JP7658196B2 - Fiber-reinforced thermoplastic resin laminate and method for producing same - Google Patents
Fiber-reinforced thermoplastic resin laminate and method for producing same Download PDFInfo
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Description
本発明は、繊維強化熱可塑性樹脂積層成形体及びその製造方法に関する。 The present invention relates to a fiber-reinforced thermoplastic resin laminate and its manufacturing method.
熱可塑性樹脂と炭素繊維等の強化繊維とを複合化した繊維強化熱可塑性樹脂からなる成形体は、軽量かつ高い力学特性を有しており、自動車や建材等、様々な分野で使用されている。このような繊維強化熱可塑性樹脂からなる成形体は、繊維強化熱可塑性樹脂が成形加工性に優れているため、射出成形により製造されることが多い。 Molded articles made of fiber-reinforced thermoplastic resin, which is a composite of thermoplastic resin and reinforcing fibers such as carbon fiber, are lightweight and have high mechanical properties, and are used in a variety of fields, including automobiles and building materials. Molded articles made of such fiber-reinforced thermoplastic resin are often manufactured by injection molding, since fiber-reinforced thermoplastic resin has excellent moldability.
例えば、特開2013-133378号公報(特許文献1)には、質量平均繊維長が1~10mmの炭素繊維を10~70質量%含む炭素繊維強化熱可塑性樹脂であって、熱可塑性樹脂中で炭素繊維が2次元ランダム配向しており、長さが3mm~30mm、幅が1mm~10mm、厚みが0.5mm~10mmの炭素繊維強化熱可塑性樹脂を射出成形することによって得られる、質量平均繊維長が0.4~10mmの炭素繊維を含む成形品が記載されている。しかしながら、この成形品においては、炭素繊維がランダムに分散しているため、大きな衝撃が加わるような用途においては、力学特性(特に、曲げ特性)が必ずしも十分なものではなかった。 For example, JP 2013-133378 A (Patent Document 1) describes a molded article containing carbon fibers with a mass average fiber length of 0.4 to 10 mm, which is obtained by injection molding a carbon fiber reinforced thermoplastic resin containing 10 to 70 mass% of carbon fibers with a mass average fiber length of 1 to 10 mm, in which the carbon fibers are two-dimensionally randomly oriented in the thermoplastic resin and have a length of 3 mm to 30 mm, a width of 1 mm to 10 mm, and a thickness of 0.5 mm to 10 mm. However, because the carbon fibers in this molded article are randomly dispersed, the mechanical properties (especially bending properties) are not necessarily sufficient in applications where a large impact is applied.
一方、特開2016-98271号公報(特許文献2)には、数平均繊維長が1μm以上5mm以下であり、数平均繊維径が5nm以上30μm以下である不連続繊維及び熱可塑性樹脂を含む組成物を、塑性域において、ストロークに対する圧力の勾配が0Pa/mm以上1.0Pa/mm以下の条件で押出成形することによって得られる、不連続繊維が熱可塑性樹脂中に十分に配向しているプリプレグが記載されている。しかしながら、このプリプレグにおいては、不連続繊維が、その表面付近では一方向に配向しているものの、中心部ではランダムに分散しているため、大きな衝撃が加わるような用途においては、力学特性(特に、曲げ特性)が必ずしも十分なものではなかった。 On the other hand, JP 2016-98271 A (Patent Document 2) describes a prepreg in which the discontinuous fibers are sufficiently oriented in the thermoplastic resin, the prepreg being obtained by extrusion molding a composition containing discontinuous fibers having a number average fiber length of 1 μm to 5 mm and a number average fiber diameter of 5 nm to 30 μm and a thermoplastic resin under conditions in which the pressure gradient with respect to the stroke is 0 Pa/mm to 1.0 Pa/mm in the plastic region. However, in this prepreg, the discontinuous fibers are oriented in one direction near the surface, but are randomly dispersed in the center, so that the mechanical properties (particularly the bending properties) are not necessarily sufficient in applications where a large impact is applied.
また、特開2000-108236号公報(特許文献3)には、強化繊維で補強した繊維強化熱可塑性樹脂層と熱可塑性樹脂層を交互に積層し、加圧プレス成形することによって得られる、強化繊維が配向している繊維強化熱可塑性樹脂積層板が記載されている。さらに、特開2016-180037号公報(特許文献4)には、一方向に配向した平均繊維長が5~50mmの炭素繊維及び熱可塑性樹脂を含む層と、一方向に配向した連続した炭素繊維及び熱可塑性樹脂を含む層とを有する炭素繊維強化熱可塑性樹脂複合材料を熱成形することによって得られる成形体が記載されている。しかしながら、これらの積層板や成形体においては、極めて薄い層を多量に積層して熱成形するため、面内全体にわたって均一に熱及び圧力を付与しても、各層でのたわみや高低差が生じることにより、繊維の向きにばらつきが生じやすく、特に、積層板や成形体の中心部における繊維の配向度は十分に高いものではなかった。このため、大きな衝撃が加わるような用途においては、力学特性(特に、曲げ特性)が必ずしも十分なものではなかった。また、これらの積層板や成形体は、射出成形により製造した積層体に比べて、コスト、賦形性、再加工性、多量生産(短時間での成形サイクル)、複雑な形状への適応性等に劣るものであった。さらに、厚さが2mmを超える積層板や成形体を製造するには、極めて多くの層を積層して熱成形する必要があるため、製造工程が複雑化するだけでなく、均一なプレス成形を行っても、繊維を均質に配向することが一層困難となる傾向にあった。 In addition, Japanese Patent Application Laid-Open No. 2000-108236 (Patent Document 3) describes a fiber-reinforced thermoplastic resin laminate in which reinforcing fibers are oriented, which is obtained by alternately laminating fiber-reinforced thermoplastic resin layers and thermoplastic resin layers reinforced with reinforcing fibers and press-molding them under pressure. Furthermore, Japanese Patent Application Laid-Open No. 2016-180037 (Patent Document 4) describes a molded body obtained by thermoforming a carbon fiber-reinforced thermoplastic resin composite material having a layer containing carbon fibers and thermoplastic resin with an average fiber length of 5 to 50 mm oriented in one direction and a layer containing continuous carbon fibers and thermoplastic resin oriented in one direction. However, in these laminates and molded bodies, since a large number of extremely thin layers are laminated and thermoformed, even if heat and pressure are applied uniformly over the entire surface, deflection and height differences occur in each layer, which tends to cause variations in the fiber orientation, and in particular, the degree of fiber orientation in the center of the laminates and molded bodies was not sufficiently high. For this reason, in applications where a large impact is applied, the mechanical properties (especially bending properties) were not necessarily sufficient. Furthermore, compared to laminates manufactured by injection molding, these laminates and molded bodies were inferior in terms of cost, formability, reworkability, mass production (short molding cycle), adaptability to complex shapes, etc. Furthermore, to manufacture laminates and molded bodies with a thickness of more than 2 mm, it is necessary to stack and thermoform an extremely large number of layers, which not only complicates the manufacturing process but also tends to make it more difficult to uniformly orient the fibers, even when uniform press molding is performed.
本発明は、上記従来技術の有する課題に鑑みてなされたものであり、力学特性(特に、曲げ弾性率及び曲げ強度)に優れた繊維強化熱可塑性樹脂からなる成形体及びその製造方法を提供することを目的とする。 The present invention was made in consideration of the problems with the above-mentioned conventional technology, and aims to provide a molded body made of a fiber-reinforced thermoplastic resin that has excellent mechanical properties (particularly, flexural modulus and flexural strength) and a method for manufacturing the same.
本発明者らは、上記目的を達成すべく鋭意研究を重ねた結果、熱可塑性樹脂と強化繊維とを複合化した繊維強化熱可塑性樹脂を射出成形した場合、厚さが2mm以下の射出成形体においては、高い力学特性(特に、曲げ弾性率及び曲げ強度)が得られるのに対して、厚さが2mmを超える単層の射出成形体においては、力学特性(特に、曲げ弾性率及び曲げ強度)が低下することを見出した。さらに、本発明者らは、厚さが2mm以下の射出成形体を重ね合わせたり、接着剤を用いて接着したりしても、得られる積層成形体においては、力学特性(特に、曲げ弾性率及び曲げ強度)が向上しないことも見出した。 As a result of intensive research conducted by the inventors to achieve the above object, they discovered that when a fiber-reinforced thermoplastic resin, which is a composite of a thermoplastic resin and reinforcing fibers, is injection molded, an injection molded body having a thickness of 2 mm or less has high mechanical properties (particularly, flexural modulus and flexural strength), whereas a single-layer injection molded body having a thickness of more than 2 mm has reduced mechanical properties (particularly, flexural modulus and flexural strength). Furthermore, the inventors discovered that even if injection molded bodies having a thickness of 2 mm or less are stacked or bonded with an adhesive, the mechanical properties (particularly, flexural modulus and flexural strength) of the resulting laminated molded body are not improved.
そこで、本発明者らは、更に鋭意研究を重ねた結果、熱可塑性樹脂と強化繊維とを複合化した繊維強化熱可塑性樹脂からなる、厚さが2mm以下の射出成形体の上に、繊維強化熱可塑性樹脂を射出成形して、厚さが2mm以下の射出成形体を積層することによって、力学特性(特に、曲げ弾性率及び曲げ強度)に優れた積層成形体が得られることを見出し、本発明を完成するに至った。 As a result of further intensive research, the inventors discovered that a laminated molded product with excellent mechanical properties (particularly flexural modulus and flexural strength) can be obtained by injection molding a fiber-reinforced thermoplastic resin on top of an injection molded product with a thickness of 2 mm or less, which is made of a fiber-reinforced thermoplastic resin that is a composite of a thermoplastic resin and reinforcing fibers, and laminating the injection molded product with a thickness of 2 mm or less, thereby completing the present invention.
すなわち、本発明の繊維強化熱可塑性樹脂積層成形体は、ポリアミドと数平均繊維長が0.05~20mmの繊維とを含有し、前記繊維の含有率が1~70質量%であり、厚さが0.5~2mmである射出成形体からなる層が2層以上積層された積層成形体であり、前記積層成形体が、下層の前記射出成形体の表面上に上層の前記射出成形体を射出成形又は射出プレス成形により形成したものであり、前記積層成形体全体について、前記積層成形体の面方向に平行な方向への前記繊維の配向度が0.75以上であり、各層の表面の少なくとも一部が互いに直接融着していることを特徴とするものである。 That is, the fiber-reinforced thermoplastic resin laminated molded body of the present invention contains polyamide and fibers having a number average fiber length of 0.05 to 20 mm, and the fiber content is 1 to 70 mass%. It is a laminated molded body in which two or more layers consisting of injection molded bodies having a thickness of 0.5 to 2 mm are laminated, and the laminated molded body is formed by injection molding or injection press molding of the upper injection molded body on the surface of the lower injection molded body, and the orientation degree of the fibers in the direction parallel to the surface direction of the laminated molded body is 0.75 or more for the entire laminated molded body, and at least a part of the surface of each layer is directly fused to each other.
本発明の繊維強化熱可塑性樹脂積層成形体においては、前記積層成形体全体の厚さが2.0mm以上であることが好ましい。また、各層において、隣接する層と直接融着している層表面の割合が10%以上であることが好ましい。さらに、前記繊維が炭素繊維であることが好ましい。 In the fiber-reinforced thermoplastic resin laminate of the present invention, it is preferable that the thickness of the entire laminate is 2.0 mm or more. It is also preferable that the ratio of the surface of each layer that is directly fused to the adjacent layer is 10% or more. Furthermore, it is preferable that the fibers are carbon fibers.
また、本発明の繊維強化熱可塑性樹脂積層成形体の製造方法は、熱可塑性樹脂と数平均繊維長が0.05~20mmの繊維とを含有し、前記繊維の含有率が1~70質量%であり、厚さが0.5~2mmである下層の成形体を射出成形又は射出プレス成形した後、前記下層の成形体の表面上に、前記熱可塑性樹脂と前記繊維とを含有し、前記繊維の含有率が1~70質量%であり、厚さが0.5~2mmである上層の成形体を射出成形又は射出プレス成形することにより、前記成形体からなる層同士が、その層表面の少なくとも一部において、互いに直接融着している積層成形体を得ることを特徴とする方法である。 The method for producing a fiber-reinforced thermoplastic resin laminated molded body of the present invention is characterized in that a lower layer molded body containing a thermoplastic resin and fibers with a number average fiber length of 0.05 to 20 mm, the fiber content being 1 to 70 mass%, and the thickness being 0.5 to 2 mm is injection molded or injection press molded, and then an upper layer molded body containing the thermoplastic resin and the fibers, the fiber content being 1 to 70 mass%, and the thickness being 0.5 to 2 mm is injection molded or injection press molded on the surface of the lower layer molded body, thereby obtaining a laminated molded body in which the layers made of the molded bodies are directly fused to each other at least in part of the layer surface.
本発明の繊維強化熱可塑性樹脂積層成形体の製造方法においては、前記下層の成形体を、表面温度が30~280℃となるように加熱しながら、前記上層の成形体を射出成形又は射出プレス成形することが好ましく、前記下層の成形体を、表面温度が前記熱可塑性樹脂のガラス転移温度(Tg)より5~100℃高い温度(Tg+5℃~Tg+100℃)となるように予熱した後、前記上層の成形体を射出成形又は射出プレス成形することがより好ましい。 In the manufacturing method of the fiber-reinforced thermoplastic resin laminate of the present invention, it is preferable to heat the lower layer molded body so that the surface temperature is 30 to 280°C while injection molding or injection press molding the upper layer molded body, and it is more preferable to preheat the lower layer molded body so that the surface temperature is 5 to 100°C higher than the glass transition temperature (Tg) of the thermoplastic resin (Tg + 5°C to Tg + 100°C), and then injection molding or injection press molding the upper layer molded body.
なお、本発明によって、力学特性(特に、曲げ弾性率及び曲げ強度)に優れた繊維強化熱可塑性樹脂積層成形体が得られる理由は必ずしも定かではないが、本発明者らは以下のように推察する。すなわち、本発明の繊維強化熱可塑性樹脂積層成形体は、繊維強化熱可塑性樹脂からなる、厚さが2mm以下の射出成形体の上に、繊維強化熱可塑性樹脂を射出成形して、厚さが2mm以下の射出成形体を積層することによって得られるものである。繊維強化熱可塑性樹脂を厚さが2mm以下となるように射出成形した場合、繊維強化熱可塑性樹脂の流路が狭いため、繊維が一定の方向に揃いやすく、得られる射出成形体においては、図1に示すように、表面から中心部までの全体にわたって、熱可塑性樹脂1中で繊維2が成形体の面方向に平行な方向に高度に配向し、高い力学特性(特に、曲げ弾性率及び曲げ強度)が得られると推察される。そして、本発明の繊維強化熱可塑性樹脂積層成形体においては、このような射出成形体を射出成形により積層しているため、射出成形体からなる各層が、その表面の少なくとも一部において直接融着しているため、積層成形体全体として、高い力学特性(特に、曲げ弾性率及び曲げ強度)が得られると推察される。 Although the reason why the present invention provides a fiber-reinforced thermoplastic resin laminate having excellent mechanical properties (particularly, flexural modulus and flexural strength) is not entirely clear, the present inventors speculate as follows. That is, the fiber-reinforced thermoplastic resin laminate of the present invention is obtained by injection molding a fiber-reinforced thermoplastic resin on an injection molded body having a thickness of 2 mm or less made of a fiber-reinforced thermoplastic resin, and laminating the injection molded body having a thickness of 2 mm or less. When the fiber-reinforced thermoplastic resin is injection molded to a thickness of 2 mm or less, the flow path of the fiber-reinforced thermoplastic resin is narrow, so that the fibers tend to be aligned in a certain direction. In the obtained injection molded body, as shown in FIG. 1, the fibers 2 in the thermoplastic resin 1 are highly oriented in a direction parallel to the surface direction of the molded body throughout the entire body from the surface to the center, and it is speculated that high mechanical properties (particularly, flexural modulus and flexural strength) are obtained. In the fiber-reinforced thermoplastic resin laminate of the present invention, such injection molded bodies are laminated by injection molding, and each layer made of the injection molded body is directly fused to at least a portion of its surface. It is therefore presumed that the laminated body as a whole has high mechanical properties (especially flexural modulus and flexural strength).
一方、繊維強化熱可塑性樹脂を射出成形して作製した、厚さが2mmを超える単層の成形体においては、繊維強化熱可塑性樹脂の流路が広いため、繊維の向きにばらつきが生じ、図2に示すように、熱可塑性樹脂1中で、繊維2は、成形体の表面付近においては成形体の面方向に平行な方向に配向しているものの、中心部においてはランダムに配向し、力学特性(特に、曲げ弾性率及び曲げ強度)が低下すると推察される。 On the other hand, in a single-layer molded body having a thickness of more than 2 mm produced by injection molding a fiber-reinforced thermoplastic resin, the flow path of the fiber-reinforced thermoplastic resin is wide, so that the orientation of the fibers varies. As shown in Figure 2, in the thermoplastic resin 1, the fibers 2 are oriented in a direction parallel to the surface direction of the molded body near the surface of the molded body, but are randomly oriented in the center, which is presumably responsible for the deterioration of the mechanical properties (especially the flexural modulus and flexural strength).
また、繊維強化熱可塑性樹脂からなる、厚さが2mm以下の射出成形体を重ね合わせた場合には、射出成形体からなる各層が直接融着していないため、各層があたかも独立した成形体として振る舞い、力学特性(特に、曲げ弾性率及び曲げ強度)が向上しないと推察される。 In addition, when injection molded bodies made of fiber-reinforced thermoplastic resin and having a thickness of 2 mm or less are stacked on top of each other, the layers of the injection molded bodies are not directly fused together, so it is believed that each layer behaves as if it were an independent molded body, and the mechanical properties (especially the flexural modulus and flexural strength) do not improve.
さらに、繊維強化熱可塑性樹脂からなる、厚さが2mm以下の射出成形体を接着剤を用いて接着した場合においては、射出成形体からなる層と接着剤層との間に界面が生じるため、力学特性(特に、曲げ弾性率及び曲げ強度)が向上しないと推察される。 Furthermore, when an injection molded body made of fiber-reinforced thermoplastic resin and having a thickness of 2 mm or less is bonded using an adhesive, an interface is generated between the layer made of the injection molded body and the adhesive layer, and it is presumed that the mechanical properties (particularly the flexural modulus and flexural strength) do not improve.
本発明によれば、力学特性(特に、曲げ弾性率及び曲げ強度)に優れた繊維強化熱可塑性樹脂からなる成形体を得ることが可能となる。 The present invention makes it possible to obtain molded articles made of fiber-reinforced thermoplastic resins that have excellent mechanical properties (particularly flexural modulus and flexural strength).
以下、本発明をその好適な実施形態に即して詳細に説明する。 The present invention will be described in detail below with reference to preferred embodiments.
〔繊維強化熱可塑性樹脂積層成形体〕
先ず、本発明の繊維強化熱可塑性樹脂積層成形体について説明する。本発明の繊維強化熱可塑性樹脂積層成形体(以下、単に「積層成形体」ともいう)は、熱可塑性樹脂と平均繊維長が0.05~20mmの繊維とを含有し、前記繊維の含有率が1~70質量%であり、厚さが0.5~2mmである射出成形体からなる層が2層以上積層された積層成形体であり、前記積層成形体全体について、前記積層成形体の面方向に平行な方向への前記繊維の配向度が0.75以上であり、各層の表面の少なくとも一部が互いに直接融着したものである。
[Fiber-reinforced thermoplastic resin laminate]
First, the fiber-reinforced thermoplastic resin laminated molded body of the present invention will be described. The fiber-reinforced thermoplastic resin laminated molded body of the present invention (hereinafter also simply referred to as "laminated molded body") contains a thermoplastic resin and fibers having an average fiber length of 0.05 to 20 mm, and the fiber content is 1 to 70 mass%. It is a laminated molded body in which two or more layers made of injection molded bodies having a thickness of 0.5 to 2 mm are laminated, and the orientation degree of the fibers in the direction parallel to the surface direction of the laminated molded body is 0.75 or more for the entire laminated molded body, and at least a part of the surface of each layer is directly fused to each other.
本発明に用いられる熱可塑性樹脂としては特に制限はなく、例えば、ポリアミド、ポリ塩化ビニル、ポリ塩化ビニリデン、ポリ酢酸ビニル、ポリビニルアルコール、ポリスチレン、スチレン-ブタジエン系樹脂、アクリロニトリル-スチレン系樹脂、アクリロニトリル-ブタジエン-スチレン系樹脂、アクリル系樹脂、メタクリル系樹脂、ポリエチレン、ポリプロピレン等のポリオレフィン、ポリアセタール、ポリカーボネート、ポリエチレンテレフタレート、ポリブチレンテレフタレート等のポリエステル、ポリアリレート、ポリフェニレンエーテル、ポリフェニレンスルフィド、ポリスルホン、ポリエーテルスルホン、ポリエーテルエーテルケトン、ポリ乳酸等が挙げられる。これらの熱可塑性樹脂は1種を単独で使用しても2種以上を併用してもよい。また、これらの熱可塑性樹脂の中でも、ポリアミド、ポリプロピレンが好ましい。 The thermoplastic resin used in the present invention is not particularly limited, and examples thereof include polyamide, polyvinyl chloride, polyvinylidene chloride, polyvinyl acetate, polyvinyl alcohol, polystyrene, styrene-butadiene resin, acrylonitrile-styrene resin, acrylonitrile-butadiene-styrene resin, acrylic resin, methacrylic resin, polyolefin such as polyethylene and polypropylene, polyester such as polyacetal, polycarbonate, polyethylene terephthalate and polybutylene terephthalate, polyarylate, polyphenylene ether, polyphenylene sulfide, polysulfone, polyether sulfone, polyether ether ketone, polylactic acid, etc. These thermoplastic resins may be used alone or in combination of two or more. Among these thermoplastic resins, polyamide and polypropylene are preferable.
本発明に用いられる繊維としては、繊維強化熱可塑性樹脂に用いられる強化繊維であれば特に制限はなく、例えば、炭素繊維、ガラス繊維、アルミナ繊維、炭化ケイ素繊維、窒化ホウ素繊維、金属繊維等の無機繊維、パルプ、リグニン、ヘミセルロース、セルロース、セルロースナノファイバー等の天然繊維、アラミド繊維、ビニロン繊維等の有機繊維等が挙げられる。これらの繊維は1種を単独で使用しても2種以上を併用してもよく、また、リサイクル繊維やリユース繊維を用いることもできる。これらの繊維の中でも、炭素繊維、ガラス繊維、パルプ、セルロースナノファイバーが好ましい。 The fibers used in the present invention are not particularly limited as long as they are reinforcing fibers used in fiber-reinforced thermoplastic resins, and examples thereof include inorganic fibers such as carbon fiber, glass fiber, alumina fiber, silicon carbide fiber, boron nitride fiber, and metal fiber; natural fibers such as pulp, lignin, hemicellulose, cellulose, and cellulose nanofiber; and organic fibers such as aramid fiber and vinylon fiber. These fibers may be used alone or in combination of two or more types. Recycled fibers and reused fibers may also be used. Among these fibers, carbon fiber, glass fiber, pulp, and cellulose nanofiber are preferred.
本発明に用いられる繊維の数平均繊維長は、0.05~20mmであることが必要であり、0.10~20mmであることが好ましく、0.15~15mmであることがより好ましく、0.20~10mmであることが更に好ましく、0.25~5mmであることが特に好ましく、0.3~4mmであることが最も好ましい。繊維の数平均繊維長が前記下限未満になると、アスペクト比が減少して繊維の配向がランダム配向となり、得られる積層成形体において、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にあり、他方、前記上限を超えると、繊維の凝集や湾曲配向による力学特性のばらつきが増大し、得られる積層成形体において、力学特性に対する信頼性が低下する傾向にある。 The number average fiber length of the fibers used in the present invention must be 0.05 to 20 mm, preferably 0.10 to 20 mm, more preferably 0.15 to 15 mm, even more preferably 0.20 to 10 mm, particularly preferably 0.25 to 5 mm, and most preferably 0.3 to 4 mm. If the number average fiber length of the fibers is less than the lower limit, the aspect ratio decreases and the fibers are randomly oriented, and the mechanical properties (particularly the flexural modulus and flexural strength) of the resulting laminated molded product tend not to be sufficiently improved. On the other hand, if the number average fiber length exceeds the upper limit, the variation in mechanical properties due to fiber aggregation and curved orientation increases, and the reliability of the mechanical properties of the resulting laminated molded product tends to decrease.
本発明の積層成形体の各層を構成する射出成形体は、このような熱可塑性樹脂と繊維とを含有するものである。このような射出成形体において、繊維の含有率は、1~70質量%であることが必要であり、2~65質量%であることが好ましく、3~60質量%であることがより好ましく、5~50質量%であることが更に好ましい。繊維の含有率が前記下限未満になると、得られる積層成形体において、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にある。他方、繊維の含有率が前記上限を超える射出成形体は、粘度上昇により繊維強化熱可塑性樹脂の流動性が低下し、射出成形性が低下する場合がある。 The injection molded body constituting each layer of the laminate molded body of the present invention contains such a thermoplastic resin and fiber. In such an injection molded body, the fiber content must be 1 to 70 mass%, preferably 2 to 65 mass%, more preferably 3 to 60 mass%, and even more preferably 5 to 50 mass%. If the fiber content is below the lower limit, the mechanical properties (particularly the flexural modulus and flexural strength) of the obtained laminate molded body tend not to be sufficiently improved. On the other hand, an injection molded body with a fiber content exceeding the upper limit may have a decreased flowability of the fiber-reinforced thermoplastic resin due to an increase in viscosity, which may decrease the injection moldability.
また、前記射出成形体の厚さは、0.5~2mmであることが必要であり、0.6~1.9mmであることが好ましく、0.7~1.8mmであることがより好ましく、0.8~1.7mmであることが更に好ましい。厚さが前記下限未満の射出成形体は、冷却固化により繊維強化熱可塑性樹脂の流動性が低下し、射出成形性が低下する場合がある。他方、射出成形体の厚さが前記上限を超えると、得られる積層成形体において、繊維の配向度が低下するため、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にある。 The thickness of the injection molded body must be 0.5 to 2 mm, preferably 0.6 to 1.9 mm, more preferably 0.7 to 1.8 mm, and even more preferably 0.8 to 1.7 mm. Injection molded bodies with a thickness less than the lower limit may experience a decrease in the fluidity of the fiber-reinforced thermoplastic resin upon cooling and solidification, resulting in a decrease in injection moldability. On the other hand, if the thickness of the injection molded body exceeds the upper limit, the degree of fiber orientation in the resulting laminated molded body decreases, and the mechanical properties (particularly the flexural modulus and flexural strength) tend not to be sufficiently improved.
本発明の積層成形体において、前記射出成形体からなる層の数は、2層以上であれば特に制限はなく、3層以上であってもよいが、生産性(総成形時間の短縮)の観点から、2層であることが好ましい。 In the laminated molded product of the present invention, the number of layers made of the injection molded product is not particularly limited as long as it is two or more layers, and may be three or more layers, but from the viewpoint of productivity (shortening the total molding time), it is preferable that it is two layers.
また、本発明の積層成形体の全体の厚さとしては特に制限はないが、1.1mm以上が好ましく、1.2mm以上がより好ましく、1.5mm以上が更に好ましく、2.0mm以上がまた更に好ましく、2.5mm以上が特に好ましく、3.0mm以上が最も好ましい。特に、成形体全体の厚さが2.0mmを超える場合には、単層で、力学特性(特に、曲げ弾性率及び曲げ強度)に優れた射出成形体を得ることが困難であり、前記射出成形体を射出成形により積層する必要がある。 The total thickness of the laminated molded product of the present invention is not particularly limited, but is preferably 1.1 mm or more, more preferably 1.2 mm or more, even more preferably 1.5 mm or more, even more preferably 2.0 mm or more, particularly preferably 2.5 mm or more, and most preferably 3.0 mm or more. In particular, if the total thickness of the molded product exceeds 2.0 mm, it is difficult to obtain a single-layer injection molded product with excellent mechanical properties (particularly flexural modulus and flexural strength), and it is necessary to laminate the injection molded products by injection molding.
本発明の積層成形体においては、積層成形体全体について、積層成形体の面方向に平行な方向への繊維の配向度が0.75以上であることが必要であり、0.76以上であることが好ましく、0.77以上であることがより好ましく、0.78以上であることが更に好ましい。繊維の配向度が前記下限未満になると、得られる積層成形体において、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にある。 In the laminated molded product of the present invention, the degree of fiber orientation in the direction parallel to the surface direction of the laminated molded product must be 0.75 or more for the entire laminated molded product, preferably 0.76 or more, more preferably 0.77 or more, and even more preferably 0.78 or more. If the degree of fiber orientation is below the lower limit, the mechanical properties (particularly the flexural modulus and flexural strength) of the resulting laminated molded product tend not to be sufficiently improved.
なお、繊維の配向度は以下の方法により求めることができる。すなわち、前記積層成形体において、5つの測定領域(縦2mm×横2mm)を無作為に抽出して切出し、これを試験片として、三次元計測X線CT装置を用いて、各試験片の3次元画像を取得する。得られた3次元画像について、CTデータ解析ソフトウェアを用いて、繊維の配向解析を行い、各試験片における繊維の配向テンソル及びその最大固有値を算出する。ここで、繊維の配向テンソルの最大固有値は、繊維の配向の強さを表す尺度として用いることができる。したがって、本発明においては、これを繊維の配向度とし、5つの測定領域(試験片)のそれぞれにおいて面方向に平行な方向への繊維の配向度を求め、その平均値を積層成形体における面方向に平行な方向への繊維の配向度とする。なお、繊維の配向度の上限は1.0であり、これは、全ての繊維が積層成形体の面方向に平行な方向に配向していることを意味する。 The degree of fiber orientation can be determined by the following method. In other words, five measurement areas (2 mm long x 2 mm wide) are randomly extracted and cut out from the laminated molded body, and these are used as test pieces. A three-dimensional image of each test piece is obtained using a three-dimensional measurement X-ray CT device. The obtained three-dimensional images are subjected to fiber orientation analysis using CT data analysis software, and the fiber orientation tensor and its maximum eigenvalue in each test piece are calculated. Here, the maximum eigenvalue of the fiber orientation tensor can be used as a measure of the strength of fiber orientation. Therefore, in the present invention, this is taken as the degree of fiber orientation, and the degree of fiber orientation in the direction parallel to the surface direction is determined in each of the five measurement areas (test pieces), and the average value is taken as the degree of fiber orientation in the direction parallel to the surface direction in the laminated molded body. The upper limit of the degree of fiber orientation is 1.0, which means that all fibers are oriented in a direction parallel to the surface direction of the laminated molded body.
また、本発明の積層成形体においては、前記射出成形体からなる各層が、その表面の少なくとも一部において互いに直接融着していることが必要であり、各層においては、隣接する層と直接融着している層表面の割合が10%以上であることが好ましく、30%以上であることがより好ましく、50%以上であることが更に好ましく、90%以上であることが特に好ましく、95%以上であることが最も好ましい。隣接する層と直接融着している層表面の割合が前記下限未満になると、積層成形体全体として、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にある。 In addition, in the laminated molded product of the present invention, it is necessary that each layer made of the injection molded product is directly fused to each other at least in a portion of its surface, and in each layer, the proportion of the layer surface that is directly fused to the adjacent layer is preferably 10% or more, more preferably 30% or more, even more preferably 50% or more, particularly preferably 90% or more, and most preferably 95% or more. If the proportion of the layer surface that is directly fused to the adjacent layer is less than the lower limit, the mechanical properties (particularly the flexural modulus and flexural strength) of the laminated molded product as a whole tend not to be sufficiently improved.
〔繊維強化熱可塑性樹脂積層成形体の製造方法〕
次に、本発明の繊維強化熱可塑性樹脂積層成形体の製造方法について説明する。本発明の繊維強化熱可塑性樹脂積層成形体の製造方法は、熱可塑性樹脂と数平均繊維長が0.05~20mmの繊維とを含有し、前記繊維の含有率が1~70質量%であり、厚さが0.5~2mmである下層の成形体を射出成形又は射出プレス成形した後、前記下層の成形体の表面上に、熱可塑性樹脂と数平均繊維長が0.05~20mmの繊維とを含有し、前記繊維の含有率が1~70質量%であり、厚さが0.5~2mmである上層の成形体を射出成形又は射出プレス成形することにより、前記成形体からなる層同士が、その層表面の少なくとも一部において、互いに直接融着している積層成形体を得る方法である。また、本発明の繊維強化熱可塑性樹脂積層成形体の製造方法においては、このような射出成形又は射出プレス成形を繰返すことにより、前記成形体からなる層が3層以上積層された積層成形体を製造することも可能である。
[Method for producing fiber-reinforced thermoplastic resin laminate]
Next, the manufacturing method of the fiber-reinforced thermoplastic resin laminated molded body of the present invention will be described. The manufacturing method of the fiber-reinforced thermoplastic resin laminated molded body of the present invention contains a thermoplastic resin and fibers having a number average fiber length of 0.05 to 20 mm, the fiber content is 1 to 70 mass%, and the thickness is 0.5 to 2 mm. After injection molding or injection press molding of a lower layer molded body having a thermoplastic resin and fibers having a number average fiber length of 0.05 to 20 mm, the fiber content is 1 to 70 mass%, and the thickness is 0.5 to 2 mm, the upper layer molded body is injection molded or injection press molded on the surface of the lower layer molded body, and the layers made of the molded body are directly fused to each other at least in a part of the layer surface. In addition, in the manufacturing method of the fiber-reinforced thermoplastic resin laminated molded body of the present invention, it is also possible to manufacture a laminated molded body in which three or more layers made of the molded body are laminated by repeating such injection molding or injection press molding.
本発明の繊維強化熱可塑性樹脂積層成形体の製造方法においては、先ず、前記熱可塑性樹脂と前記繊維とを含有し、繊維の含有率が1~70質量%であり、厚さが0.5~2mmである下層の成形体を射出成形又は射出プレス成形(好ましくは、射出成形)により作製する。具体的には、前記熱可塑性樹脂と前記繊維とを含有し、繊維の含有率が1~70質量%である繊維強化熱可塑性樹脂を、得られる下層の成形体の厚さが0.5~2mmとなるように射出成形又は射出プレス成形(好ましくは、射出成形)することによって、前記下層の成形体を作製する。 In the manufacturing method of the fiber-reinforced thermoplastic resin laminate of the present invention, first, a lower layer molded body containing the thermoplastic resin and the fibers, having a fiber content of 1 to 70% by mass, and having a thickness of 0.5 to 2 mm is produced by injection molding or injection press molding (preferably injection molding). Specifically, the fiber-reinforced thermoplastic resin containing the thermoplastic resin and the fibers and having a fiber content of 1 to 70% by mass is injection molded or injection press molded (preferably injection molding) so that the thickness of the resulting lower layer molded body is 0.5 to 2 mm, thereby producing the lower layer molded body.
前記繊維強化熱可塑性樹脂としては、前記熱可塑性樹脂と前記繊維とを所定の割合で含有するものであれば、特に制限はなく、市販の繊維強化熱可塑性樹脂であっても、成形直前に前記熱可塑性樹脂と前記繊維とを所定の割合で混合して調製したものであってもよい。 There are no particular limitations on the fiber-reinforced thermoplastic resin, so long as it contains the thermoplastic resin and the fibers in a specified ratio. It may be a commercially available fiber-reinforced thermoplastic resin, or it may be prepared by mixing the thermoplastic resin and the fibers in a specified ratio immediately before molding.
成形時に使用する金型としては特に制限はないが、射出成形と必要に応じて予熱とを行うことが可能な成形体の型を複数有する金型が好ましい。このような金型を用いることによって、一回の成形サイクルで複数の成形体の射出成形と必要に応じて予熱とを同時に実施することが可能である。また、コアバックシステムを採用した金型のように、成形体の厚さを変更することが可能な金型を用いることによって、下層の成形体を作製した後、金型の設定厚さを変更することによって、下層の成形体を金型から脱型せずに、上層の成形体を作製することが可能となる。 There are no particular limitations on the mold used during molding, but a mold having multiple molds for molded bodies that can perform injection molding and preheating as necessary is preferred. By using such a mold, it is possible to simultaneously perform injection molding of multiple molded bodies and preheating as necessary in one molding cycle. In addition, by using a mold that allows the thickness of the molded bodies to be changed, such as a mold that employs a core-back system, it is possible to create an upper layer molded body without removing the lower layer molded body from the mold by changing the set thickness of the mold after creating the lower layer molded body.
成形時の樹脂の溶融温度は、使用する樹脂に応じて適宜設定することができるが、150~450℃であることが好ましい。また、金型温度も、使用する樹脂に応じて適宜設定することができるが、30~280℃であることが好ましく、40~200℃であることがより好ましく、50~150℃であることが更に好ましい。 The melting temperature of the resin during molding can be set appropriately depending on the resin used, but is preferably 150 to 450°C. The mold temperature can also be set appropriately depending on the resin used, but is preferably 30 to 280°C, more preferably 40 to 200°C, and even more preferably 50 to 150°C.
次に、このようにして作製した下層の成形体の表面上に、前記熱可塑性樹脂と前記繊維とを含有し、繊維の含有率が1~70質量%であり、厚さが0.5~2mmである上層の成形体を射出成形又は射出プレス成形(好ましくは、射出成形)により作製する。具体的には、前記下層の成形体の表面上に、前記熱可塑性樹脂と前記繊維とを含有し、繊維の含有率が1~70質量%である前記繊維強化熱可塑性樹脂を、得られる上層の成形体の厚さが0.5~2mmとなるように射出成形又は射出プレス成形(好ましくは、射出成形)することによって、前記上層の成形体を作製する。このように、下層の成形体の表面上に、射出成形又は射出プレス成形により上層の成形体を作製することによって、成形体からなる層同士を、その層表面の少なくとも一部において、互いに直接融着させることができ、力学特性(特に、曲げ弾性率及び曲げ強度)に優れた積層成形体を得ることができる。 Next, an upper layer molded body containing the thermoplastic resin and the fibers, having a fiber content of 1 to 70% by mass, and having a thickness of 0.5 to 2 mm is produced on the surface of the lower layer molded body produced in this manner by injection molding or injection press molding (preferably injection molding). Specifically, the fiber-reinforced thermoplastic resin containing the thermoplastic resin and the fibers and having a fiber content of 1 to 70% by mass is injection molded or injection press molded (preferably injection molding) on the surface of the lower layer molded body so that the thickness of the upper layer molded body obtained is 0.5 to 2 mm, thereby producing the upper layer molded body. In this way, by producing an upper layer molded body on the surface of the lower layer molded body by injection molding or injection press molding, the layers made of molded bodies can be directly fused to each other at least in part of the layer surfaces, and a laminated molded body with excellent mechanical properties (particularly, bending modulus and bending strength) can be obtained.
成形時の樹脂の溶融温度は、使用する樹脂に応じて適宜設定することができるが、150~450℃であることが好ましい。また、金型温度も、使用する樹脂に応じて適宜設定することができるが、30~280℃であることが好ましく、40~200℃であることがより好ましく、50~150℃であることが更に好ましい。 The melting temperature of the resin during molding can be set appropriately depending on the resin used, but is preferably 150 to 450°C. The mold temperature can also be set appropriately depending on the resin used, but is preferably 30 to 280°C, more preferably 40 to 200°C, and even more preferably 50 to 150°C.
また、上層の成形体を作製する際の下層の成形体の表面温度としては特に制限はないが、30~280℃が好ましく、40~200℃がより好ましく、50~150℃が更に好ましい。下層の成形体の表面温度が前記下限未満になると、成形体からなる層同士が十分に融着せず、積層成形体全体として、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にあり、他方、前記上限を超えると、下層の成形体が熱変形して、繊維の配向が乱れるため、得られる積層成形体において、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にある。 The surface temperature of the lower layer molded body when preparing the upper layer molded body is not particularly limited, but is preferably 30 to 280°C, more preferably 40 to 200°C, and even more preferably 50 to 150°C. If the surface temperature of the lower layer molded body is below the lower limit, the layers of the molded body will not be sufficiently fused together, and the mechanical properties (particularly the flexural modulus and flexural strength) of the laminated molded body as a whole will tend not to be sufficiently improved. On the other hand, if the surface temperature exceeds the upper limit, the lower layer molded body will be thermally deformed and the fiber orientation will be disturbed, so that the mechanical properties (particularly the flexural modulus and flexural strength) of the resulting laminated molded body will tend not to be sufficiently improved.
また、本発明の繊維強化熱可塑性樹脂積層成形体の製造方法においては、前記下層の成形体を、前記熱可塑性樹脂の融点や軟化点以下の温度で予熱した後、前記上層の成形体を射出成形又は射出プレス成形することが好ましい。これにより、成形体からなる層同士を、その層表面の少なくとも一部において、互いに直接融着させることができ、力学特性(特に、曲げ弾性率及び曲げ強度)に優れた積層成形体を得ることができる。 In addition, in the manufacturing method of the fiber-reinforced thermoplastic resin laminate of the present invention, it is preferable to preheat the lower layer molded body at a temperature below the melting point or softening point of the thermoplastic resin, and then injection mold or injection press mold the upper layer molded body. This allows the layers of molded bodies to be directly fused to each other at least in part of their layer surfaces, and a laminated molded body with excellent mechanical properties (particularly flexural modulus and flexural strength) can be obtained.
予熱温度として具体的には、下層の積層体の表面温度が、前記熱可塑性樹脂のガラス転移温度(Tg)より5~100℃高い温度(Tg+5℃~Tg+100℃)となる温度が好ましく、前記Tgより10~60℃高い温度(Tg+10℃~Tg+60℃)となる温度がより好ましく、前記Tgより15~50℃高い温度(Tg+15℃~Tg+50℃)となる温度が更に好ましく、前記Tgより20~45℃高い温度(Tg+20℃~Tg+45℃)となる温度が特に好ましい。予熱温度が前記下限未満になると、成形体からなる層同士が十分に融着せず、積層成形体全体として、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にあり、他方、前記上限を超えると、下層の成形体が熱変形して、繊維の配向が乱れるため、得られる積層成形体において、力学特性(特に、曲げ弾性率及び曲げ強度)が十分に向上しない傾向にある。 Specifically, the preheating temperature is preferably a temperature at which the surface temperature of the lower laminate is 5 to 100°C higher than the glass transition temperature (Tg) of the thermoplastic resin (Tg + 5°C to Tg + 100°C), more preferably a temperature at which the surface temperature is 10 to 60°C higher than the Tg (Tg + 10°C to Tg + 60°C), even more preferably a temperature at which the surface temperature is 15 to 50°C higher than the Tg (Tg + 15°C to Tg + 50°C), and particularly preferably a temperature at which the surface temperature is 20 to 45°C higher than the Tg (Tg + 20°C to Tg + 45°C). If the preheating temperature is below the lower limit, the layers of the molded body will not be sufficiently fused together, and the mechanical properties (particularly the flexural modulus and flexural strength) of the laminated molded body as a whole will tend not to be sufficiently improved. On the other hand, if the preheating temperature exceeds the upper limit, the lower molded body will be thermally deformed and the fiber orientation will be disturbed, so the mechanical properties (particularly the flexural modulus and flexural strength) of the resulting laminated molded body will tend not to be sufficiently improved.
以下、実施例及び比較例に基づいて本発明をより具体的に説明するが、本発明は以下の実施例に限定されるものではない。 The present invention will be described in more detail below with reference to examples and comparative examples, but the present invention is not limited to the following examples.
(実施例1)
先ず、炭素繊維(CF)含有率が30質量%の炭素繊維強化ポリアミド6(東レ株式会社製「長繊維CF強化6ナイロン トレカTLP1060」)にポリアミド6(東レ株式会社製「アミランCM1001」)を混合して、CF含有率が10質量%の炭素繊維強化ポリアミド6を調製した。
Example 1
First, a carbon fiber reinforced polyamide 6 having a carbon fiber (CF) content of 30 mass% ("long fiber CF reinforced 6 nylon Torayca TLP1060" manufactured by Toray Industries, Inc.) was mixed with polyamide 6 ("Amilan CM1001" manufactured by Toray Industries, Inc.) to prepare a carbon fiber reinforced polyamide 6 having a CF content of 10 mass%.
次に、この炭素繊維強化ポリアミド6を用いて、溶融温度280℃、金型温度80℃の条件で射出成形を行い、図3(A)に示すように、厚さが2mmの多目的試験片形状の下層用成形体3を作製した。得られた下層用成形体3を金型に挿入し、この下層用成形体3の表面温度が50℃なるように加熱しながら、図(B)に示すように、前記炭素繊維強化ポリアミド6(CF含有率:10質量%)を溶融温度280℃の条件で前記下層用成形体3の表面上に射出成形して、厚さが2mmの上層の成形体4を積層し、図(C)に示すように、前記下層用成形体3と前記上層の成形体4とが直接融着している多目的試験片形状の積層成形体(全長:170mm、平行部の長さ:80mm、端部の幅:20mm、中央の平行部の幅:10mm、厚さ:4mm)を作製した。 Next, using this carbon fiber reinforced polyamide 6, injection molding was performed under conditions of a melting temperature of 280°C and a mold temperature of 80°C, and a lower layer molded body 3 with a multipurpose test piece shape and a thickness of 2 mm was produced as shown in Figure 3 (A). The obtained lower layer molded body 3 was inserted into a mold, and while heating the surface temperature of this lower layer molded body 3 to 50°C, as shown in Figure (B), the carbon fiber reinforced polyamide 6 (CF content: 10 mass%) was injection molded on the surface of the lower layer molded body 3 under conditions of a melting temperature of 280°C, and an upper layer molded body 4 with a thickness of 2 mm was laminated, and as shown in Figure (C), a laminated molded body (total length: 170 mm, length of parallel part: 80 mm, width of end: 20 mm, width of central parallel part: 10 mm, thickness: 4 mm) with a multipurpose test piece shape in which the lower layer molded body 3 and the upper layer molded body 4 are directly fused was produced.
(実施例2)
CF含有率が30質量%の炭素繊維強化ポリアミド6(東レ株式会社製「長繊維CF強化6ナイロン トレカTLP1060」)にポリアミド6(東レ株式会社製「アミランCM1001」)を混合して、CF含有率が20質量%の炭素繊維強化ポリアミド6を調製した。
Example 2
Carbon fiber reinforced polyamide 6 with a CF content of 20 mass% was prepared by mixing polyamide 6 with a CF content of 30 mass% (long fiber CF reinforced 6 nylon Torayca TLP1060 manufactured by Toray Industries, Inc.) and polyamide 6 with a CF content of 20 mass% (Amilan CM1001 manufactured by Toray Industries, Inc.).
CF含有率が10質量%の炭素繊維強化ポリアミド6の代わりに、この炭素繊維強化ポリアミド6(CF含有率:20質量%)を用いた以外は実施例1と同様にして、前記下層用成形体3(厚さ:2mm)と前記上層の成形体4(厚さ:2mm)とが直接融着している多目的試験片形状の積層成形体(厚さ:4mm)を作製した。積層成形体を作製した。 A laminated molded body (thickness: 4 mm) in the shape of a multipurpose test piece was produced in the same manner as in Example 1, except that this carbon fiber reinforced polyamide 6 (CF content: 20% by mass) was used instead of the carbon fiber reinforced polyamide 6 with a CF content of 10% by mass, in which the lower layer molded body 3 (thickness: 2 mm) and the upper layer molded body 4 (thickness: 2 mm) were directly fused together. A laminated molded body was produced.
(実施例3)
CF含有率が10質量%の炭素繊維強化ポリアミド6の代わりに、CF含有率が30質量%の炭素繊維強化ポリアミド6(東レ株式会社製「長繊維CF強化6ナイロン トレカTLP1060」)を、ポリアミド6を混合せずに、そのまま用いた以外は実施例1と同様にして、前記下層用成形体3(厚さ:2mm)と前記上層の成形体4(厚さ:2mm)とが直接融着している多目的試験片形状の積層成形体(厚さ:4mm)を作製した。
Example 3
A multipurpose test piece-shaped laminated molded body (thickness: 4 mm) in which the lower layer molded body 3 (thickness: 2 mm) and the upper layer molded body 4 (thickness: 2 mm) were directly fused to each other was produced in the same manner as in Example 1, except that a carbon fiber reinforced polyamide 6 having a CF content of 30 mass% ("long fiber CF reinforced 6 nylon Torayca TLP1060" manufactured by Toray Industries, Inc.) was used as is without mixing it with polyamide 6 instead of the carbon fiber reinforced polyamide 6 having a CF content of 10 mass%.
(実施例4)
下層用成形体を金型に挿入し、この下層用成形体の表面温度が80℃なるように予熱した後、前記炭素繊維強化ポリアミド6(CF含有率:30質量%)を溶融温度280℃の条件で前記下層用成形体の表面上に射出成形した以外は実施例3と同様にして、前記下層用成形体3(厚さ:2mm)と前記上層の成形体4(厚さ:2mm)とが直接融着している多目的試験片形状の積層成形体(厚さ:4mm)を作製した。
Example 4
A multipurpose test piece-shaped laminated molded body (thickness: 4 mm) in which the lower layer molded body 3 (thickness: 2 mm) and the upper layer molded body 4 (thickness: 2 mm) were directly fused to each other was produced in the same manner as in Example 3, except that the lower layer molded body was inserted into a mold and preheated so that the surface temperature of the lower layer molded body was 80°C. The carbon fiber reinforced polyamide 6 (CF content: 30% by mass) was then injection molded onto the surface of the lower layer molded body at a melting temperature of 280°C.
(比較例1)
実施例1と同様にして調製した炭素繊維強化ポリアミド6(CF含有率:10質量%)を用いて、溶融温度280℃、金型温度80℃の条件で射出成形を行い、多目的試験片形状の単層の成形体(全長:170mm、平行部の長さ:80mm、端部の幅:20mm、中央の平行部の幅:10mm、厚さ:4mm)を作製した。
(Comparative Example 1)
Carbon fiber reinforced polyamide 6 (CF content: 10% by mass) prepared in the same manner as in Example 1 was injection molded under conditions of a melt temperature of 280°C and a mold temperature of 80°C to produce a single-layer molded body in the shape of a multipurpose test specimen (total length: 170 mm, parallel portion length: 80 mm, end width: 20 mm, central parallel portion width: 10 mm, thickness: 4 mm).
(比較例2)
実施例2と同様にして調製した炭素繊維強化ポリアミド6(CF含有率:20質量%)を用いて、溶融温度280℃、金型温度80℃の条件で射出成形を行い、多目的試験片形状の単層の成形体(全長:170mm、平行部の長さ:80mm、端部の幅:20mm、中央の平行部の幅:10mm、厚さ:4mm)を作製した。
(Comparative Example 2)
Carbon fiber reinforced polyamide 6 (CF content: 20% by mass) prepared in the same manner as in Example 2 was injection molded under conditions of a melt temperature of 280°C and a mold temperature of 80°C to produce a single-layer molded body in the shape of a multipurpose test specimen (total length: 170 mm, parallel portion length: 80 mm, end width: 20 mm, central parallel portion width: 10 mm, thickness: 4 mm).
(比較例3)
CF含有率が30質量%の炭素繊維強化ポリアミド6(東レ株式会社製「長繊維CF強化6ナイロン トレカTLP1060」)を用いて、溶融温度280℃、金型温度80℃の条件で射出成形を行い、多目的試験片形状の単層の成形体(全長:170mm、平行部の長さ:80mm、端部の幅:20mm、中央の平行部の幅:10mm、厚さ:4mm)を作製した。
(Comparative Example 3)
Carbon fiber reinforced polyamide 6 with a CF content of 30 mass% ("long fiber CF reinforced 6 nylon Torayca TLP1060" manufactured by Toray Industries, Inc.) was injection molded at a melt temperature of 280°C and a mold temperature of 80°C to produce a single-layer molded body in the shape of a multipurpose test specimen (total length: 170 mm, length of parallel portion: 80 mm, width of end portion: 20 mm, width of central parallel portion: 10 mm, thickness: 4 mm).
(比較例4)
CF含有率が30質量%の炭素繊維強化ポリアミド6(東レ株式会社製「長繊維CF強化6ナイロン トレカTLP1060」)を用いて、溶融温度280℃、金型温度80℃の条件で射出成形を行い、厚さが2mmの多目的試験片形状の成形体を2枚作製した。この2枚の成形体を重ね合わせて、多目的試験片形状の積層成形体(全長:170mm、平行部の長さ:80mm、端部の幅:20mm、中央の平行部の幅:10mm、厚さ:4mm)を作製した。
(Comparative Example 4)
Using carbon fiber reinforced polyamide 6 with a CF content of 30% by mass ("long fiber CF reinforced 6 nylon Torayca TLP1060" manufactured by Toray Industries, Inc.), injection molding was performed under conditions of a melt temperature of 280° C. and a mold temperature of 80° C. to produce two molded bodies in the shape of a multipurpose test piece with a thickness of 2 mm. These two molded bodies were stacked together to produce a laminated molded body in the shape of a multipurpose test piece (total length: 170 mm, length of parallel part: 80 mm, width of end part: 20 mm, width of central parallel part: 10 mm, thickness: 4 mm).
(比較例5)
比較例4と同様にして、厚さが2mmの多目的試験片形状の成形体を2枚作製した。この2枚の成形体を、接着剤(セメダイン株式会社製「SuperX」)を用いて接着し、多目的試験片形状の積層成形体(全長:170mm、平行部の長さ:80mm、端部の幅:20mm、中央の平行部の幅:10mm、厚さ:4mm)を作製した。
(Comparative Example 5)
Two molded bodies having a multipurpose test piece shape and a thickness of 2 mm were prepared in the same manner as in Comparative Example 4. The two molded bodies were bonded together using an adhesive ("SuperX" manufactured by Cemedine Co., Ltd.) to prepare a laminated molded body having a multipurpose test piece shape (total length: 170 mm, length of parallel portion: 80 mm, width of end portion: 20 mm, width of central parallel portion: 10 mm, thickness: 4 mm).
<繊維の数平均繊維長>
得られた多目的試験片形状の積層成形体の平行部から試験片(縦10mm×横10mm×厚さ4mm)を切出し、空気気流下、500℃で加熱して樹脂部を灰化除去した。残存した繊維を撮影し、画像解析ソフトを用いて、無作為に抽出した6千本の繊維について繊維長を測定して、その数平均値を求め、これを繊維の数平均繊維長とした。その結果を表1に示す。
<Number average fiber length of fibers>
A test piece (10 mm long x 10 mm wide x 4 mm thick) was cut out from the parallel part of the multipurpose test piece-shaped laminate and heated at 500°C under air flow to remove the resin part by incineration. The remaining fibers were photographed and the fiber lengths of 6,000 randomly selected fibers were measured using image analysis software to determine the number average value, which was used as the number average fiber length of the fibers. The results are shown in Table 1.
<積層成形体における繊維の配向度>
得られた積層成形体から、無作為に抽出した5つの測定領域(縦2mm×横2mm)を切出し、これを試験片(縦2mm×横2mm×厚さ4mm)として、三次元計測X線CT装置(ヤマト科学株式会社製「TDM1000H-II」)を用いて、各試験片の3次元画像を取得した。得られた3次元画像について、CTデータ解析ソフトウェア(ボリュームグラフィックス株式会社製「VGSTUDIO MAX」)を用いて、繊維の配向解析を行い、各試験片における繊維の配向テンソル及びその最大固有値を算出した。繊維の配向テンソルの最大固有値は、繊維の配向の強さを表す尺度として用いることができ、本発明においては、これを繊維の配向度とした。5つの測定領域(試験片)のそれぞれにおいて面方向に平行な方向への繊維の配向度を求め、その平均値を積層成形体における面方向に平行な方向への繊維の配向度とした。その結果を表1に示す。
<Degree of fiber orientation in laminated molded body>
From the obtained laminated molded body, five randomly extracted measurement areas (2 mm long x 2 mm wide) were cut out, and these were used as test pieces (2 mm long x 2 mm wide x 4 mm thick). A three-dimensional measurement X-ray CT device (Yamato Scientific Co., Ltd. "TDM1000H-II") was used to obtain three-dimensional images of each test piece. For the obtained three-dimensional images, fiber orientation analysis was performed using CT data analysis software (Volume Graphics Co., Ltd. "VGSTUDIO MAX") to calculate the fiber orientation tensor and its maximum eigenvalue in each test piece. The maximum eigenvalue of the fiber orientation tensor can be used as a measure of the strength of fiber orientation, and in the present invention, this was taken as the degree of fiber orientation. The degree of fiber orientation in the direction parallel to the surface direction was determined in each of the five measurement areas (test pieces), and the average value was taken as the degree of fiber orientation in the direction parallel to the surface direction in the laminated molded body. The results are shown in Table 1.
<融着領域の割合>
得られた積層成形体の積層間を剥離し、剥離面をデジタル式マイクロスコープ(キーエンス株式会社製「VHX-7000)を用いて観察し、剥離面の輝度の差に基づいて融着領域を特定し、剥離面全体に占める融着領域の割合を求めた。その結果を表1に示す。
<Proportion of fused area>
The layers of the obtained laminated molded body were peeled away from each other, and the peeled surface was observed using a digital microscope ("VHX-7000" manufactured by Keyence Corporation). The fused regions were identified based on the difference in brightness of the peeled surface, and the proportion of the fused regions in the entire peeled surface was calculated. The results are shown in Table 1.
<曲げ弾性率及び曲げ強度>
得られた積層成形体を用いて、試験速度:2mm/min、支持間距離:64mm、温度:23℃で3点曲げ試験を行い、曲げ弾性率及び曲げ強さを測定した。その結果を表1に示す。
<Flexural modulus and flexural strength>
The obtained laminate was subjected to a three-point bending test at a test speed of 2 mm/min, a support distance of 64 mm, and a temperature of 23° C. to measure the flexural modulus and flexural strength. The results are shown in Table 1.
表1に示したように、熱可塑性樹脂と炭素繊維とを含有する、特定の厚さの下層用成形体を射出成形した後、この下層用成形体上に、熱可塑性樹脂と炭素繊維とを含有する、特定の厚さの上層の成形体を射出成形することによって、面方向への炭素繊維の配向度が高く、力学特性(特に、曲げ特性)に優れた積層成形体が得られることがわかった(実施例1~4)。 As shown in Table 1, it was found that by injection molding a lower layer molded body of a specific thickness containing thermoplastic resin and carbon fiber, and then injection molding an upper layer molded body of a specific thickness containing thermoplastic resin and carbon fiber on top of this lower layer molded body, it is possible to obtain a laminated molded body with a high degree of carbon fiber orientation in the planar direction and excellent mechanical properties (especially bending properties) (Examples 1 to 4).
また、下層用成形体を所定の温度に予熱した後、上層の成形体を射出成形した場合(実施例4)には、下層用成形体を所定の温度に予熱しなかった場合(実施例3)に比べて、力学特性(特に、曲げ特性)が向上することがわかった。 In addition, it was found that when the lower layer molded body was preheated to a specified temperature and then the upper layer molded body was injection molded (Example 4), the mechanical properties (especially the bending properties) were improved compared to when the lower layer molded body was not preheated to the specified temperature (Example 3).
一方、熱可塑性樹脂と炭素繊維とを含有する単層の射出成形体(比較例1~3)は、実施例1~3で得られた積層成形体に比べて、面方向への炭素繊維の配向度が低く、力学特性(特に、曲げ特性)に劣ることがわかった。 On the other hand, it was found that the single-layer injection molded products containing thermoplastic resin and carbon fiber (Comparative Examples 1 to 3) had a lower degree of carbon fiber orientation in the planar direction and were inferior in mechanical properties (especially bending properties) compared to the laminated molded products obtained in Examples 1 to 3.
また、熱可塑性樹脂と炭素繊維とを含有する、特定の厚さの射出成形体を、重ね合わせた場合(比較例4)や、接着剤により接着した場合(比較例5)には、面方向への炭素繊維の配向度が高い積層成形体が得られるものの、この積層成形体は、実施例1~3で得られた積層成形体に比べて、力学特性(特に、曲げ特性)に劣ることがわかった。 In addition, when injection molded bodies of a specific thickness containing thermoplastic resin and carbon fiber were stacked (Comparative Example 4) or bonded with an adhesive (Comparative Example 5), a laminated molded body with a high degree of orientation of the carbon fibers in the planar direction was obtained, but it was found that this laminated molded body had inferior mechanical properties (particularly bending properties) compared to the laminated molded bodies obtained in Examples 1 to 3.
以上説明したように、本発明によれば、力学特性(特に、曲げ弾性率及び曲げ強度)に優れた繊維強化熱可塑性樹脂からなる成形体を得ることが可能となる。したがって、本発明の繊維強化熱可塑性樹脂積層成形体は、大きな衝撃が加わるような部材、例えば、自動車用部材、電車用部材、航空宇宙用部材、産業機械用部材、建築用部材、家電用素材、スポーツ・レジャー用素材、圧力容器、保護具用素材等として特に有用である。 As described above, according to the present invention, it is possible to obtain a molded product made of fiber-reinforced thermoplastic resin with excellent mechanical properties (particularly flexural modulus and flexural strength). Therefore, the fiber-reinforced thermoplastic resin laminate molded product of the present invention is particularly useful as a component that is subjected to a large impact, such as an automobile component, a train component, an aerospace component, an industrial machinery component, a construction component, a material for home appliances, a material for sports and leisure, a pressure vessel, a material for protective equipment, etc.
1:熱可塑性樹脂、2:繊維、3:下層用成形体、4:上層の成形体 1: Thermoplastic resin, 2: Fiber, 3: Lower layer molded body, 4: Upper layer molded body
Claims (7)
前記積層成形体が、下層の前記射出成形体の表面上に上層の前記射出成形体を射出成形又は射出プレス成形により形成したものであり、
前記積層成形体全体について、前記積層成形体の面方向に平行な方向への前記繊維の配向度が0.75以上であり、
各層の表面の少なくとも一部が互いに直接融着していることを特徴とする繊維強化熱可塑性樹脂積層成形体。 a laminated molded article including two or more layers of injection molded articles each containing polyamide and fibers having a number average fiber length of 0.05 to 20 mm, the fiber content being 1 to 70 mass %, and the thickness being 0.5 to 2 mm;
the laminated molded body is formed by forming an upper layer injection molded body on a surface of a lower layer injection molded body by injection molding or injection press molding,
With respect to the entire laminated molded body, the orientation degree of the fibers in a direction parallel to the surface direction of the laminated molded body is 0.75 or more,
A fiber-reinforced thermoplastic resin laminate, characterized in that at least a portion of the surface of each layer is directly fused to the other layer.
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| JP2004243686A (en) | 2003-02-14 | 2004-09-02 | Mitsubishi Engineering Plastics Corp | Thick resin molded product |
| JP2012006331A (en) | 2010-06-28 | 2012-01-12 | Mitsubishi Heavy Ind Ltd | Fiber-reinforced composite material |
| WO2012117975A1 (en) | 2011-02-28 | 2012-09-07 | 東レ株式会社 | Injection formed body and fabrication method for same |
| JP2015009436A (en) | 2013-06-28 | 2015-01-19 | 東レ株式会社 | Fiber-reinforced resin molding, and method for producing the same |
| JP2016221970A (en) | 2015-06-02 | 2016-12-28 | 東レ株式会社 | Manufacturing method of composite molded body and carbon fiber reinforced thermoplastic resin composition for internal heating deposition |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2004243686A (en) | 2003-02-14 | 2004-09-02 | Mitsubishi Engineering Plastics Corp | Thick resin molded product |
| JP2012006331A (en) | 2010-06-28 | 2012-01-12 | Mitsubishi Heavy Ind Ltd | Fiber-reinforced composite material |
| WO2012117975A1 (en) | 2011-02-28 | 2012-09-07 | 東レ株式会社 | Injection formed body and fabrication method for same |
| JP2015009436A (en) | 2013-06-28 | 2015-01-19 | 東レ株式会社 | Fiber-reinforced resin molding, and method for producing the same |
| JP2016221970A (en) | 2015-06-02 | 2016-12-28 | 東レ株式会社 | Manufacturing method of composite molded body and carbon fiber reinforced thermoplastic resin composition for internal heating deposition |
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