WO2023189108A1 - 共押出シート及び樹脂成形品 - Google Patents

共押出シート及び樹脂成形品 Download PDF

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Publication number
WO2023189108A1
WO2023189108A1 PCT/JP2023/007276 JP2023007276W WO2023189108A1 WO 2023189108 A1 WO2023189108 A1 WO 2023189108A1 JP 2023007276 W JP2023007276 W JP 2023007276W WO 2023189108 A1 WO2023189108 A1 WO 2023189108A1
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WO
WIPO (PCT)
Prior art keywords
skin layer
coextruded sheet
core layer
resin
thickness
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/JP2023/007276
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English (en)
French (fr)
Japanese (ja)
Inventor
敏晴 後藤
智史 山本
圭 水谷
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Maxell Ltd
Original Assignee
Maxell Ltd
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
Application filed by Maxell Ltd filed Critical Maxell Ltd
Priority to US18/575,112 priority Critical patent/US20250033336A1/en
Priority to EP23779138.9A priority patent/EP4501580A4/en
Priority to JP2024511510A priority patent/JPWO2023189108A1/ja
Priority to CN202380012429.XA priority patent/CN117561155A/zh
Priority to KR1020237044134A priority patent/KR20240012499A/ko
Publication of WO2023189108A1 publication Critical patent/WO2023189108A1/ja
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B27/00—Layered products comprising a layer of synthetic resin
    • B32B27/36—Layered products comprising a layer of synthetic resin comprising polyesters
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/04—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles consisting of at least two parts of chemically or physically different materials, e.g. having different densities
    • B29C44/0461—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles consisting of at least two parts of chemically or physically different materials, e.g. having different densities by having different chemical compositions in different places, e.g. having different concentrations of foaming agent, feeding one composition after the other
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/02—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles for articles of definite length, i.e. discrete articles
    • B29C44/12—Incorporating or moulding on preformed parts, e.g. inserts or reinforcements
    • B29C44/14—Incorporating or moulding on preformed parts, e.g. inserts or reinforcements the preformed part being a lining
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B29C44/00—Shaping by internal pressure generated in the material, e.g. swelling or foaming ; Producing porous or cellular expanded plastics articles
    • B29C44/34—Auxiliary operations
    • B29C44/36—Feeding the material to be shaped
    • B29C44/46—Feeding the material to be shaped into an open space or onto moving surfaces, i.e. to make articles of indefinite length
    • B29C44/50—Feeding the material to be shaped into an open space or onto moving surfaces, i.e. to make articles of indefinite length using pressure difference, e.g. by extrusion or by spraying
    • B29C44/505—Feeding the material to be shaped into an open space or onto moving surfaces, i.e. to make articles of indefinite length using pressure difference, e.g. by extrusion or by spraying extruding the compound through a flat die
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    • B32B5/18—Layered products characterised by the non- homogeneity or physical structure, i.e. comprising a fibrous, filamentary, particulate or foam layer; Layered products characterised by having a layer differing constitutionally or physically in different parts characterised by features of a layer of foamed material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001—Combinations of extrusion moulding with other shaping operations
    • B29C48/0012—Combinations of extrusion moulding with other shaping operations combined with shaping by internal pressure generated in the material, e.g. foaming
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/001—Combinations of extrusion moulding with other shaping operations
    • B29C48/0017—Combinations of extrusion moulding with other shaping operations combined with blow-moulding or thermoforming
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C48/00—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor
    • B29C48/03—Extrusion moulding, i.e. expressing the moulding material through a die or nozzle which imparts the desired form; Apparatus therefor characterised by the shape of the extruded material at extrusion
    • B29C48/07—Flat, e.g. panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29C—SHAPING OR JOINING OF PLASTICS; SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDED FOR; AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
    • B29C51/00—Shaping 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
    • B29C51/10—Forming by pressure difference, e.g. vacuum
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2069/00—Use of PC, i.e. polycarbonates or derivatives thereof, as moulding material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
    • B29K—INDEXING SCHEME ASSOCIATED WITH SUBCLASSES B29B, B29C OR B29D, RELATING TO MOULDING MATERIALS OR TO MATERIALS FOR MOULDS, REINFORCEMENTS, FILLERS OR PREFORMED PARTS, e.g. INSERTS
    • B29K2105/00—Condition, form or state of moulded material or of the material to be shaped
    • B29K2105/04—Condition, form or state of moulded material or of the material to be shaped cellular or porous
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B29—WORKING OF PLASTICS; WORKING OF SUBSTANCES IN A PLASTIC STATE IN GENERAL
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    • B—PERFORMING OPERATIONS; TRANSPORTING
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Definitions

  • the present disclosure relates to engineering plastics, particularly coextruded sheets and resin molded products containing polycarbonate resins.
  • foamed resins have attracted attention as they can increase convenience by reducing the weight of resin molded bodies and reduce carbon dioxide emissions.
  • Molding methods for foamed resin include physical foaming and chemical foaming.
  • the chemical foam molding method uses a chemical foaming agent as a foaming agent. Chemical blowing agents have a high environmental impact and are not preferred from the perspective of protecting the global environment.
  • the physical foaming method uses a physical foaming agent such as nitrogen or carbon dioxide as a foaming agent. Physical foaming agents have a small environmental impact and are therefore preferable from the perspective of protecting the global environment.
  • the physical foam molding method includes a method of foaming highly heat-resistant engineering plastics and super engineering plastics by shearing and kneading the molten resin of engineering plastics and super engineering plastics with high-pressure supercritical fluid. .
  • Patent Document 1 discloses a method for manufacturing a foam molded body using a relatively low pressure physical foaming agent such as nitrogen or carbon dioxide instead of a high pressure supercritical fluid. According to this method, fine foam cells can be formed in a resin molded body by a relatively simple process using a low-pressure physical foaming agent without using a special high-pressure device. Further, Patent Document 1 discloses a method of molding a foam molded article by injection molding and extrusion molding.
  • the injection molding method can produce foam molded products with complex shapes. However, the surface layer of the molten resin flows inside the mold while being cooled and solidified. At this time, a relatively thin non-foamed skin layer is formed on the surface layer of the foamed molded product.
  • the extrusion molding method has fewer restrictions on the size and load of the mold than the injection molding method, and is suitable for continuously producing foam molded products of a single shape and a single thickness. Further, the sheet-like foamed product obtained by extrusion molding can be shaped into a somewhat complicated shape or a relatively large size by applying vacuum forming or the like.
  • Patent Document 1 does not consider a foam molded product made of a polycarbonate resin made of a non-crystalline resin that can be vacuum formed, and the surface of the foam molded product when heated at a temperature exceeding the glass transition temperature of the polycarbonate resin. No consideration has been given to ensuring smoothness.
  • a non-foamed resin even if the crystalline resin is heated at a temperature higher than the glass transition temperature, it is unlikely to undergo large deformation or dimensional change if heated at a temperature lower than the melting point.
  • amorphous resins tend to be thermally deformed when heated at temperatures higher than the glass transition temperature (the glass transition temperature of polycarbonate resin is about 145° C.).
  • Patent Document 2 discloses a method for manufacturing a thermoplastic resin foam sheet. According to the method for manufacturing a thermoplastic resin foam sheet, a skin layer can be easily formed on the surface of the thermoplastic resin foam sheet by extrusion molding.
  • Patent Document 3 discloses a method for manufacturing a multilayer laminate molded product. The multilayer laminate molded product has a core layer and a skin layer made of foamed resin formed by coextrusion molding.
  • Patent Document 2 and the manufacturing method of Patent Document 3 use a general-purpose plastic such as polypropylene or polystyrene, which has relatively low heat resistance and mechanical strength, as the main resin material, and is an engineering material with excellent heat resistance and mechanical strength. No plastic, especially polycarbonate resin. Moreover, the manufacturing methods of Patent Document 2 and Patent Document 3 are intended for ease of manufacturing or stability of a foamed molded product, and are not intended for improving heat resistance and mechanical strength. Moreover, if the thickness of the skin layer is too large, that is, if the thickness of the core layer is too small, weight reduction cannot be achieved.
  • a general-purpose plastic such as polypropylene or polystyrene, which has relatively low heat resistance and mechanical strength, as the main resin material, and is an engineering material with excellent heat resistance and mechanical strength. No plastic, especially polycarbonate resin.
  • the manufacturing methods of Patent Document 2 and Patent Document 3 are intended for ease of manufacturing or stability of a foamed molded product, and are not intended for improving heat resistance and mechanical strength.
  • Patent Document 4 discloses an extruded polycarbonate resin foam laminate sheet in which a plurality of extruded polycarbonate resin foam sheets are bonded together.
  • Patent Document 4 a relatively thick polycarbonate resin foam sheet is manufactured by cutting and laminating extruded polycarbonate resin foam sheets, and the surface skin layer is controlled. It's not something you do.
  • resin molded bodies made of foamed resin have a problem in that their mechanical strength decreases due to lower density aimed at improving lightweight properties.
  • a foamed molded article made of polycarbonate resin that requires mechanical strength has a problem in that its mechanical strength is significantly lower than that of a resin molded article made of a non-foamed resin.
  • Patent Document 5 JP-A-8-174780 discloses a polycarbonate extruded resin foam laminate sheet with a high expansion ratio manufactured by a coextrusion method. Polycarbonate extruded resin foam laminate sheets have excellent heat processability, particularly deep drawing processability, and are also excellent in appearance design and mechanical strength. Patent Document 5 discloses a heating dimensional change when a polycarbonate extruded resin foam laminate sheet is heated in a relatively low temperature atmosphere of 170°C.
  • Patent Document 6 discloses a polycarbonate resin multilayer body.
  • the polycarbonate resin multilayer body consists of a polycarbonate resin foam and a polycarbonate resin film layer laminated and adhered to at least one side of the polycarbonate resin foam.
  • the melt tension of the constituent resin of the film layer at 250° C. is 2.45 cN or more.
  • the polycarbonate resin multilayer body does not cause deterioration of the surface condition or decrease in physical properties when the multilayer sheet is heated during heating vacuum forming, and there is no occurrence of cracks or cracks at the bent part during the bending process. .
  • Patent Document 7 discloses a polycarbonate resin foam board.
  • a polycarbonate resin foam board consists of a polycarbonate resin foam sheet and a polycarbonate resin film or sheet formed on at least one side of the foam sheet.
  • the polycarbonate resin foam board has improved surface appearance and bending strength by focusing on various conditions such as the density and thickness of the polycarbonate resin foam sheet.
  • Patent Documents 1 to 7 discuss the efficiency of vacuum forming polycarbonate extruded resin foam laminated sheets, etc., that is, vacuum forming can be performed at higher temperatures and in a shorter time, and that the coalescence of air bubbles after vacuum forming is suppressed, and the machine There are no suggestions regarding the sheet to improve its strength.
  • a polycarbonate laminated foam resin sheet with a high expansion ratio as disclosed in Patent Document 5 can obtain excellent lightness, but the mechanical strength is lower than that of a polycarbonate lamination foam resin sheet with a low expansion ratio. There was also.
  • the present inventors have found that in a coextruded sheet, if the MVR of the resin used for the core layer and the skin layer is controlled within a certain range, the coextrusion sheet including the core layer made of foamed resin can be used for weight reduction. It has been found that in an extruded sheet, it is possible to improve the production efficiency during heat forming such as vacuum forming, and to improve the mechanical strength after heat forming such as vacuum forming.
  • the present disclosure provides a coextruded sheet containing a polycarbonate resin and a coextruded sheet that can improve production efficiency in heat forming such as vacuum forming and improve mechanical strength after heat forming such as vacuum forming.
  • Our goal is to provide resin molded products.
  • the coextruded sheet according to the present disclosure includes a core layer containing a polycarbonate resin and made of a foamed resin, a first skin layer made of a non-foamed resin and laminated on one main surface of the core layer, and a core layer made of a foamed resin. It may also include a skin layer laminated on the other main surface.
  • the melt volume rate of the polycarbonate resin contained in the core layer (hereinafter referred to as MVRc) and the melt volume rate of the polycarbonate resin contained in either the first skin layer or the second skin layer (hereinafter referred to as MVRs). may satisfy the following formula (1). 1.5 ⁇ MVRs/MVRc ⁇ 8.0 (1)
  • the coextruded sheet and resin molded product according to the present disclosure it is possible to improve the mechanical strength after heat forming such as vacuum forming while improving the production efficiency in heat forming such as vacuum forming.
  • FIG. 1 is a perspective view showing a coextruded sheet according to an embodiment.
  • FIG. 2 is a sectional view showing the coextruded sheet shown in FIG. 1.
  • FIG. 3 is a cross-sectional view showing the coextruded sheet after heating.
  • FIG. 4 is a cross-sectional view showing the coextruded sheet after heating.
  • FIG. 5 is a perspective view showing a vacuum forming mold.
  • the coextruded sheet according to the present disclosure includes a core layer containing a polycarbonate resin and made of a foamed resin, a first skin layer made of a non-foamed resin and laminated on one main surface of the core layer, and a core layer made of a foamed resin. It may also include a skin layer laminated on the other main surface.
  • the melt volume rate of the polycarbonate resin contained in the core layer (hereinafter referred to as MVRc) and the melt volume rate of the polycarbonate resin contained in either the first skin layer or the second skin layer (hereinafter referred to as MVRs). may satisfy the following formula (1). 1.5 ⁇ MVRs/MVRc ⁇ 8.0 (1)
  • the coextruded sheet may satisfy the following formula (2). 1.5 ⁇ MVRs/MVRc ⁇ 2.5 (2) Thereby, it is possible to further improve production efficiency in heat forming such as vacuum forming.
  • the coextruded sheet 1 may satisfy the following formula (3). 1.7 ⁇ MVRs/MVRc ⁇ 2.3 (3) Thereby, it is possible to improve the mechanical strength after heat forming such as vacuum forming while shortening the takt time, and furthermore, it is possible to obtain excellent surface smoothness.
  • the coextruded sheet may have an apparent density of 0.4 to 0.8 g/cm 3 .
  • the coextruded sheet may have a thickness of 1.5 to 6 mm.
  • the coextruded sheet may satisfy the following formula (3). 0.10 ⁇ (t1+t2)/T ⁇ 0.5 (3)
  • t1 represents the thickness of the first skin layer
  • t2 represents the thickness of the second skin layer
  • T represents the thickness of the coextruded sheet.
  • the resin molded article of the present disclosure may be made of a coextruded sheet.
  • FIGS. 1 to 4 embodiments of the coextruded sheet 1 of the present disclosure will be specifically described using FIGS. 1 to 4.
  • the same reference numerals are attached to the same or corresponding components in the figures, and the same explanations will not be repeated. Note that, in order to make the explanation easier to understand, in the drawings referred to below, the configuration is shown in a simplified or schematic manner, and some structural members are omitted.
  • the coextruded sheet 1 is made of polycarbonate resin.
  • the coextruded sheet 1 according to this embodiment has a sheet shape.
  • the coextruded sheet 1 is manufactured by coextruding molten polycarbonate resin.
  • the resin used in the present disclosure may be other engineering plastics as long as they include polycarbonate resin. Since the coextruded sheet 1 contains polycarbonate resin, it has excellent toughness.
  • Engineering plastics are thermoplastic resins that have a deflection temperature under load of 100°C or higher. Examples of engineering plastics include polycarbonate resin (PC), modified polyphenylene ether (m-PPE), and syndiotactic polystyrene (SPS).
  • the resin used in the coextruded sheet 1 of the present disclosure can contain at least one selected from the group consisting of these engineering plastics.
  • the resin material of the coextruded sheet 1 may be any engineering plastic that can be extruded.
  • an ultraviolet absorber, an anti-aging agent, etc. may be added to the resin material of the coextruded sheet 1.
  • the coextruded sheet 1 includes a core layer 2, a skin layer 3 laminated on one main surface of the core layer 2, and a skin layer 4 laminated on the other main surface of the core layer 2. It has
  • the core layer 2 is made of foamed resin.
  • the core layer 2 can be formed by foam-molding molten polycarbonate resin. That is, the core layer 2 has many air bubbles.
  • a large number of cells have a substantially elliptical shape extending in the extrusion direction in a cross-sectional view taken in the thickness direction in a direction along the extrusion direction during extrusion molding.
  • the bubbles included near the center of the core layer 2 in the thickness direction have a larger bubble diameter than the bubbles 21 included near the ends of the core layer 2 in the thickness direction.
  • the bubble diameter of the large number of bubbles 21 gradually becomes smaller from the center in the thickness direction of the core layer 2 toward the ends in the thickness direction.
  • the skin layer 3 is made of non-foamed resin. That is, the skin layer 3 is not foam-molded.
  • the skin layer 3 is extruded from the die outlet in an unfoamed state by a coextrusion method, and is laminated integrally with the core layer 2.
  • the skin layer 3 has a thickness t1.
  • a thermoplastic resin that can be well bonded to the core layer 2 may be used. More specifically, it is particularly preferable that the resin material of the skin layer 3 is the same resin material as the core layer 2. Further, the skin layer 3 can be made of a reinforced resin containing an inorganic filler in order to strengthen the skin layer 3. With these configurations of the skin layer 3, it is possible to reduce the weight and improve the strength while efficiently improving the strength. Examples of the inorganic filler include glass fiber, carbon fiber, aramid fiber, talc, and mica.
  • the skin layer 4 is the same as the skin layer 3 except that it is laminated on the other main surface of the core layer 2. Therefore, a detailed explanation of the skin layer 4 will be omitted.
  • MVRs The melt volume rate (hereinafter referred to as MVRs) of the polycarbonate resin contained in the skin layer 3 is the same as the melt volume rate (hereinafter referred to as MVRc) of the polycarbonate resin contained in the core layer 2, or is higher than MVRc. It's also expensive. From the viewpoint of shortening takt time to improve production efficiency, suppressing coalescence of bubbles after heat forming such as vacuum forming, and improving mechanical strength, MVRs and MVRc are defined by the following formulas. (1) is satisfied. 1.5 ⁇ MVRs/MVRc ⁇ 8.0 (1)
  • the temperature of the resin forming the skin layer 3 can be lowered as much as possible immediately after being discharged from the die outlet during extrusion molding.
  • the viscosity of the skin layer 3 within the die can be reduced, making it possible to extrude the skin layer 3 at a lower temperature.
  • the core layer 2 can also be cooled by heat conduction through the skin layer 3, thereby suppressing swelling or tearing of the surface of the skin layer 3 caused by foaming of the resin contained in the core layer 2. I can do it.
  • MVRs higher than MVRc
  • the skin layer 3 becomes more easily deformed by heating, and as a result, it becomes easier to draw down during vacuum forming, so the takt time can be shortened.
  • the value of MVRs/MVRc is smaller than 1.5, the effect of lowering the resin temperature during extrusion molding is small, making it difficult to suppress swelling or tearing of the surface of the skin layer 3.
  • the heating temperature during vacuum forming is set to It is necessary to raise the temperature significantly higher than the optimum processing temperature. In this case, the skin layer 3 is excessively deformed, resulting in a decrease in molding efficiency.
  • the heating temperature is lowered, the preheating time during vacuum forming becomes longer and production efficiency decreases. Therefore, consideration must be given to ensuring appropriate fluidity of the resin forming the core layer 2 and skin layer 3 during extrusion molding, and controlling the viscosity to suppress swelling or tearing of the surface of the skin layer 3.
  • the value of MVRs/MVRc is preferably 1.7 or more.
  • the value of MVRs/MVRc is preferably 2.5 or less, most preferably 2.3 or less. That is, by setting the value of MVRs/MVRc to 1.5 or more, preferably 1.7 or more, and 8.0 or less, preferably 2.5 or less, and more preferably 2.3 or less, production during vacuum forming can be improved.
  • viscosity to improve properties ensure appropriate fluidity of the resin forming the core layer 2 and skin layer 3 during extrusion molding, and suppress swelling or tearing of the surface of the skin layer 3. can be controlled. This also applies to the skin layer 4 and the core layer 2.
  • the range of 1.5 to 8.0, particularly 1.7 to 2.3 is the viscosity of the core layer 2 whose viscosity has decreased due to melting of the foaming agent and the viscosity of the non-foamed layer. It can be determined by considering the viscosity ratio of the skin layer 3, the viscosity characteristics of the polycarbonate resin, and the viscosity characteristics of the polycarbonate resin in a state in which the blowing agent is melted.
  • MVRs and MVRc are based on JIS K7210-1:2014 (ISO1133-1:2011) for the resin materials included in skin layer 3, skin layer 4, and core layer 2, using the so-called B method, and measuring temperature 300. Measured under the conditions of °C and a load of 1.2 kg. The deflection temperature under load of each layer is measured by peeling the skin layer 3 and the skin layer 4 from the core layer 2 of the coextruded sheet 1.
  • the method of peeling the skin layer 3 and the skin layer 4 from the core layer 2 is not particularly limited, but for example, the skin layer 3 and the skin layer 4 may be cut out (surfaced) using a contour or the like, or the skin layer 3 and the skin layer 4 may be removed using an NC cutter or the like. Layer 3 and skin layer 4 may be cut out.
  • the coextruded sheet 1 has a thickness T of 1.5 to 6 mm.
  • the skin layer 3 has a thickness t1.
  • the skin layer 4 has a thickness t2.
  • the thickness t1 of the skin layer 3 and the thickness t2 of the skin layer 4 are measured as follows.
  • a cross section of the coextruded sheet 1 cut in the thickness direction along the width direction is observed using a microscope.
  • a KEYENCE model number VHX-60000 is used as a microscope.
  • the magnification of the microscope may be such that the diameter of the bubbles at the interface between the skin layer 3 and the core layer 2 of the coextruded sheet 1 can be confirmed.
  • 15 are the air bubbles close to the surface of the co-extruded sheet 1 on each virtual boundary line when the cross-section of the co-extruded sheet 1 is divided into 16 equal parts in the width direction. Among them, the bubble closest to the surface of the coextruded sheet 1 is confirmed.
  • the boundary between the core layer 2 and the skin layer 4 was similarly defined, and the thickness t1 of the skin layer 3 and the thickness t2 of the skin layer 4 were measured.
  • the thickness t1 of the skin layer 3 and the thickness t2 of the skin layer 4 are each preferably 0.050 mm or more from the viewpoint of making the thickness T of the coextruded sheet 1 as uniform as possible during coextrusion molding.
  • the total thickness of the skin layer which is the sum of the thickness t1 of the skin layer 3 and the thickness t2 of the skin layer 4, is preferably 0.15 to 0.5 with respect to the thickness T of the coextruded sheet 1. That is, the coextruded sheet 1 satisfies the following formula (4). 0.10 ⁇ (t1+t2)/T ⁇ 0.5 (4) If the thickness (t1+t2) of the entire skin layer is less than 0.10 with respect to the thickness T of the coextruded sheet 1, it will be difficult to obtain the mechanical strength reinforcing effect by the non-foamed resin of the skin layer, and the specific flexural modulus etc. mechanical strength decreases.
  • the thickness (t1+t2) of the entire skin layer becomes larger than 0.5 with respect to the thickness T of the coextruded sheet 1, the density of the coextruded sheet 1 increases. As a result, the coextruded sheet 1 loses its lightweight properties due to foaming, and it also takes time for heat conduction, which increases the preheating time during vacuum forming, etc., which can reduce production efficiency.
  • the ratio of the thickness of the entire skin layer (t1+t2) to the thickness T of the coextruded sheet 1 is preferably in the range of 0.15 to 0.45, more preferably in the range of 0.2 to 0.4. It is better.
  • the specific flexural modulus can be improved while reducing the weight by reducing the density.
  • the ratio of the thickness of the entire skin layer (t1+t2) to the thickness T of the coextruded sheet 1 in the range of 0.2 to 0.4 the thickness of the core layer 2 to make the bubble unevenness uniform is ensured. While achieving this, it is possible to improve secondary processability such as vacuum forming.
  • the specific flexural modulus is a value obtained by dividing the flexural modulus of the coextruded sheet 1 by the density of the coextruded sheet 1.
  • the bending elastic modulus is measured by a three-point bending test (according to ISO178 or JIS7171). At this time, the flexural modulus is measured in the atmosphere. The test speed is 10 mm/min.
  • the expansion of the surface that occurs during coextrusion molding can be controlled. It is possible to suppress the deterioration of the appearance design due to extrusion, etc., it is also possible to suppress the swelling and cracking of the surface that occurs during heat forming such as vacuum forming, and it is possible to obtain excellent mechanical strength.
  • the coextruded sheet 1 has an apparent density of 0.4 to 0.8 g/cm 3 .
  • the thickness was measured at 10 points at equal intervals excluding the edges, and the arithmetic mean value of these thicknesses was taken as the average thickness of the coextruded sheet 1.
  • the length of each side of the coextruded sheet 1 in the width direction and extrusion direction is measured using a tape measure, and the volume of the coextruded sheet 1 is calculated from the length of each side and the average thickness. Further, the weight of the coextruded sheet 1 is measured using an electronic balance, and the apparent density of the coextruded sheet 1 is determined by dividing the weight by the volume.
  • the core layer 2 of the present disclosure is preferably foam-molded using a physical foaming agent such as nitrogen or carbon dioxide at a relatively low pressure.
  • a physical foaming agent such as nitrogen or carbon dioxide
  • the pressure of the physical blowing agent can be set at a relatively low level of 1 to 6 MPa, and a large number of fine bubbles can be formed.
  • the average cell diameter of the bubbles is preferably 0.1 mm or more, and 1.0 mm or less, preferably 0.3 mm or less.
  • the coextruded sheet 1 is formed into various shapes by vacuum forming.
  • vacuum forming the coextruded sheet 1 is usually heated to about 200° C. to begin drawdown, and then applied to a mold or the like and vacuum-suctioned to form the sheet. That is, it is preferable that the coextruded sheet 1 has a small amount of deformation (dimensional change rate before and after heating) during heating during vacuum forming.
  • the coextruded sheet 1 has a dimensional change rate of -5% to 0% in the extrusion direction when the coextruded sheet is heated in an atmosphere of 200° C. for 30 minutes. Further, the coextruded sheet 1 has a dimensional change rate of -5 to 0% in the width direction.
  • the coextruded sheet 1 has a dimensional change rate of -5 to 0% in either the extrusion direction or the width direction.
  • the coextruded sheet 1 has a dimensional change rate of -5 to 0% in both the extrusion direction and the width direction.
  • the width direction is a direction perpendicular to the above-mentioned extrusion direction in plan view. Thereby, the coextruded sheet 1 has excellent dimensional stability before and after heating.
  • the dimensional change rate in the extrusion direction can be calculated using the following formula.
  • Dimensional change rate in the extrusion direction (%) ⁇ (distance between gauge lines in the extrusion direction after heating - distance between gauge lines in the extrusion direction before heating) / distance between gauge lines in the extrusion direction before heating ⁇ x 100
  • the dimensional change rate in the width direction can be calculated according to the following formula.
  • Dimensional change rate in the width direction (%) ⁇ (distance between gauge lines in the width direction after heating - distance between gauge lines in the width direction before heating/distance between gauge lines in the width direction before heating) ⁇ x 100
  • the coextruded sheet 1 is heat-shaped into a desired shape mainly by vacuum forming or the like.
  • bulges may occur on the sheet surface, which may deteriorate the appearance and design of the sheet surface. Therefore, it is preferable to suppress the occurrence of bulges in the coextruded sheet 1.
  • FIG. 3 when the coextruded sheet 1 is heated for 30 minutes in a 250°C heating atmosphere, the average thickness t3 of the coextruded sheet 1 after heating is relative to the average thickness t4 of the coextruded sheet before heating. It is 1.5 times or less.
  • S indicated by a broken line is the surface of the coextruded sheet 1 before heating.
  • the coextruded sheet 1 can suppress the generation of bulges due to heating, and can reduce changes in thickness by comparing before and after heating. Thereby, the coextruded sheet 1 can improve its appearance and design during heat forming such as vacuum forming.
  • the thickness t5 of the coextruded sheet including the above-described bulged portion 11 is 1.5 times or less of the average thickness t4 of the coextruded sheet before heating shown in FIG.
  • the coextruded sheet 1 after heating has one or less bulges 11 per 100 cm 2 of its surface. That is, according to the coextruded sheet 1, the height of the bulges 11 generated on the surface due to heating can be reduced, and the number of bulges 11 generated can be suppressed. Thereby, the coextruded sheet 1 can improve its appearance and design during heat forming such as vacuum forming.
  • the coextruded sheet 1 may contain a large number of scaly fillers.
  • the scaly filler is, for example, an inorganic filler such as talc, calcium carbonate, mica, clay, boron nitride, clastonite, potassium titanate, or glass flakes.
  • the scale-like filler may be surface-treated with a silane coupling agent, a titanate coupling agent, a phosphate coupling agent, a fatty acid coupling agent, or the like.
  • the scaly filler has an aspect ratio of 5 or more. The aspect ratio is calculated by dividing the average particle size of the scaly filler by the average thickness (average particle size/average thickness).
  • the aspect ratio of the scaly filler is preferably 10 or more, more preferably 30 or more.
  • the aspect ratio of the scaly filler is preferably less than 50.
  • the specific surface area of the scaly filler is preferably 5 to 20 m 2 /g. If the specific surface area of the scaly filler becomes too small, surface smoothness will be difficult to develop due to the scaly filler sliding on the surface, and if the specific surface area becomes too large, the resistance of the scaly filler in the molten resin will increase. As a result, it becomes difficult to orient the scaly filler appropriately.
  • the core layer 2 may include a scale-like filler oriented substantially parallel to the interface between the core layer 2 and the skin layer 3 in a region near the boundary with the skin layer 3.
  • the neighboring region is a region positioned in the thickness direction of the core layer 2 in a range from the interface between the core layer 2 and the skin layer 3 to a thickness of 5% of the core layer thickness.
  • the bubbles contained in the core layer 2 have a shape extending along the extrusion direction during extrusion molding.
  • the scale-like filler is also oriented substantially parallel to the cell walls of the cells extending in the stretching direction, so that the strength of the cell walls can be improved. As a result, tearing of the coextruded sheet 1 along the extrusion direction can be suppressed.
  • the scale-like filler when the scale-like filler is approximately parallel, it means that the scale-like filler is located at the boundary between the core layer 2 and the skin layer 3 in a cross section of the coextruded sheet 1 cut in the thickness direction in the direction along the extrusion direction during extrusion molding. It means having an inclination of 0° or more and less than 5° with respect to the plane. In other words, it refers to a state in which the surface (principal surface) of the scale-like filler and the boundary surface between the core layer 2 and the skin layer 3 are opposed to each other so as to be substantially parallel to each other. The same applies to the scale-like filler oriented in the core layer 2 near the boundary between the core layer 2 and the skin layer 4.
  • the orientation state of a large number of scale-like fillers included in the region near the boundary between the core layer 2 and the skin layer 3 was calculated as follows. First, in a cross section in the thickness direction along the extrusion direction during extrusion molding, 50 electron micrographs of 150 x 150 ⁇ m were taken at equal intervals from the tip to the rear end in the extrusion direction in the neighboring region, and at the center in the thickness direction of the neighboring region. Take a photo. Among all the scaly fillers included in these 50 electron micrographs, the scaly fillers oriented substantially parallel to the interface between the core layer 2 and the skin layer 3 are confirmed. Thereby, the proportion of the scale-like fillers oriented substantially in parallel among the large number of scale-like fillers included in the neighboring region is calculated.
  • the core layer 2 may include a scale-like filler oriented at an angle of 5° to 90° with respect to the surface of the coextruded sheet 1 in the central region of the core layer 2 in the thickness direction.
  • the central region refers to a region having a thickness of 25% from the center in the thickness direction toward the interface between the core layer 2 and the skin layer 3, assuming that the thickness of the core layer 2 is 100%. It is preferable that 40% or more of the scale-like fillers included in the central region are oriented at an angle of 5° to 90° with respect to the surface S of the coextruded sheet 1. Thereby, the moldability of the coextruded sheet 1 can be improved.
  • the moldability of the coextruded sheet 1 can be further improved.
  • the bubbles contained in the central region of the core layer 2 tend to become larger during extrusion molding compared to the above-mentioned neighboring region. This is because the central region is less likely to be cooled after extrusion than the neighboring regions. If the bubbles become too large, they may cause damage to the coextruded sheet 1.
  • by tilting the scale-like filler in the central region and arranging it randomly between the bubbles it is possible to suppress the growth of the bubbles in all directions.
  • the strength of the coextruded sheet 1 or the strength during molding, that is, the moldability can be improved.
  • a foamed resin molded product is produced by vacuum forming the coextruded sheet 1 as a material, it is possible to suppress the bubbles contained in the coextruded sheet 1 from bursting or the coextruded sheet 1 from being damaged.
  • the orientation state of the large number of scale-like fillers included in the central region of the core layer 2 can be calculated as follows. First, as in the case of the neighboring region, 50 microscopic photographs are taken at equal intervals at the center of the core layer 2 in the thickness direction. Among all the scale-like fillers included in these 50 electron micrographs, scale-like fillers oriented at an angle of 5° to 90° with respect to the surface of the coextruded sheet 1 are confirmed. Accordingly, the proportion of the scale-like fillers that are oriented at an angle of 5° to 90° with respect to the surface of the coextruded sheet 1 among the large number of scale-like fillers included in the central region is calculated.
  • resin pellets as a resin material are charged into the screw cylinder of the main extruder.
  • the resin material is polycarbonate resin.
  • the resin pellets are heated in a screw cylinder to produce molten resin.
  • a blowing agent is injected into the molten resin from a blowing agent injection cylinder attached to the screw cylinder of the main extruder.
  • the blowing agent is dissolved in the molten resin by the above-mentioned screw cylinder and kneaded to be uniformly dispersed. In this way, a mixed molten resin is produced.
  • the mixed molten resin is discharged from the die outlet to form the core layer 2 .
  • resin pellets serving as a resin material are placed in each of the screw cylinders of the two sub-extruders, and are heated and melted to produce two molten resins.
  • One of the two molten resins is discharged from the die outlet to form the skin layer 3, and the other is discharged from the die outlet to form the skin layer 4.
  • the mixed molten resin and the two molten resins are combined in a die from each extruder, and a skin layer 3 is laminated on one of the main surfaces of the core layer 2, and a skin layer 4 is laminated on the other main surface of the core layer 2. are discharged from the die outlet so that they are stacked.
  • the pressure in the die manifold is preferably higher than the pressure of the blowing agent to be injected, and more preferably maintained at 10 MPa or higher.
  • the adhesion between the core layer 2 and the skin layer 3 and between the core layer 2 and the skin layer 4 can be improved, and bubble breakage in the core layer 2 can be suppressed.
  • the vacuum formability of the coextruded sheet 1 can be improved.
  • the foaming method is a physical foaming method using an inert gas such as nitrogen and carbon dioxide gas as a foaming agent.
  • the coextruded sheet 1 thus extruded is conveyed to a cutting machine by a take-up machine.
  • the cutting machine cuts the coextruded sheet 1 into a desired shape.
  • the coextruded sheet 1 produced in this way can be used in the following applications by shaping it into a desired shape by vacuum forming or the like.
  • products and parts that require relatively high strength such as signboards or mobility materials such as automobile exterior materials, products and parts that require heat resistance such as batteries or trays for heat generating parts used in manufacturing processes that involve heating processes.
  • products and parts that require weight reduction The coextrusion sheet 1 contains a polycarbonate resin and is foam-molded by a coextrusion method, so that it is suitable as a material for molding resin molded articles such as these products and parts.
  • the coextruded sheet 1 can contribute to improving resource utilization efficiency, reducing transportation burden, reducing energy consumption, and reducing CO 2 emissions.
  • Goal 7 Affordable and Clean Energy
  • Goal 9 Industry and Technology
  • SDGs 17 Sustainable Development Goals
  • test pieces of Examples 1 to 6 and Comparative Examples 1 to 4 were prepared, and the dimensional change rate, appearance of the test pieces (mechanical strength after vacuum forming), and minimum preheating time during vacuum forming were determined.
  • the resin material used for these test pieces is polycarbonate resin.
  • T indicates the thickness of the test piece.
  • the present disclosure is not limited to these examples.
  • Example 1 The test piece of Example 1 was produced as follows using a coextrusion molding method. First, polycarbonate resin was charged into the screw cylinder of the main extruder, and was shear-kneaded while heating at 270°C. Then, the blowing agent N2 was injected under a pressure of 4 MPa. A core layer was obtained by heating and melting the polycarbonate resin and the blowing agent at 215°C, and setting the temperature at the exit of the die to 215°C. At the same time, polycarbonate resin was charged into the screw cylinder of the sub-extruder, and was shear kneaded while heating at 255°C, and the exit temperature of the die was set at 215°C to obtain two skin layers.
  • Example 1 a test piece of Example 1 was obtained in which skin layers made of non-foamed resin were laminated on both main surfaces of the core layer made of foamed resin.
  • the exit gap of the die was set so that the thickness T of the test piece of Example 1 had the value shown in Table 1, and the test piece of Example 1 was coextruded at a drawing speed of 0.7 m/min.
  • Examples 2 to 13 and Comparative Examples 1 to 3, 5 The test pieces of Examples 2 to 13 and Comparative Examples 1 to 3 and 5 were all produced in the same manner as in Example 1. However, the test pieces of Examples 2 to 6 and Comparative Examples 1 to 3 were manufactured to have different thicknesses from Example 1 by changing the outlet gap of the die during extrusion molding and adjusting the drawing speed as appropriate. In addition, the test pieces of Examples 7 to 9 were made to have the same thickness as the test piece of Example 5 by changing the combination of various polycarbonate resins used for the skin layer and core layer so that the MVR ratio was different. did. The test pieces of Examples 10 to 13 were made using the same polycarbonate resin as the resin material used for the test piece of Example 5, and were made so that the thickness T and the thickness of the skin layer were different from those of the test piece of Example 2. did.
  • Comparative example 4 The test piece of Comparative Example 4 was produced as follows using a coextrusion molding method. First, polycarbonate resin was charged into the screw cylinder of the main extruder, and was shear-kneaded while heating at 270°C. Thereafter, isobutane as a foaming agent was injected so that the content was 0.7 wt%/kg resin. A core layer was obtained by heating and melting the polycarbonate resin and the blowing agent at 215°C, and setting the temperature at the exit of the die to 215°C.
  • the dimensional change rate shown in Table 1 was calculated as follows. First, a sample piece with dimensions of 120 mm x 120 mm was obtained from a sheet-like test piece. At this time, sample pieces were taken from the center and both ends of the entire width of the test piece. The center part is a part located at 1/2 of the length of the full width of the test piece, and both end parts are parts 50 mm apart from the extreme end of the full width of the test piece. Marks were placed on each sample piece in the extrusion direction and width direction, and furthermore, a mark was placed in the center of each sample piece for measuring the distance between gauge lines in the extrusion direction and width direction.
  • the distance between the gauge lines in the extrusion direction and the width direction was measured using a scale ruler or metal ruler capable of measuring the distance to a minimum of 0.5 mm. Thereafter, the metal container whose inner bottom was covered with a Teflon (registered trademark) sheet was placed in a dryer, and the temperature of the dryer was adjusted so that the temperature of the metal container was 200 ⁇ 2°C. The sample piece was placed in a metal container and heated for 30 minutes. After the heat treatment was completed, the sample piece was taken out from the metal container and cooled to room temperature, and then the distance between the gauge lines in the extrusion direction and width direction was measured. Then, the dimensional change rate was calculated using the above-mentioned formula.
  • the absolute value of the dimensional change rate in the extrusion direction was larger than the dimensional change rate in the width direction, so Table 1 shows the dimensional change rate in the extrusion direction. That is, the dimensional change rate in the width direction is smaller than the dimensional change rate in the extrusion direction. Therefore, the dimension in the width direction was more stable than in the extrusion direction before and after heating.
  • the MVR ratio shown in Table 1 is a value calculated by MVRs/MVRc, and MVRs and MVRc were measured by the above-mentioned measurement method.
  • the corners of the recess 101 are rounded with a radius of curvature of 15 mm, the distance between the opposing short sides of the substantially rectangular shape is 200 mm, the distance between the opposing long sides is 80 mm, and the depth of the recess 101 is was 35 mm.
  • Each test piece was vacuum formed using this vacuum forming mold 100.
  • the molded product was cut in the depth direction along a diagonal line of a rectangle consisting of an extension line of a short side and an extension line of a long side. The diameter of the bubbles on the cut surface was confirmed.
  • the heater optimum temperature refers to the dimensional accuracy of each test piece and the molded product after vacuum forming, specifically, the dimensional accuracy of each short side and long side of the molded product excluding corners with curved surfaces. This is the maximum temperature at which the dimensional accuracy is ⁇ 2 mm and the test piece does not swell or tear.
  • the minimum preheating time is the minimum heating time during vacuum forming under optimal heater temperature conditions.
  • "CFS-65P model” manufactured by Wakisaka Engineering Co., Ltd. was used as the vacuum forming apparatus.
  • Example 4 The MVR ratios of Examples 1 to 13 were 1.5 to 8.0. In Examples 1 to 13, the appearance and mechanical strength (merging of bubbles) were "A", and it was confirmed that the minimum preheating time was shortened, that is, the takt time was shortened. The reason why the minimum preheating time in Example 4 is relatively long is considered to be because the thickness of the test piece is relatively large compared to other Examples. Therefore, it is considered that Example 4 had the same minimum preheating time as Example 3 if the thickness was the same as Example 3. Further, when comparing Examples 1 to 9, it was found that the takt time could be further shortened, especially when the MVR ratio was 1.5 to 2.5, and even 2.3 or less.
  • Example 3 when comparing Example 3 with Examples 7 to 9, in Examples 7 and 9, even though the results were rated "A", blistering, etc., occurring on the surface of the vacuum-formed product was suppressed. That is, by setting the MVR ratio to 1.7 to 2.3, it was possible to obtain a vacuum-formed product with better surface smoothness. Further, when comparing Examples 10 to 13, in Example 12, the minimum preheating time was relatively long because the ratio of the thickness of the skin layer to the thickness of the test piece was large. It is thought that because the skin layer became thicker, it took longer for heat to be conducted to the core layer. Although not shown in Table 1, Example 10 showed a decrease in flexural modulus compared to Examples 11 to 13.
  • Example 10 the flexural modulus decreased because the skin layer was thin. Furthermore, in Examples 1 to 13, it was confirmed that the dimensional change rate was further reduced by setting the MVR ratio to 1.5 to 8.0.
  • Comparative Example 1 the evaluation of appearance and mechanical strength was "A”, but the minimum preheating time was relatively long. This is considered to be because the MVR ratio of Comparative Example 1 was relatively large at 8.57, and the minimum preheating time was long, so coalescence of bubbles was suppressed.

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PCT/JP2023/007276 2022-03-31 2023-02-28 共押出シート及び樹脂成形品 Ceased WO2023189108A1 (ja)

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