 1 and the second sheet 2 include a sheet material. As the sheet material, for example, a fibrous sheet or a film such as a non-woven fabric, a woven fabric, and a knitted fabric can be used. From the viewpoint of skin feel and the like, a fibrous sheet is preferably used, and a non-woven fabric is particularly preferred. The types of the sheet materials constituting the first sheet 1 and the second sheet 2 may be the same or different. Examples of the nonwoven fabric in the case where a nonwoven fabric is used as a sheet material constituting the first sheet 1 and the second sheet 2 include, for example, a hot air nonwoven fabric, a spunbond nonwoven fabric, a spunlace nonwoven fabric, a meltblown nonwoven fabric, a resin adhesive nonwoven fabric, Needle-punched non-woven fabrics, etc. A laminated body obtained by combining two or more kinds of these non-woven fabrics or a laminated body obtained by combining these non-woven fabrics and films can also be used. The basis weight of the nonwoven fabric used as the sheet material constituting the first sheet 1 and the second sheet 2 is preferably 10 g / m 2 Above, more preferably 15 g / m 2 Above, and preferably 40 g / m 2 Below, more preferably 35 g / m 2 the following. The basis weight of the non-woven fabric is preferably 10 g / m 2 Above 40 g / m 2 Below, more preferably 15 g / m 2 Above 35 g / m 2 the following. As the fibers constituting the nonwoven fabric, fibers including various thermoplastic resins can be used. As the sheet material other than the non-woven fabric, a constituent fiber or a constituent resin can be preferably used including various thermoplastic resins. Examples of the thermoplastic resin include polyolefins such as polyethylene, polypropylene, and polybutene, polyesters such as polyethylene terephthalate and polybutylene terephthalate, polyamides such as nylon 6, nylon 66, and the like. Polyacrylic acid, polyalkyl methacrylate, polyvinyl chloride, polyvinylidene chloride, etc. These resins can be used alone or as a mixture of two or more. Moreover, it can be used in the form of a composite fiber such as a core-sheath type or a side-by-side type. As shown in FIG. 1, the composite sheet 10 has a plurality of recesses 3 sandwiched between the protrusions 5 on the surface of the first sheet 1 side in two directions of the X direction and the Y direction, and is formed at the bottom of each recess 3. There is a fused portion 4 having a through hole 14. When viewed as a whole, the surface of the composite sheet 10 on the side of the first sheet 1 has unevenness including the undulations 3 and the protrusions 5 on the side, and the surface on the side of the second sheet 2 is flat, or it is relatively The surface on one side of one sheet is a substantially flat surface with relatively small fluctuations. As shown in FIG. 2, each of the fusion portions 4 in the composite sheet 10 has a substantially rectangular plan view shape that is longer in the Y direction, and a through hole 14 having a substantially rectangular plan view shape is formed inside each of them. In other words, each of the fused portions 4 is formed in a ring shape surrounding the through hole 14. It is preferable that only one through hole 14 is formed in one fused portion 4, and it is preferable that the through hole 14 is formed in a specific position determined in advance in relation to the position of the fused portion 4. In addition, the shape of the through hole 14 in plan view may be similar to the shape of the outer periphery of the fused portion 4 or may be a dissimilar shape, but a similar shape is preferred. In the fusion section 4, the first sheet 1 and the second sheet 2 are joined by melting and solidifying a heat-fusible resin constituting at least one of the first sheet 1 and the second sheet 2. When the first sheet 1 and the second sheet 2 include a fibrous sheet such as a non-woven fabric, in the fusion section 4, the constituent fibers of the first sheet 1 and the second sheet 2 are preferably melted or buried to melt The resin cannot be visually observed in a fibrous state, that is, it is in a state of being film-formed. Next, a first embodiment of the method for manufacturing a composite sheet of the present invention will be described. In the first embodiment, the above-mentioned composite sheet 10 is manufactured using the composite sheet manufacturing apparatus 20 of the first embodiment shown in FIG. 3. If the manufacturing apparatus 20 for a composite sheet shown in FIG. 3 is described, the manufacturing apparatus 20 for a composite sheet is provided with a concave-convex shaping part 30, an ultrasonic processing part 40, and a preheating mechanism 6, which The sheet is preheated to a controlled temperature before the ultrasonic vibration is applied. As shown in FIG. 3, the concave-convex forming portion 30 has first and second rollers 31 and 32 having irregularities that engage with each other on the peripheral surface portion, and the two rolls 31 and 32 are rotated by one side and the first sheet 1 It is introduced into the meshing portion 33 of the two rollers 31 and 32 to deform the first sheet 1 into a concave-convex shape having a concave-convex shape along the peripheral surface of the first roller 31. FIG. 4 is an enlarged perspective view showing a main part of the first roller 31. A part of the peripheral surface of the first roller 31 is shown in FIG. 4. The first roller 31 is formed by combining a plurality of spur gears 31a, 31b, ... having a specific tooth width into a roll shape. The teeth of each gear form a concave-convex convex portion 35 in the peripheral surface of the first roller 31. The front end surface 35c of the convex portion 35 is between the front end surface 42t of the ultrasonic welding head 42 of the ultrasonic fusion machine 41 described below. A pressing surface for pressing the first and second sheets 1 and 2 to be fused. The tooth width (length of the gear in the axial direction) of each gear determines the size of the X direction in the convex portion 5 of the composite sheet 10, and the thickness of the teeth of the gear (length of the gear in the rotation direction) determines the size of the composite sheet 10. The dimension in the above-mentioned Y direction in the convex portion 5. Adjacent gear trains are combined in such a way that the pitch of their teeth is offset by half a pitch, respectively. As a result, the peripheral surface portion of the first roller 31 has an uneven shape. In this embodiment, the front end surface 35c of each convex portion 35 has a rectangular shape in which the rotation direction of the first roller 31 is a long side and the axial direction is a short side. If the front end surface 35c has a long shape in the rotation direction, it is preferable that the contact time between one of the convex portions 35 of the first roller 31 and the front end surface 42t of the ultrasonic horn 42 becomes longer and the temperature is easily increased. The cogging portion of each gear in the first roller 31 forms a concave and convex concave portion on the peripheral surface of the first roller 31. A suction hole 34 is formed in the bottom of the cogging portion of each gear. The suction hole 34 is connected to a suction source (not shown) such as a blower or a vacuum pump, so that the suction portion 34 extends from the engagement portion 33 of the first roller 31 and the second roller 32 to the confluence portion of the first sheet 1 and the second sheet 2. The manner in which suction is performed until now is controlled. Therefore, the first sheet 1 deformed into a concave-convex shape by the engagement of the first roller 31 and the second roller 32 is maintained to be deformed along the first roller 31 by the suction force of the suction hole 34. The state of the shape of the unevenness is conveyed to the confluence part of the first sheet 1 and the second sheet 2 and the ultrasonic vibration application part 36 using an ultrasonic fusion machine. In this case, as shown in FIG. 4, if a specific gap G is provided between adjacent gears, it is possible to suppress excessive stretching force from being applied to the first sheet 1 or the meshing portion 33 of the two rollers 31 and 32. It is preferable to cut the first sheet 1 to deform the first sheet 1 into a shape along the peripheral surface of the first roller 31. The second roller 32 has a concavo-convex shape on the peripheral surface portion which meshes with the concavities and convexities on the peripheral surface portion of the first roller 31. The second roller 32 has the same configuration as the first roller 31 except that it does not have the suction hole 34. In addition, the first sheet 1 is introduced into the meshing portion 33 of the two rollers 31 and 32 while the first and second rollers 31 and 32 having the mutually engaging irregularities are rotated, and the first sheet 1 can be deformed. It is a concave-convex shape. In the engaging portion 33, a plurality of portions of the first sheet 1 are pressed into the concave portions of the peripheral surface of the first roller 31 by the convex portions of the second roller 32, and the pressed portions become the manufactured composite sheet 10 The convex part 5. A plurality of convex portions are formed on the peripheral surface of the second roller 32 and are inserted into the concave portions of the first roller 31. As shown in FIG. 3, the ultrasonic processing unit 40 is provided with an ultrasonic fusion machine 41 having an ultrasonic welding head 42 to superimpose the second sheet 2 on the first sheet 1 which is deformed into an uneven shape, and then The two sheets are sandwiched between the convex portion of the first roller 31 and the ultrasonic horn 42 to locally apply ultrasonic vibration to form a fusion portion 4 having a through hole 14. As shown in FIGS. 3 and 5, the ultrasonic fusion machine 41 includes an ultrasonic oscillator (not shown), a converter 43, an accelerator 44, and an ultrasonic welding head 42. An ultrasonic oscillator (not shown) is electrically connected to the converter 43, and a high-voltage electric signal having a frequency of about 15 kHz to 50 kHz generated by the ultrasonic oscillator is input to the converter 43. An ultrasonic oscillator (not shown) is provided on or outside the movable table 45. The transducer 43 includes a piezoelectric element such as a piezoelectric element, and converts an electric signal input from the ultrasonic oscillator into a mechanical vibration by the piezoelectric element. The amplitude adjustment of the mechanical vibration emitted from the converter 43 by the accelerator 44 is preferably amplified and transmitted to the ultrasonic welding head 42. The ultrasonic horn 42 is formed of a metal block such as an aluminum alloy or a titanium alloy, and is designed to accurately resonate according to the frequency used. The ultrasonic vibration transmitted from the accelerator 44 to the ultrasonic horn 42 is amplified or attenuated inside the ultrasonic horn 42 and then applied to the first and second sheets 1 and 2 as fusion targets. As this ultrasonic fusion machine 41, a commercially available ultrasonic welding head, converter, accelerator, and ultrasonic oscillator can be used in combination. The ultrasonic fusion machine 41 is fixed on the movable table 45, and by moving the position of the movable table 45 toward the direction close to the peripheral surface of the first roller 31, the front end face 42t of the ultrasonic welding head 42 and the first roller 31 can be adjusted. The gap between the front end surface 35c of the convex portion 35 and the pressing force applied to the laminated first and second sheets 1 and 2. Furthermore, the pressure is sandwiched between the front end surface 35c of the convex portion 35 of the first roller 31 and the front end surface 42t of the ultrasonic welding head 42 of the ultrasonic fusion machine 41, and the first and the first objects to be fused are pressed. The two sheets 1 and 2 are subjected to ultrasonic vibration, and each of the portions of the first sheet 1 located on the front end surface 35c of the convex portion 35 is fused to the second sheet 2 to form a fusion portion 4, and the two The through holes 14 of the sheets 1 and 2 are formed in a state surrounded by the molten portion. In a preferred embodiment, the manufacturing apparatus 20 for the composite sheet includes a preheating mechanism 6 having a heater 61 disposed in the first roller 31. More specifically, it includes a heating mechanism such as a heater 61 disposed in the first roller 31, a temperature measuring mechanism (not shown) capable of measuring the temperature of the sheet before ultrasonic vibration is applied, and measurement by the temperature measuring mechanism A temperature control unit (not shown) that controls the temperature of the heater 61. By controlling the heating temperature of the peripheral surface of the first roller 31 by the heater 61 by the measured value based on the temperature measurement mechanism, the temperature of the first sheet 1 immediately before the ultrasonic vibration is applied can be accurately controlled. Expected temperature. In a preferred embodiment, the heater 61 is fitted into the first roller 31 along its axial length direction. Further, the heaters 61 are arranged in the vicinity of the outer periphery of the rotation axis of the first roller 31 and are arranged in the circumferential direction with a plurality of them. The heating temperature of the peripheral surface of the first roller 31 by the heater 61 is controlled by a temperature control section (not shown), and the composite sheet manufacturing apparatus 20 can be introduced to the ultrasonic vibration application section 36 during operation. The temperature of the first sheet 1 is maintained at a specific range of temperature. The preheating mechanism 6 is preferably provided with a heating mechanism that applies heat energy to the object to be heated from the outside and heats it. Examples of the heating mechanism include a cassette heater using an electric heating wire, but the invention is not limited to this, and various known heating mechanisms can be used without particular limitation. The ultrasonic fusion machine applies ultrasonic vibration to a fusion object, thereby heating and melting the fusion object to fuse, and does not include the heating mechanism mentioned here. In the manufacturing method according to the first embodiment of the present invention, as shown in FIG. 3, while rotating the first and second rolls 31 and 32, the first sheet rolled out from the raw sheet roll (not shown) 1 is introduced into the meshing portion 33 of the two rollers 31 and 32 to deform it into a concave-convex shape (forming step). Then, the first sheet 1 deformed into a concave-convex shape is conveyed while being held on the first roll 31, and the second sheet 2 rolled out from a raw sheet roll (not shown) different from the first sheet 1 is conveyed. Superimposed on the first sheet 1 being conveyed (overlapping step). Then, the overlapping two sheets 1 and 2 are sandwiched between the convex portion 35 of the first roller 31 and the ultrasonic welding head 42 of the ultrasonic fusion machine to apply ultrasonic vibration (ultrasonic processing step). In the ultrasonic processing step, when ultrasonic vibration is applied, a fusion portion 4 having a through hole 14 is formed. In the manufacturing method of the first embodiment, it is preferable that at least one of the first sheet 1 and the second sheet 2 is heated in advance to a temperature below the melting point of the sheet, before the ultrasonic vibration is applied. It is more than 50 ° C lower than the melting point. That is, it is preferable to perform any one or both of the following (1) and (2) before the ultrasonic vibration is applied. (1) The first sheet 1 is heated in advance to a temperature that does not reach the melting point of the first sheet and is 50 ° C lower than the melting point. (2) The second sheet 2 is heated in advance to a temperature that does not reach the melting point of the second sheet and is 50 ° C lower than the melting point. Preferably, the first sheet 1 is heated in advance to a temperature that does not reach the melting point of the first sheet and is 50 ° C lower than the melting point, and the second sheet 2 is heated in advance to the second sheet. The melting point of the material is at least 50 ° C lower than the melting point. As a method of making the first sheet 1 less than the melting point of the first sheet 1 and a temperature that is 50 ° C. or more lower than the melting point, for example, the meshing portion 33 of the first and second rollers 31 and 32 and Yuchao The temperature of the first sheet 1 on the first roller 31 is measured between the ultrasonic vibration application unit 36 performed by the sonic fusion machine, and the circumference of the first roller 31 is controlled so that the measured value falls within the above-mentioned specific range. Face temperature. As a method for preheating the first sheet 1 to a temperature in a specific range, instead of making the first sheet 1 into a temperature in a specific range, the first roller 31 may be controlled by a heater disposed in the first roller 31. Various methods can be used to measure the temperature of the face. For example, the heater may be provided near the peripheral surface of the first roller 31, a hot air outlet, and a far-infrared irradiation device, and the first roller may be controlled before or after along the first sheet 1 by these. A method of heating the peripheral surface of the 31st sheet; a method of heating the second roller 32 in contact with the first sheet 1 in the engaging portion 33 and controlling the temperature of the first sheet 1 by controlling the temperature of the peripheral surface; and The first sheet 1 along the first roller 31 is brought into contact with a heating roller or passed through a space maintained at a high temperature or a method of blowing hot air. On the other hand, as a method for making the second sheet 2 a temperature lower than the melting point of the second sheet and at a temperature of 50 ° C. or more lower than the melting point, it is preferable that the second sheet 2 be merged with the first sheet 1 The temperature of the sheet is measured by a temperature measuring mechanism arranged in the conveying path of the second sheet, and the measurement value of the sheet is controlled to be within the above-mentioned specific range, and the temperature of the second sheet disposed in the conveying path of the second sheet is controlled. Temperature of heating mechanism (not shown). The heating mechanism of the second sheet may be a contact method such as contacting heated rollers or the like, or a non-contact method such as maintaining a high temperature space, blowing hot air, penetrating or irradiating the outer line of a hole. The melting points of the first sheet 1 and the second sheet 2 are measured by the following methods. For example, a differential scanning calorimetry (DSC, Pyris Diamond DSC) manufactured by Perkin-Elmer is used for measurement. The melting point was calculated from the peak value of the measurement data. When the first sheet 1 or the second sheet 2 is a fibrous sheet such as a non-woven fabric, and the constituent fibers are composite fibers including a plurality of components such as a core-sheath type and a side-by-side type, the melting point of the sheet will be calculated by Among the plurality of melting points measured by DSC, the melting point of the lowest temperature is the melting point of the composite fiber sheet. In the manufacturing method of the composite sheet of the first embodiment, the overlapping first and second sheets 1 and 2 are sandwiched between the convex portion of the first roller 31 and the ultrasonic welding head 42 of the ultrasonic fusion machine. Ultrasonic vibration is applied from time to time to form a fused portion 4 having a through hole 14. In the manufacturing method of the composite sheet of the first embodiment, it is preferable that at least one of the first and second sheets 1 and 2 is pre-heated to a temperature within the above-mentioned specific range where the sheet does not melt, and then , Ultrasonic vibration is applied to the two sheets 1 and 2 in a state where one or both are preheated. At this time, the conditions when applying the ultrasonic vibration are adjusted, for example, the wavelength and intensity of the applied ultrasonic vibration, the pressure for pressing the two sheets 1, 2 and the like, and the two sheets 1 are ultrasonically vibrated. 2 and 2 are melted to form a fused portion 4, and the through-holes 14 penetrating through the two sheets 1 and 2 are formed in a state surrounded by the melted portion. According to the method for manufacturing a composite sheet according to the first embodiment, at least one of the first sheet 1 and the second sheet 2 is preferably heated to the sheet in advance by a heating mechanism such as a heater. The temperature is not high enough to melt, and then ultrasonic vibration is applied between the convex portion 35 of the first roller 31 and the ultrasonic welding head 42 of the ultrasonic fusion machine to form a fusion portion 4 having a through hole 14, Thereby, compared with the case where the two sheets 1, 2 are not preheated, the fusion portion 4 having the through holes 14 can be formed more reliably, and it is less likely to occur that the two sheets 1, 2 are preheated to exceed Defects that easily occur in the case of the temperature of the melting point, for example, the adhesion of the molten resin to the conveying mechanism or the winding of the sheet to the conveying roller, so the maintenance burden on the device is also small. In addition, since the formation of the fusion portion 4 and the formation of the through hole 14 are performed simultaneously between the convex portion 35 of the first roller 31 and the ultrasonic welding head 42 of the ultrasonic fusion machine, the position and penetration of the fusion portion 4 are formed. There is also no positional shift between the positions of the holes 14. The composite sheet 10 obtained by the method for manufacturing a composite sheet according to the first embodiment has irregularities, and has a fused portion 4 at the bottom of the recessed portion. The fused portion 4 has a through hole 14. The liquid has excellent diffusion prevention properties, and also has excellent air permeability or liquid introduction properties. The composite sheet 10 exhibits this characteristic and is preferably used as a surface sheet of an absorbent article, but the use of the composite sheet 10 is not limited to this. From the viewpoint of more reliably exerting one or more of the effects described above, the manufacturing method and manufacturing apparatus of the present invention preferably have the following configurations. (1) The first sheet 1 is preferably preheated to a temperature that is 50 ° C lower than the melting point of the first sheet 1 and does not reach the melting point, and more preferably it is preheated to a temperature lower than the melting point of the first sheet 1 Above 20 ° C and below 5 ° C below the melting point. (2) The second sheet 2 is preferably preheated to a temperature that is 50 ° C lower than the melting point of the second sheet 2 and does not reach the melting point, and more preferably is preheated to a temperature lower than the melting point of the second sheet 2 A temperature above 20 ° C and below 5 ° C below the melting point. The preheating temperature of each of the first sheet 1 and the second sheet 2 is preferably 100 ° C. or higher, more preferably 130 ° C. or higher, from the viewpoint of easily forming the through-holes 14. From the viewpoint of adhesion or prevention of winding on the conveying roller, it is preferably 150 ° C or lower, and more preferably 145 ° C or lower. In addition, from the viewpoint of easily forming the fused portion 4 and the through hole 14, it is sandwiched between the front end surface 35c of the convex portion 35 of the first roller 31 and the front end surface 42t of the ultrasonic horn 42 and is applied to the first and second pieces. The pressing force of the materials 1 and 2 is preferably 10 N / mm or more, more preferably 15 N / mm or more, more preferably 150 N / mm or less, even more preferably 120 N / mm or less, and more preferably 10 N / mm or more and 150 N / mm or less, more preferably 15 N / mm or more and 120 N / mm or less. The applied pressure referred to here is the so-called linear pressure, which is the sum of the applied pressure (N) of the ultrasonic welding head 42 divided by the tooth width (X direction) of the convex portion 35 in contact with the ultrasonic welding head 42 (excluding the first The value (the pressure per unit length) obtained by the length of the concave portion of 1 roll 31 is expressed. Further, from the viewpoint of easily forming the fused portion 4 and the through hole 14, the frequency of the applied ultrasonic vibration is preferably 15 kHz or more, more preferably 20 kHz or more, and more preferably 50 kHz or less, and more preferably 40 kHz or less, preferably 15 kHz or more and 50 kHz or less, and more preferably 20 kHz or more and 40 kHz or less. [Frequency measurement method] Use a laser shift meter to measure the displacement of the front end of the horn. The frequency is measured by setting the sampling frequency to 200 kHz or more and the accuracy to 1 μm or more. In addition, from the viewpoint of easily forming a fusion portion and a through hole, the amplitude of the applied ultrasonic vibration is preferably 20 μm or more, more preferably 25 μm or more, and further preferably 50 μm or less, and more preferably 40 μm. Hereinafter, it is more preferably 20 μm or more and 50 μm or less, and more preferably 25 μm or more and 40 μm or less. [Measurement method of amplitude] Use a laser shift meter to measure the displacement of the horn tip. The amplitude was measured by setting the sampling frequency to 200 kHz or more and the accuracy to 1 μm or more. Next, the second and third embodiments of the method for producing a composite sheet of the present invention will be described. In the second embodiment, the above-mentioned composite sheet 10 is manufactured using the composite sheet manufacturing apparatus of the second embodiment showing the main part of FIG. 6. The manufacturing apparatus of the composite sheet of the second embodiment is only in the aspect of replacing the heater 61 (preheating mechanism) arranged in the first roller 31 with a mechanism for heating the ultrasonic welding head 42 of the ultrasonic fusion machine 41, It is different from the manufacturing apparatus 20 of the said composite sheet. More specifically, the apparatus for manufacturing a composite sheet according to the second embodiment includes a heater 62 mounted on the ultrasonic horn 42 as a mechanism for heating the ultrasonic horn 42. In the manufacturing method of the composite sheet of the second embodiment, by controlling the temperature of the ultrasonic horn 42 heated by the heater 62, the temperature of the second sheet 2 immediately before the application of ultrasonic vibration is heated in advance Under the condition that the melting point of the sheet 2 is less than 50 ° C lower than the melting point, in this state, it is sandwiched between the convex portion 35 of the first roller 31 and the ultrasonic welding head 42 of the ultrasonic fusion machine. The first and second sheets 1 and 2 are subjected to ultrasonic vibration. When the ultrasonic welding head 42 is heated by a heating mechanism such as a heater 62, in a state where ultrasonic vibration is applied by an ultrasonic fusion machine, the first and second sheets 1 and 2 generate heat and are difficult to measure. The temperature of the sheet heated by the preheating mechanism. Therefore, in the case where one or both of the first and second sheets 1 and 2 are preheated via the heated ultrasonic welding head 42, the ultrasonic vibration is not generated, and the measurement is performed only after heating for 30 minutes. The temperature of the front end 42t of the ultrasonic horn was set to the temperature of the sheet heated by the preheating mechanism. The points that are not particularly explained about the second embodiment are the same as those of the first embodiment, and the description about the first embodiment is appropriately applied. In the third embodiment, the above-mentioned composite sheet 10 is manufactured by using a manufacturing apparatus for a composite sheet according to the third embodiment, which shows the main part. The apparatus for manufacturing a composite sheet according to the third embodiment does not include a preheating mechanism for heating at least one of the first sheet and the second sheet to a specific temperature before applying ultrasonic vibration. On the other hand, Yu Chao A front end of the sonic horn 42 is provided with a heat storage member 7 (hereinafter also referred to as a "heat storage material"). In the manufacturing method of the third embodiment, the first sheet 1 is introduced into the engaging portion 33 of the first and second rollers 31 and 32 to be deformed into a concave-convex shape in the same manner as the manufacturing method of the first embodiment. After that, the first sheet 1 deformed into a concave-convex shape is conveyed toward the application unit 36 of the ultrasonic vibration while being held on the first roller 31, and the second sheet 2 is overlapped with the first sheet 1 being conveyed. The superimposed two sheets 1 and 2 are sandwiched between the convex portion 35 of the first roller 31 and the front end face 42t of the ultrasonic welding head 42 of the ultrasonic fusion machine, and an ultrasonic wave is applied to the ultrasonic vibration application portion 36. vibration. In the manufacturing method of the third embodiment, as shown in FIG. 7, the application of the ultrasonic vibration is performed in a state in which a heat storage material 7 is disposed at the front end of the ultrasonic horn 42. According to the manufacturing method of the third embodiment, the temperature of the front end of the ultrasonic welding head 42 including the heat storage material 7 is immediately after the operation of the manufacturing device of the composite sheet is at the temperature of the first and second sheets 1 and 2. Below the melting point, but if the operation continues, the heat of the first and second sheets 1 and 2 that are generated by ultrasonic vibration is accumulated in the heat storage material 7, and the temperature of the heat storage material 7 rises to become the first sheet 1 and the second The melting point of the sheet 2 or more. Then, in a state where the temperature of the heat storage material 7 is above the melting point of each of the first sheet 1 and the second sheet 2, the conditions when the ultrasonic vibration is applied, for example, the wavelength, intensity, When the sheets 1 and 2 are pressurized and the like, when the ultrasonic vibration is applied, the two sheets 1 and 2 are melted, and if the through holes 14 penetrating the two sheets 1 and 2 are formed to be surrounded by the molten portion, State, the fusion portion 4 having the through-holes 14 can be reliably formed, and troubles such as the adherence of the molten resin to the conveying mechanism or the winding of the sheet to the conveying roller caused by the melting of the sheet are not easy to occur, so the maintenance of the device The burden is also smaller. In addition, since the formation of the fusion portion 4 and the formation of the through hole 14 are performed simultaneously between the convex portion 35 of the first roller 31 and the ultrasonic welding head 42 of the ultrasonic fusion machine, the position and penetration of the fusion portion 4 are formed. There is no positional shift between the positions of the holes 14. The thermal storage material 7 has a lower thermal conductivity than a metal constituting at least the ultrasonic horn 42. The thermal storage material 7 preferably has a thermal conductivity measured by the following method of 2.0 W / mK or less. The thermal conductivity of the heat storage material is preferably 2.0 W / mK or less, more preferably 1.0 W / mK or less, from the viewpoint that it is not easy to radiate heat to the ultrasonic welding head or the atmosphere. From the viewpoint of efficiently heating the sheet, In particular, it is preferably 0.1 W / mK or more, more preferably 0.5 W / mK or more, and still more preferably 0.1 W / mK or more and 2.0 W / mK or less, more preferably 0.5 W / mK or more and 1.0 W / mK or less. [Method for Measuring Thermal Conductivity] The thermal conductivity of the heat storage material 7 is measured using a thermal conductivity measuring device. The heat storage material 7 is preferably one having heat resistance. The heat-resistant temperature of the heat storage material 7 is preferably 150 ° C or higher, more preferably 200 ° C or higher, and even more preferably 250 ° C or higher. There is no particular upper limit of the heat-resistant temperature, and it is, for example, 1500 ° C or lower. The heat storage material 7 may also include a body part having heat storage properties and an adhesive layer for adhering the body to an ultrasonic welding head. In this case, the thermal conductivity is measured by excluding the adhesive part. As the heat storage material, for example, commercially available products such as "glass cloth tape" manufactured by Nitto Denko and "polyimide tape for heat-resistant insulation" manufactured by Nitto Denko can also be used. Examples of the material of the heat storage material 7 having a heat storage body include glass, polyimide, and the like. From the viewpoint of having moderate heat storage and high heat resistance, polyimide and the like are preferred. The heat storage material 7 may be a single-layered sheet, or a laminated body such as two or more sheets including the same or different materials. The heat storage material 7 preferably has a shape that is longer in the same direction than the front end surface of the ultrasonic horn 42 that is longer in the axial length direction of the first roller 31. In addition, from the viewpoint of preventing seizure when the ultrasonic wave is applied, the heat storage material 7 is preferably as shown in FIG. 7. In addition to covering the front end face of the ultrasonic horn 42, it also has The portion of the corner portion 42a on the upstream side (left side in FIG. 7) of the sheet traveling direction of the end surface 42t is preferably the downstream side of the sheet traveling direction (the right side in FIG. 7) having the end surface 42t covering the front of the ultrasonic horn 42 Part of the corner portion 42b. Polyimide used in the body portion of the heat storage material 7 is also preferred in terms of excellent abrasion resistance and heat resistance, and is a synthetic resin that has the property of generating heat even when it receives ultrasonic vibration. From the same point of view, the synthetic resin layer 42h provided on the body portion of the thermal storage material 7 or the ultrasonic horn 42 shown in FIG. 8 (a) preferably includes polyimide or polybenzimidazole, poly Synthetic resins such as ether ethyl ketone, polyphenylene sulfide, polyetherimide, polyimide, imine, etc. with a Rockwell hardness of R120 or more and R140 or less, and a heat resistance temperature of 150 or more and 500 or less Including synthetic resins such as polyimide or polybenzimidazole with a Rockwell hardness of R125 or more and R140 or less, and a heat resistance temperature of 280 ° C or more and 400 ° C or less. Here, the Rockwell hardness is a value measured according to ASTM D785, and the heat resistance temperature is a value measured according to ASTM D648. The heat-resistant temperature of the synthetic resin layer provided at the front end of the ultrasonic horn 42 is preferably 150 ° C or higher, more preferably 280 ° C or higher, further preferably 500 ° C or lower, more preferably 400 ° C or lower, and The temperature is preferably 150 ° C or higher and 500 ° C or lower, and more preferably 280 ° C or higher and 400 ° C or lower. The Rockwell hardness of the synthetic resin layer provided at the front end of the ultrasonic horn 42 is preferably R120 or more, more preferably R125 or more, more preferably R140 or less, and still more preferably R120 or more and R140 or less. It is preferably R125 or more and R140 or less. Fig. 8 (a) is a view showing another example of the ultrasonic welding head 42 in which the heat storage material 7 is provided at the front end portion. In FIG. 8 (a), the circle C2 portion is an enlarged cross-sectional view of the circle C1 portion. In the ultrasonic welding head 42 shown in FIG. 8 (a), as shown in FIG. 8 (b), the front end face 42t of the body portion 42c of the ultrasonic welding head 42 including a metal such as an aluminum alloy or a titanium alloy. After forming a connecting layer 42f having a gap 42e from one surface 42d to the inside by thermal spraying, as shown in FIG. 8 (a), a synthetic resin layer as a member having heat storage properties is fixed on the side 42d of the connecting layer 42f. 42h. The so-called thermal spraying refers to a surface treatment method in which particles of a thermal spraying material such as metal or ceramic which is melted or nearly melted by heating are accelerated to collide with a substrate surface at a high speed, and a film is formed on the substrate surface. A synthetic resin layer 42h having a heat storage property is provided on the front end surface 42t of the main body portion 42c of the ultrasonic horn 42 including a metal such as titanium alloy through a connection layer 42f formed by thermal spraying. The material of the resin layer 42h is excellent in abrasion resistance and heat resistance. On the other hand, even in the case of using a synthetic resin such as polyimide, which is not easy to obtain sufficient fixing strength when directly fixed, it is also easy. Ground to obtain sufficient fixed strength. In addition, if the fixing strength is insufficient, defects such as peeling of the synthetic resin layer 42h are likely to occur during the production of the composite sheet 10. As the heat-spraying material used to form the connection layer 42f, those which can be heat-sprayed and can help improve the fixing strength of the synthetic resin layer 42h having heat storage properties can be used without particular limitation. From the viewpoint of excellent bonding strength of the body portion 42c of the ultrasonic horn 42 and excellent wear resistance or heat resistance, ceramics such as tungsten carbide, zirconia, and chromium carbide, aluminum magnesium, zinc aluminum, and the like are preferably used. Metals such as alloys, aluminum, stainless steel, titanium, molybdenum, and cermets as composite materials of metals and ceramics are more preferably ceramics from the viewpoint of forming voids 42e that improve the fixed strength of the synthetic resin layer 42h. To use tungsten carbide. In addition, the forming material of the connecting layer 42f has a higher melting point than the synthetic resin constituting the synthetic resin layer 42h having heat storage properties, and maintains the shape of the void 42e when the synthetic resin 42h is formed. From the viewpoint of improving the fixing strength of the synthetic resin layer 42h It ’s better. Examples of the method for fixing the synthetic resin layer 42h having heat storage property to the connecting layer 42f include a method of dipping the connecting layer 42f in a synthetic resin melted by heating; and applying a synthetic resin melted by heating to A method for connecting the layer 42f; a method for pressing the plate-shaped body of the softened synthetic resin against the connection layer 42f; The thickness Tf of the connecting layer 42f [see FIG. 8 (a)] is not particularly limited. If an example is given, it is preferably 10 μm or more, more preferably 20 μm or more, and further preferably 100 μm or less, and more preferably 50 μm. μm or less, more preferably 10 μm or more and 100 μm or less, and more preferably 20 μm or more and 50 μm or less. The thickness Th of the synthetic resin layer 42h having heat storage properties [refer to FIG. 8 (a)] is not particularly limited. If an example is given, it is preferably 5 μm or more, more preferably 10 μm or more, and still more preferably 100 μm or less. , More preferably 50 μm or less, more preferably 5 μm or more and 100 μm or less, and even more preferably 10 μm or more and 50 μm or less. In addition, the ratio of the thickness Tf of the connection layer 42f to the total thickness Tt of the thickness Tf and the thickness Th of the synthetic resin layer 42h is preferable from the viewpoint of maintaining the fixed strength of the synthetic resin and not hindering ultrasonic vibration or heat generation. 30% or more, more preferably 50% or more, more preferably 85% or less, more preferably 75% or less, still more preferably 30% or more and 85% or less, more preferably 50% or more and 75% or more the following. Even if it is a manufacturing apparatus of a composite sheet having a heat storage material 7 like the third embodiment, it may have a preheating mechanism 6 provided in the manufacturing apparatus of the composite sheet of the first embodiment or a composite sheet of the second embodiment. A mechanism for heating the ultrasonic welding head 42 provided in the material manufacturing apparatus. It is preferable that the composite sheet 10 manufactured in each said embodiment has the following structures. The height H (see FIG. 1) of the convex portion 5 is 1 to 10 mm, and particularly preferably 3 to 6 mm. Composite sheet 10 per unit area (1 cm 2 The number of convex portions 5) is 1-20, and particularly preferably 6-15. The bottom dimension A (see FIG. 1) of the convex portion 5 in the X direction is 0.5 to 5.0 mm, and particularly preferably 1.0 to 4.0 mm. The bottom dimension B (see FIG. 1) of the convex portion 5 in the Y direction is 1.0 to 10 mm, and particularly preferably 2.0 to 7.0 mm. The ratio of the bottom dimension A in the X direction to the bottom dimension B in the Y direction (bottom dimension A: bottom dimension B) is 1: 1 to 1:10, particularly preferably 1: 2 to 2: 5. The bottom area (bottom size A × bottom size B) of the protrusion 5 is 0.5 to 50 mm 2 , Especially good for 2 ~ 20 mm 2 . The size C (see FIG. 1) of the fusion zone 4 in the X direction is 0.5 to 2 mm, particularly preferably 0.8 to 1.5 mm, and the size D (see FIG. 1) in the Y direction is 1.0 to 5.0 mm, and particularly preferably 1.2 to 3.0. mm. The ratio of the dimension C in the X direction to the dimension D in the Y direction (dimension C: dimension D) is 1: 1 to 1: 3, particularly preferably 2: 3 to 2: 5. The inner area of the fusion portion 4 from the outer periphery is preferably 0.5 mm 2 Above, more preferably 1.0 mm 2 Above, again, preferably 5.0 mm 2 Below, more preferably 4.0 mm 2 Below, again, preferably 0.5 mm 2 Above 5.0 mm 2 Below, more preferably 1.0 mm 2 Above 4.0 mm 2 the following. The area on the inner side of the fusion portion 4 from the outer periphery also includes the area of the through hole 14. The opening area of the through hole 14 is preferably 50% or more, more preferably 80% or more, and more preferably less than 100%, and more preferably 95% or less with respect to the area on the inner side of the fusion portion 4 than the outer periphery. Moreover, it is preferably 50% or more and 100% or less, and more preferably 80% or more and 95% or less. The above-mentioned composite sheet 10 is preferably used as a surface sheet of absorbent articles such as disposable diapers, menstrual tampons, sanitary pads, incontinence pads and the like. Moreover, it can also be used for applications other than the surface sheet of an absorbent article. For example, as a sheet for an absorbent article, a sheet disposed between a surface sheet and an absorbent body, a sheet for forming a three-dimensional wrinkle (leak-proof wall) (particularly a sheet forming an inner wall of a wrinkle) can be used. ), Etc., and for applications other than absorbent articles, it can be used as a cleaning sheet, especially a cleaning sheet mainly for liquid absorption, or a cosmetic sheet for humans. When it is used for cleaning a sheet, the convex part has a good followability to a non-smooth surface to be cleaned. Therefore, it is preferable to use the first nonwoven fabric side toward the surface to be cleaned. When it is used as a cosmetic sheet, it can follow the skin of the subject in the convex part, and it can show the massage effect, and it can absorb excess makeup (other use) or sweat, so it is better to use the first non-woven fabric. Use with the side facing the skin. The manufacturing method and manufacturing apparatus of the composite sheet of the present invention are not limited in any way by the foregoing embodiments, and can be appropriately modified. For example, the above-mentioned composite sheet 10 is formed with one fused portion in each recessed portion, but the composite sheet manufactured in the present invention may also include a plurality of fused portions in one recessed portion. Moreover, although the convex part 5 of the composite sheet 10 is a quadrangular frustum shape, it may be a hemispherical shape or the like. Moreover, the extent to which the convex portion 5 and the fusion portion 4 in the mutually adjacent rows are shifted in the X direction may replace the ½ pitch, 1/3 pitch, 1/4 pitch, etc., and may not be in the X direction. Offset. In addition, the plan view shapes of the fused portion and the through hole may be oval, circular, polygonal (corner, rectangle, triangle, diamond, etc.) with rounded corners. In addition, the manufactured composite sheet 10 may be one in which convex portions and fusion portions are formed as shown in FIG. 4 or FIG. 5 of Japanese Patent Laid-Open No. 2016-116582, or Japanese Patent Laid-Open No. 2016-116583 In the aspect shown in FIG. 3 of the publication, a convex portion and a fused portion are formed. In addition, instead of setting all of the fused portions of the composite sheet as a fused portion having a through hole, one of the fused portions of the composite sheet may be a fused portion with a through hole. For example, one or both of the first and second sheets in the central region in the width direction of the band-shaped composite sheet may be preheated to form a fusion portion having a through hole. Preheating is performed across both the first and second sheets in the side region of the center region to form a fused portion without a through hole. Regarding the embodiment (aspect) of the present invention described above, the following method for manufacturing a composite sheet and a device for manufacturing a composite sheet will be disclosed. <1> A method for manufacturing a composite sheet, the composite sheet having a plurality of fused portions where the first sheet and the second sheet are fused, and at least a part of the first sheet except for the fused portion A method of manufacturing a composite sheet is provided by forming a convex portion protruding to the side opposite to the second sheet side. The forming step includes rotating a first roll and a second roll that have irregularities that engage with each other on the peripheral surface. , While introducing the first sheet to the engaging portions of the two rolls to deform it into a concave-convex shape; in the overlapping step, the first sheet deformed into the concave-convex shape is held on the first roll while being conveyed And superimposing the second sheet on the first sheet during transportation; and an ultrasonic processing step of sandwiching the two overlapping sheets between the convex portion of the first roller and the ultrasonic wave of the ultrasonic fusion machine Ultrasonic vibration is applied between the welding heads; in the above-mentioned ultrasonic processing step, when the ultrasonic vibration is applied, the fusion portion having a through hole is formed. <2> The method for manufacturing a composite sheet according to the above <1>, wherein the ultrasonic welding head is heated to a specific temperature, and in the ultrasonic processing step, the first sheet is heated together with the application of the ultrasonic vibration And at least one of the second sheet. <3> The method for producing a composite sheet according to <1> or <2>, wherein the first roll is heated to a specific temperature, and the first sheet and the first sheet are heated in advance before the ultrasonic vibration is applied. At least one of 2 sheets. <4> The method for producing a composite sheet according to any one of <1> to <3>, wherein at least one of the first sheet and the second sheet is applied before the ultrasonic vibration is applied. Directly preheat to a specific temperature. <5> The method for producing a composite sheet according to any one of the above <2> to <4>, wherein the specific temperature does not reach the melting point of the first sheet or the second sheet, which is lower than the melting point, Above 50 ° C. <6> The method for producing a composite sheet according to any one of <1> to <5>, wherein in the above-mentioned ultrasonic processing step, a member having heat storage properties is arranged at an end portion before the above-mentioned ultrasonic welding head. The above-mentioned application of the ultrasonic vibration is performed in a state of, and when the ultrasonic vibration is applied, the fused portion having a through hole is formed. <7> The method for manufacturing a composite sheet according to the above <6>, wherein the thermal storage member has a lower thermal conductivity than a material constituting the ultrasonic horn. <8> The method for producing a composite sheet according to the above <6> or <7>, wherein the thermal conductivity of the heat storage member is 2.0 W / mK or less, preferably 1.0 W / mK or less. 0.1 W / mK or more, preferably 0.5 W / mK or more, and 0.1 W / mK or more and 2.0 W / mK or less, preferably 0.5 W / mK or more and 1.0 W / mK or less. <9> The method for producing a composite sheet according to any one of <6> to <8>, wherein the heat storage member has heat resistance, and the heat storage member has a heat resistance temperature of 150 ° C or higher, The temperature is preferably 200 ° C. or higher, more preferably 250 ° C. or higher, and the upper limit of the heat-resistant temperature of the heat storage member is 1500 ° C. or lower. <10> The method for producing a composite sheet according to any one of the above <6> to <9>, wherein the material of the heat storage member is glass or polyimide. <11> The method for manufacturing a composite sheet according to any one of the above <6> to <10>, wherein the member having heat storage properties has a function of covering the ultrasonic wave in addition to a portion covering the front end face of the ultrasonic horn. The portion of the corner on the upstream side of the sheet on the front face of the horn. <12> The method for manufacturing a composite sheet according to the above <11>, wherein the member having heat storage properties further has a corner portion covering a downstream side of the sheet in the direction of travel of the sheet on the front end face of the ultrasonic horn. <13> The method for manufacturing a composite sheet according to any one of the above <1> to <12>, wherein the first end face of the first roller and the front end face of the ultrasonic welding head are sandwiched between the first end face of the ultrasonic welding head and the first end face. The pressure applied by one sheet and the second sheet is 10 N / mm or more, preferably 15 N / mm or more, and 150 N / mm or less, and preferably 120 N / mm or less. 10 N / mm or more and 150 N / mm or less, preferably 15 N / mm or more and 120 N / mm or less. <14> The method for manufacturing a composite sheet according to any one of the above <1> to <13>, wherein the frequency of the above-mentioned ultrasonic vibration is 15 kHz or more, preferably 20 kHz or more, and 50 kHz Hereinafter, it is preferably 40 kHz or less, and 15 kHz or more and 50 kHz or less, and more preferably 20 kHz or more and 40 kHz or less. <15> The method for producing a composite sheet according to any one of the above <1> to <14>, wherein the amplitude of the ultrasonic vibration applied is 20 μm or more, preferably 25 μm or more, and 50 μm Hereinafter, it is preferably 40 μm or less, and more preferably 20 μm or more and 50 μm or less, and more preferably 25 μm or more and 40 μm or less. <16> The method for manufacturing a composite sheet according to any one of the above <1> to <15>, wherein the composite sheet is used as an absorbent article such as disposable diapers, menstrual cotton, sanitary pads, incontinence pads, etc. Surface sheet. <17> An apparatus for manufacturing a composite sheet, the composite sheet having a plurality of fused portions where the first sheet and the second sheet are fused, and at least a part of the first sheet except for the fused portion A convex portion protruding toward the opposite side to the second sheet side is formed, and the manufacturing apparatus of the composite sheet includes: a concave-convex forming portion having a first roller and a second roller having irregularities that mesh with each other on a peripheral surface portion, And deforming the first sheet introduced into the meshing portion of the two rolls into a concave-convex shape; and an ultrasonic processing section including an ultrasonic fusion machine, and superimposing the second sheet on the deformed concave-convex shape After the state of the first sheet, the two sheets are sandwiched between the convex portion of the first roller and the ultrasonic welding head of the ultrasonic fusion machine to locally apply ultrasonic vibration to form a through hole. The above-mentioned fusion portion of the hole. <18> The apparatus for manufacturing a composite sheet according to the above <17>, which includes a mechanism for heating the ultrasonic horn. <19> The device for manufacturing a composite sheet according to the above <17> or <18>, which includes a preheating mechanism that applies the first sheet and the second sheet before the ultrasonic vibration is applied. At least one is preheated to a specific temperature. <20> The device for manufacturing a composite sheet according to the above <19>, wherein the preheating mechanism is a heater arranged in the first roller. <21> The device for manufacturing a composite sheet according to the above <19> or <20>, wherein the first sheet is heated to a temperature lower than the melting point of the sheet and lower than the melting point by the preheating mechanism. Above 50 ° C. <22> The manufacturing apparatus for a composite sheet according to any one of the above <19> to <21>, wherein the preheating mechanism is used to preheat to a temperature 20 ° C or lower than the melting point of the first sheet. And below 5 ° C below the melting point. <23> The apparatus for producing a composite sheet according to any one of the items <17> to <22>, wherein a member having a heat storage property is arranged at the front end portion of the ultrasonic horn. <24> The device for manufacturing a composite sheet according to the above <23>, wherein the heat storage member has a lower thermal conductivity than a material constituting the ultrasonic horn. <25> The device for manufacturing a composite sheet according to the above <23> or <24>, wherein the thermal conductivity of the heat storage member is 2.0 W / mK or less, preferably 1.0 W / mK or less, and is 0.1 W / mK or more, preferably 0.5 W / mK or more, and 0.1 W / mK or more and 2.0 W / mK or less, preferably 0.5 W / mK or more and 1.0 W / mK or less. <26> The device for manufacturing a composite sheet according to any one of the above <23> to <25>, wherein the heat storage member has heat resistance, and the heat storage member has a heat resistance temperature of 150 ° C or higher, The temperature is preferably 200 ° C. or higher, more preferably 250 ° C. or higher, and the upper limit of the heat-resistant temperature of the heat storage member is 1500 ° C. or lower. <27> The device for manufacturing a composite sheet according to any one of the above <23> to <26>, wherein the member having heat storage properties has a coating on the ultrasonic wave in addition to a portion covering the front end face of the ultrasonic horn. The portion of the corner on the upstream side of the sheet on the front face of the horn. <28> The device for manufacturing a composite sheet according to the above <27>, wherein the heat storage member further has a corner portion covering the downstream side of the sheet in the direction of travel of the sheet on the front end face of the ultrasonic horn. <29> The device for producing a composite sheet according to any one of the above <23> to <28>, wherein the material of the heat storage member is glass or polyimide. <30> The apparatus for manufacturing a composite sheet according to any one of the items <23> to <29>, in which a heat-resistant synthetic resin is provided as a member having heat storage property at the front end of the ultrasonic horn. Floor. <31> The device for manufacturing a composite sheet according to the above <30>, wherein the heat-resistant temperature of the synthetic resin layer is 150 ° C or higher, preferably 280 ° C or higher, and 500 ° C or lower, preferably 400 ° C or lower, The temperature is 150 ° C or higher and 500 ° C or lower, preferably 280 ° C or higher and 400 ° C or lower. <32> The device for manufacturing a composite sheet according to any one of the items <23> to <31>, wherein the front end portion of the ultrasonic horn is provided with a wear-resistant member as a member having heat storage properties. Synthetic resin layer. <33> The device for manufacturing a composite sheet according to the above <32>, wherein the Rockwell hardness of the synthetic resin layer is R120 or more, preferably R125 or more, and R140 or less, and R120 or more and R140 or less, It is preferably R125 or more and R140 or less. <34> The apparatus for producing a composite sheet according to any one of the items <30> to <33>, wherein the synthetic resin layer is fixed to the ultrasonic welding head through a connection layer formed by thermal spraying. Front end face of metal body part. <35> The apparatus for manufacturing a composite sheet according to any one of <17> to <34>, wherein the first sheet and the first sheet are sandwiched between the convex portion of the first roller and the ultrasonic welding head. The pressure applied by the second sheet is 10 N / mm or more, preferably 15 N / mm or more, 150 N / mm or less, preferably 120 N / mm or less, and 10 N / mm. Above 150 N / mm, preferably above 15 N / mm and below 120 N / mm. <36> The device for manufacturing a composite sheet according to any one of the above <17> to <35>, wherein the frequency of the above-mentioned ultrasonic vibration is 15 kHz or more, preferably 20 kHz or more, and 50 kHz Hereinafter, it is preferably 40 kHz or less, and 15 kHz or more and 50 kHz or less, and more preferably 20 kHz or more and 40 kHz or less. <37> The device for manufacturing a composite sheet according to any one of <17> to <36>, wherein the amplitude of the ultrasonic vibration applied is 20 μm or more, preferably 25 μm or more, and 50 μm or less It is preferably 40 μm or less, more preferably 20 μm or more and 50 μm or less, and more preferably 25 μm or more and 40 μm or less. <38> The device for manufacturing a composite sheet according to any one of the above <17> to <37>, wherein the composite sheet is used as an absorbent article such as disposable diapers, menstrual cotton, sanitary pads, incontinence pads, etc. Surface sheet. [Industrial Applicability] According to the manufacturing method of the composite sheet of the present invention, a fused portion having a through hole can be easily formed, and a positional deviation is not easily generated between the position of the fused portion and the position of the through hole. The maintenance burden is also small. According to the manufacturing device of the composite sheet of the present invention, a fusion portion having a through hole can be easily formed, and a positional displacement is not easily generated between the position of the fusion portion and the position of the through hole, and the maintenance burden of the device is also small.

1‧‧‧第1片材1‧‧‧ the first sheet

2‧‧‧第2片材2‧‧‧ 2nd sheet

3‧‧‧凹部3‧‧‧ recess

4‧‧‧熔合部4‧‧‧ fusion section

5‧‧‧凸部5‧‧‧ convex

6‧‧‧預熱機構6‧‧‧preheating mechanism

7‧‧‧蓄熱材7‧‧‧ heat storage material

10‧‧‧複合片材10‧‧‧ composite sheet

14‧‧‧貫通孔14‧‧‧through hole

20‧‧‧製造裝置20‧‧‧Manufacturing equipment

30‧‧‧凹凸賦形部30‧‧‧ Bump forming section

31‧‧‧第1輥31‧‧‧Roll 1

31a、31b‧‧‧正齒輪31a, 31b‧‧‧‧Spur gear

32‧‧‧第2輥32‧‧‧ 2nd roller

33‧‧‧嚙合部33‧‧‧ meshing part

34‧‧‧抽吸孔34‧‧‧ Suction hole

35‧‧‧凸部35‧‧‧ convex

35c‧‧‧凸部35之前端面35c‧‧‧ convex 35 front face

36‧‧‧施加部36‧‧‧ Application Department

40‧‧‧超音波處理部40‧‧‧ Ultrasonic Processing Department

41‧‧‧超音波熔合機41‧‧‧ Ultrasonic fusion machine

42‧‧‧超音波焊頭42‧‧‧ Ultrasonic Welding Head

42a‧‧‧角部42a‧‧‧Corner

42b‧‧‧角部42b‧‧‧ Corner

42c‧‧‧本體部分42c‧‧‧Body

42d‧‧‧一面42d‧‧‧ side

42e‧‧‧空隙42e‧‧‧Gap

42f‧‧‧連接層42f‧‧‧ Connection layer

42h‧‧‧合成樹脂層42h‧‧‧Synthetic resin layer

42t‧‧‧超音波焊頭42之前端面42t‧‧‧ Ultrasonic Welding Head

43‧‧‧轉換器43‧‧‧ converter

44‧‧‧加速器44‧‧‧ accelerator

45‧‧‧可動台45‧‧‧ movable table

61‧‧‧加熱器61‧‧‧heater

62‧‧‧加熱器62‧‧‧heater

A‧‧‧凸部5之X方向之底部尺寸A‧‧‧ Bottom dimension of X direction of convex part 5

B‧‧‧凸部5之Y方向之底部尺寸B‧‧‧ Bottom dimension of Y direction of convex part 5

C‧‧‧X方向之尺寸C‧‧‧X dimension

C1‧‧‧圓C1‧‧‧circle

C2‧‧‧圓C2‧‧‧circle

D‧‧‧Y方向之尺寸D‧‧‧Y dimension

G‧‧‧空隙G‧‧‧Gap

Tf‧‧‧連接層42f之厚度Tf‧‧‧ thickness of connecting layer 42f

Th‧‧‧合成樹脂層42h之厚度Thickness of Th‧‧‧ synthetic resin layer 42h

Tt‧‧‧合計厚度Tt‧‧‧Total thickness

圖1係表示藉由本發明之複合片材之製造方法及裝置而製造之複合片材之一例的主要部分立體圖。 圖2係自第1片材側觀察圖1所示之複合片材之放大俯視圖。 圖3係表示本發明之複合片材之製造方法之第1實施態樣及本發明之複合片材之製造裝置之第1實施形態的概略圖。 圖4係將圖3所示之第1輥之主要部分放大表示之立體圖。 圖5係表示圖3所示之超音波焊接機之主要部分之圖,且表示自圖3中之左側觀察之狀態之圖。 圖6係表示本發明之複合片材之製造方法之第2實施態樣及本發明之複合片材之製造裝置之第2實施形態之主要部分的圖。 圖7係表示本發明之複合片材之製造方法之第3實施態樣及本發明之複合片材之製造裝置之第3實施形態之主要部分的圖。 圖8(a)係表示於前端部設置有具有蓄熱性之合成樹脂層之超音波焊頭之另一例的圖,圖8(b)係表示於包括鈦合金等金屬之超音波焊頭之本體部分之前端面,藉由熔射而僅形成連接層之狀態之圖。FIG. 1 is a perspective view of main parts showing an example of a composite sheet manufactured by the method and apparatus for manufacturing a composite sheet of the present invention. FIG. 2 is an enlarged plan view of the composite sheet shown in FIG. 1 as viewed from the first sheet side. Fig. 3 is a schematic view showing a first embodiment of a method for manufacturing a composite sheet of the present invention and a first embodiment of a device for manufacturing a composite sheet of the present invention. FIG. 4 is an enlarged perspective view showing a main part of the first roller shown in FIG. 3. FIG. 5 is a diagram showing a main part of the ultrasonic welding machine shown in FIG. 3 and a diagram showing a state viewed from the left side in FIG. 3. FIG. 6 is a diagram showing the main parts of the second embodiment of the method for manufacturing a composite sheet of the present invention and the second embodiment of the device for manufacturing a composite sheet of the present invention. FIG. 7 is a view showing a main part of a third embodiment of the method for manufacturing a composite sheet according to the present invention and the third embodiment of the device for manufacturing a composite sheet according to the present invention. Fig. 8 (a) is a view showing another example of an ultrasonic welding head provided with a synthetic resin layer having a heat storage property at a tip portion, and Fig. 8 (b) is a view showing a body of an ultrasonic welding head including a metal such as titanium alloy. A part of the front end surface is formed by a thermal spray to form only the connection layer.

Claims (38)

一種複合片材之製造方法,該複合片材具有第1片材及第2片材熔合之多個熔合部,且上述第1片材中之除上述熔合部以外之部分之至少一部分形成向與上述第2片材側為相反側突出之凸部,該複合片材之製造方法具備: 賦形步驟,其一面使於周面部具有相互嚙合之凹凸之第1輥及第2輥旋轉,一面將上述第1片材導入至該等兩輥之嚙合部而使之變形為凹凸形狀;重疊步驟,其將變形為凹凸形狀之上述第1片材一面保持於上述第1輥上一面搬送,且使上述第2片材重疊於搬送中之上述第1片材;及超音波處理步驟,其將重疊之兩個片材夾於上述第1輥之凸部與超音波熔合機之超音波焊頭之間而施加超音波振動;且 於上述超音波處理步驟中,於該超音波振動之施加時,形成具有貫通孔之上述熔合部。A method for manufacturing a composite sheet, the composite sheet having a plurality of fused portions where a first sheet and a second sheet are fused, and at least a part of the first sheet except for the fused portion is formed to be opposite to The second sheet side is a convex portion protruding on the opposite side. The manufacturing method of the composite sheet includes: a forming step of rotating the first roller and the second roller that have irregularities that engage with each other on the peripheral surface, and The first sheet is introduced into the meshing portion of the two rollers to deform it into a concave-convex shape; in the overlapping step, the first sheet deformed into the concave-convex shape is transported while holding the first sheet on the first roller, and The second sheet is superimposed on the first sheet being transported; and an ultrasonic processing step of sandwiching the two overlapped sheets between the convex portion of the first roller and the ultrasonic welding head of the ultrasonic fusion machine. In the above ultrasonic processing step, when the ultrasonic vibration is applied, the fused portion having a through hole is formed. 如請求項1之複合片材之製造方法,其中將上述超音波焊頭加熱至特定溫度,於上述超音波處理步驟中,與上述超音波振動之施加一同地加熱上述第1片材及上述第2片材之至少一者。For example, the method for manufacturing a composite sheet according to claim 1, wherein the ultrasonic horn is heated to a specific temperature, and in the ultrasonic processing step, the first sheet and the first sheet are heated together with the application of the ultrasonic vibration. At least one of 2 sheets. 如請求項1之複合片材之製造方法,其中將上述第1輥加熱至特定溫度,於上述超音波振動之施加之前,預先加熱上述第1片材及上述第2片材之至少一者。For example, the method for manufacturing a composite sheet according to claim 1, wherein the first roll is heated to a specific temperature, and at least one of the first sheet and the second sheet is heated in advance before the ultrasonic vibration is applied. 如請求項1之複合片材之製造方法,其中於上述超音波振動之施加之前,將上述第1片材及上述第2片材之至少一者直接預先加熱至特定溫度。For example, the method for manufacturing a composite sheet according to claim 1, wherein at least one of the first sheet and the second sheet is directly heated in advance to a specific temperature before the ultrasonic vibration is applied. 如請求項2之複合片材之製造方法,其中特定溫度係未達加熱之上述第1片材或上述第2片材之熔點,且為較該熔點低50℃之溫度以上。For example, the method for manufacturing a composite sheet according to claim 2, wherein the specific temperature is the melting point of the above-mentioned first sheet or the above-mentioned second sheet, which is not higher than the melting point by 50 ° C or more. 如請求項1之複合片材之製造方法,其中於上述超音波處理步驟中,於在上述超音波焊頭之前端部配置有具有蓄熱性之構件的狀態下進行上述超音波振動之施加,於該超音波振動之施加時,形成具有貫通孔之上述熔合部。For example, the method for manufacturing a composite sheet according to claim 1, wherein in the above-mentioned ultrasonic processing step, the application of the above-mentioned ultrasonic vibration is performed in a state where a member having a heat storage property is arranged at the front end of the above-mentioned ultrasonic welding head, in When the ultrasonic vibration is applied, the fused portion having a through hole is formed. 如請求項6之複合片材之製造方法,其中上述具有蓄熱性之構件與構成上述超音波焊頭之材料相比,熱導率較低。For example, the method for manufacturing a composite sheet according to claim 6, wherein the thermal storage member has a lower thermal conductivity than the material constituting the ultrasonic horn. 如請求項6之複合片材之製造方法,其中上述具有蓄熱性之構件之熱導率為0.1 W/mK以上且2.0 W/mK以下。The method for manufacturing a composite sheet according to claim 6, wherein the thermal conductivity of the above-mentioned member having thermal storage properties is 0.1 W / mK or more and 2.0 W / mK or less. 如請求項6之複合片材之製造方法,其中上述具有蓄熱性之構件具有耐熱性, 上述具有蓄熱性之構件之耐熱溫度為150℃以上且1500℃以下。The method for manufacturing a composite sheet according to claim 6, wherein the heat storage member has heat resistance, and the heat storage member has a heat resistance temperature of 150 ° C to 1500 ° C. 如請求項6之複合片材之製造方法,其中上述具有蓄熱性之構件之材料為玻璃或聚醯亞胺。The method for manufacturing a composite sheet according to claim 6, wherein the material of the heat storage member is glass or polyimide. 如請求項6之複合片材之製造方法,其中上述具有蓄熱性之構件除了被覆上述超音波焊頭之前端面之部分以外,還具有被覆該超音波焊頭之前端面之片材行進方向上游側的角部之部分。For example, the method for manufacturing a composite sheet according to claim 6, wherein in addition to the part having the heat storage property covering the part of the front end face of the ultrasonic horn, the member having the upstream side of the sheet traveling direction covering the front end face of the ultrasonic horn is also provided. Corner section. 如請求項11之複合片材之製造方法,其中上述具有蓄熱性之構件進而具有被覆上述超音波焊頭之前端面之片材行進方向下游側的角部之部分。The method for manufacturing a composite sheet according to claim 11, wherein the member having heat storage properties further has a portion covering a corner portion on a downstream side of a sheet in a traveling direction of the front end face of the ultrasonic horn. 如請求項1之複合片材之製造方法,其中夾於上述第1輥之凸部之前端面與上述超音波焊頭之前端面之間而對上述第1片材及上述第2片材施加之加壓力為10 N/mm以上且150 N/mm以下。For example, the method for manufacturing a composite sheet according to claim 1, wherein the first sheet and the second sheet are added between the front end surface of the convex portion of the first roller and the front end surface of the ultrasonic horn. The pressure is 10 N / mm or more and 150 N / mm or less. 如請求項1之複合片材之製造方法,其中施加之上述超音波振動之頻率為15 kHz以上且50 kHz以下。The method for manufacturing a composite sheet according to claim 1, wherein the frequency of the above-mentioned ultrasonic vibration is 15 kHz or more and 50 kHz or less. 如請求項1之複合片材之製造方法,其中施加之上述超音波振動之振幅為20 μm以上且50 μm以下。For example, the method for manufacturing a composite sheet according to claim 1, wherein the amplitude of the above-mentioned ultrasonic vibration is 20 μm or more and 50 μm or less. 如請求項1之複合片材之製造方法,其中上述複合片材係用作拋棄式尿布、經期衛生棉、衛生護墊、失禁護墊等吸收性物品之表面片材。For example, the method for manufacturing a composite sheet according to claim 1, wherein the composite sheet is used as a surface sheet for absorbent articles such as disposable diapers, menstrual tampons, sanitary pads, and incontinence pads. 一種複合片材之製造裝置,該複合片材具有第1片材及第2片材熔合之多個熔合部,且上述第1片材中之除上述熔合部以外之部分之至少一部分形成向與上述第2片材側為相反側突出之凸部,該複合片材之製造裝置具備: 凹凸賦形部,其具有於周面部具有相互嚙合之凹凸之第1輥及第2輥,且使導入至該等兩輥之嚙合部之上述第1片材變形為凹凸形狀;及超音波處理部,其具備超音波熔合機,且於使上述第2片材重疊於變形為凹凸形狀之狀態之上述第1片材上之後,將該等兩個片材夾於上述第1輥之凸部與上述超音波熔合機之超音波焊頭之間而局部地施加超音波振動,形成具有貫通孔之上述熔合部。An apparatus for manufacturing a composite sheet, the composite sheet having a plurality of fusion portions where a first sheet and a second sheet are fused, and at least a part of the first sheet except for the fusion portion is formed to be opposite to The second sheet side is a convex portion protruding on the opposite side, and the manufacturing apparatus of the composite sheet includes: a concave-convex forming portion having a first roller and a second roller that have convex and concave portions that mesh with each other on a peripheral surface portion, and is introduced. The above-mentioned first sheet to the meshing portion of the two rollers is deformed into a concave-convex shape; and the ultrasonic processing unit is provided with an ultrasonic fusion machine, and the above-mentioned second sheet is superimposed on the state deformed into an uneven shape. After the first sheet is placed, the two sheets are sandwiched between the convex portion of the first roll and the ultrasonic welding head of the ultrasonic fusion machine to locally apply ultrasonic vibration to form the above-mentioned through hole. Fusion section. 如請求項17之複合片材之製造裝置,其具備將上述超音波焊頭加熱之機構。The apparatus for manufacturing a composite sheet according to claim 17, further comprising a mechanism for heating the ultrasonic welding head. 如請求項17之複合片材之製造裝置,其具備預熱機構,該預熱機構將施加上述超音波振動之前之上述第1片材及上述第2片材之至少一者預熱至特定溫度。For example, the device for manufacturing a composite sheet according to claim 17 includes a preheating mechanism that preheats at least one of the first sheet and the second sheet before applying the ultrasonic vibration to a specific temperature. . 如請求項19之複合片材之製造裝置,其中上述預熱機構為配置於上述第1輥內之加熱器。The device for manufacturing a composite sheet according to claim 19, wherein the preheating mechanism is a heater arranged in the first roller. 如請求項19之複合片材之製造裝置,其中藉由上述預熱機構,而將上述第1片材加熱至未達該片材之熔點、且較該熔點低50℃之溫度以上。For example, the device for manufacturing a composite sheet according to claim 19, wherein the first sheet is heated to a temperature not higher than the melting point of the sheet and 50 ° C lower than the melting point by the preheating mechanism. 如請求項19之複合片材之製造裝置,其中藉由上述預熱機構,而預熱至較上述第1片材之熔點低20℃之溫度以上、且較該熔點低5℃之溫度以下。For example, the device for manufacturing a composite sheet according to claim 19, wherein the preheating mechanism is used to preheat to a temperature 20 ° C lower than the melting point of the first sheet and 5 ° C lower than the melting point. 如請求項17之複合片材之製造裝置,其中於上述超音波焊頭之前端部,配置有具有蓄熱性之構件。The manufacturing apparatus of the composite sheet according to claim 17, wherein a member having a heat storage property is arranged at the front end portion of the ultrasonic horn. 如請求項23之複合片材之製造裝置,其中上述具有蓄熱性之構件與構成上述超音波焊頭之材料相比,熱導率較低。For example, the device for manufacturing a composite sheet according to claim 23, wherein the thermal storage member has a lower thermal conductivity than the material constituting the ultrasonic horn. 如請求項23之複合片材之製造裝置,其中上述具有蓄熱性之構件之熱導率為0.1 W/mK以上且2.0 W/mK以下。For example, the device for manufacturing a composite sheet according to claim 23, wherein the thermal conductivity of the above-mentioned member having a heat storage property is 0.1 W / mK or more and 2.0 W / mK or less. 如請求項23之複合片材之製造裝置,其中上述具有蓄熱性之構件具有耐熱性, 上述具有蓄熱性之構件之耐熱溫度為150℃以上且1500℃以下。The manufacturing apparatus of the composite sheet according to claim 23, wherein the heat storage member has heat resistance, and the heat storage member has a heat resistance temperature of 150 ° C or more and 1500 ° C or less. 如請求項23之複合片材之製造裝置,其中上述具有蓄熱性之構件除了被覆上述超音波焊頭之前端面之部分以外,還具有被覆該超音波焊頭之前端面之片材行進方向上游側的角部之部分。For example, the device for manufacturing a composite sheet according to claim 23, wherein in addition to a part covering the front end face of the ultrasonic horn, the member having heat storage properties further includes a sheet on the upstream side of the direction of travel of the sheet covering the front end face of the ultrasonic horn. Corner section. 如請求項27之複合片材之製造裝置,其中上述具有蓄熱性之構件進而具有被覆上述超音波焊頭之前端面之片材行進方向下游側的角部之部分。The apparatus for manufacturing a composite sheet according to claim 27, wherein the member having heat storage properties further has a portion covering a corner portion on the downstream side of the sheet in the traveling direction of the front end face of the ultrasonic horn. 如請求項23之複合片材之製造裝置,其中上述具有蓄熱性之構件之材料為玻璃或聚醯亞胺。The device for manufacturing a composite sheet according to claim 23, wherein the material of the heat storage member is glass or polyimide. 如請求項23之複合片材之製造裝置,其中於上述超音波焊頭之前端部,作為具有蓄熱性之構件而設置有具有耐熱性之合成樹脂層。The manufacturing apparatus of the composite sheet according to claim 23, wherein a heat-resistant synthetic resin layer is provided as a member having heat storage property at the front end of the ultrasonic horn. 如請求項30之複合片材之製造裝置,其中上述合成樹脂層之耐熱溫度為150℃以上且500℃以下。The apparatus for manufacturing a composite sheet according to claim 30, wherein the heat-resistant temperature of the synthetic resin layer is 150 ° C or higher and 500 ° C or lower. 如請求項23之複合片材之製造裝置,其中於上述超音波焊頭之前端部,作為具有蓄熱性之構件而設置有具有耐磨損性之合成樹脂層。The manufacturing apparatus of the composite sheet according to claim 23, wherein a synthetic resin layer having abrasion resistance is provided as a member having heat storage property at the front end portion of the ultrasonic horn. 如請求項32之複合片材之製造裝置,其中上述合成樹脂層之洛氏硬度為R120以上且R140以下。The device for manufacturing a composite sheet according to claim 32, wherein the Rockwell hardness of the synthetic resin layer is R120 or more and R140 or less. 如請求項30之複合片材之製造裝置,其中上述合成樹脂層係隔著藉由熔射形成之連接層而固定於上述超音波焊頭之包含金屬之本體部分之前端面。For example, the device for manufacturing a composite sheet according to claim 30, wherein the synthetic resin layer is fixed to the front end face of the metal-containing body portion of the ultrasonic horn via a connection layer formed by thermal spraying. 如請求項17之複合片材之製造裝置,其中夾於上述第1輥之凸部與上述超音波焊頭之間而對上述第1片材及上述第2片材施加之加壓力為10 N/mm以上且150 N/mm以下。For example, the device for manufacturing a composite sheet according to claim 17, wherein the pressing force applied to the first sheet and the second sheet is sandwiched between the convex portion of the first roller and the ultrasonic welding head, and the pressure is 10 N. / mm to 150 N / mm. 如請求項17之複合片材之製造裝置,其中施加之上述超音波振動之頻率為15 kHz以上且50 kHz以下。For example, the device for manufacturing a composite sheet according to claim 17, wherein the frequency of the above-mentioned ultrasonic vibration is 15 kHz or more and 50 kHz or less. 如請求項17之複合片材之製造裝置,其中施加之上述超音波振動之振幅為20 μm以上且50 μm以下。For example, the apparatus for manufacturing a composite sheet according to claim 17, wherein the amplitude of the above-mentioned ultrasonic vibration is 20 μm or more and 50 μm or less. 如請求項17之複合片材之製造裝置,其中上述複合片材係用作拋棄式尿布、經期衛生棉、衛生護墊、失禁護墊等吸收性物品之表面片材。For example, the device for manufacturing a composite sheet according to claim 17, wherein the composite sheet is used as a surface sheet for absorbent articles such as disposable diapers, menstrual tampons, sanitary pads, and incontinence pads.
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