JP2016124182A - Bonded structure bonding method - Google Patents

Bonded structure bonding method Download PDF

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JP2016124182A
JP2016124182A JP2014266309A JP2014266309A JP2016124182A JP 2016124182 A JP2016124182 A JP 2016124182A JP 2014266309 A JP2014266309 A JP 2014266309A JP 2014266309 A JP2014266309 A JP 2014266309A JP 2016124182 A JP2016124182 A JP 2016124182A
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adhesive
composite material
thermoplastic resin
bonded
melted
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JP6540024B2 (en
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貴文 福本
Takafumi Fukumoto
貴文 福本
諸星 勝己
Katsumi Morohoshi
勝己 諸星
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Nissan Motor Co Ltd
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Abstract

PROBLEM TO BE SOLVED: To provide a bonded structure capable of improving adhesiveness between a composite material formed by impregnating a reinforced substrate with a thermoplastic resin and an adhesive while suppressing an increase in cost and complication of a production process.SOLUTION: A bonded structure 1 is formed by bonding a composite material 10 obtained by impregnating a reinforced substrate 11 with a thermoplastic resin 12 and a composite material 30 obtained by impregnating a reinforced substrate 31 with a thermoplastic resin 32 through an adhesive 20. A reinforced substrate 11A on the surface of the composite material where the thermoplastic resin is melted on a surface 13 on the adhesive side is embedded in the adhesive.SELECTED DRAWING: Figure 2

Description

本発明は、接着構造体及び接着方法に関する。   The present invention relates to a bonding structure and a bonding method.

近年、自動車の車体軽量化のために強化基材に樹脂を含浸させた複合材料が自動車部品として用いられており、自動車部品は、複合材料同士を、接着剤を介して接合することによって形成される。   In recent years, a composite material in which a reinforced base material is impregnated with a resin has been used as an automobile part to reduce the weight of the automobile body, and the automobile part is formed by joining the composite materials together with an adhesive. The

また、複合材料を構成する樹脂として、現在はその機械的特性の高さから、熱硬化性樹脂が主に用いられている。しかしながら、熱硬化性樹脂では、材料コストや硬化させるのに時間がかかるといった理由から、熱可塑性樹脂に置き換えられると予想されている。   Further, as a resin constituting the composite material, a thermosetting resin is mainly used at present because of its high mechanical properties. However, the thermosetting resin is expected to be replaced with a thermoplastic resin because of the material cost and the time required for curing.

ところが、この熱可塑性樹脂は、一般的に接着剤に対して接着性が低く、強化基材に熱可塑性樹脂を含浸させた複合材料も、表面に熱可塑性樹脂が形成されるため、同様に接着剤に対して接着性が低くなる。   However, this thermoplastic resin generally has low adhesion to adhesives, and a composite material in which a reinforced base material is impregnated with a thermoplastic resin also forms a thermoplastic resin on the surface. Adhesiveness to the agent is lowered.

これに関連して、例えば下記の特許文献1には、誘電加熱性を有し加圧によって複合材料に食い込み可能な顆粒・繊維状の誘電加熱媒体が混合された接着剤を用いる接合方法が開示されている。   In relation to this, for example, the following Patent Document 1 discloses a bonding method using an adhesive mixed with a granular / fibrous dielectric heating medium having a dielectric heating property and capable of biting into a composite material by pressing. Has been.

この方法によれば、誘電加熱媒体が混合された接着剤を一対の複合材料の間に配置して、誘導加熱で加熱しつつ加圧することによって、誘電加熱媒体が複合材料に食い込むため、複合材料及び接着剤間の接着が実現可能となる。   According to this method, the adhesive mixed with the dielectric heating medium is disposed between the pair of composite materials, and the dielectric heating medium bites into the composite material by applying pressure while heating by induction heating. And adhesion between adhesives can be realized.

特開2013−166904号公報JP 2013-166904 A

しかしながら、特許文献1に記載の接合方法では、接着剤に、複合材料に食い込み可能な顆粒・繊維状の誘電加熱媒体が混合されるため、コストの増加や製造工程の煩雑化が懸念される。   However, in the joining method described in Patent Document 1, since an adhesive is mixed with a granular / fibrous dielectric heating medium that can bite into the composite material, there is a concern about an increase in cost and a complicated manufacturing process.

本発明は、上記の課題を解決するためになされたものであり、コストの増加や製造工程の煩雑化を抑制しつつ、強化基材に熱可塑性樹脂を含浸させた複合材料の接着剤に対する接着性を向上させることのできる接着構造体及び接着方法を提供することを目的とする。   The present invention has been made to solve the above-described problems, and is capable of adhering a composite material in which a reinforced base material is impregnated with a thermoplastic resin to an adhesive while suppressing an increase in cost and complication of a manufacturing process. It is an object of the present invention to provide a bonding structure and a bonding method capable of improving the property.

上記目的を達成する本発明に係る接着構造体は、強化基材に熱可塑性樹脂を含浸させた複合材料及び被接着部材が、接着剤を介して接着されてなる接着構造体である。接着構造体は、前記接着剤側の表面における前記熱可塑性樹脂が溶融した前記複合材料の、前記表面における前記強化基材が、前記接着剤内に埋設されてなる。   An adhesive structure according to the present invention that achieves the above object is an adhesive structure in which a composite material in which a reinforced base material is impregnated with a thermoplastic resin and a member to be bonded are bonded via an adhesive. In the adhesive structure, the reinforcing base material on the surface of the composite material in which the thermoplastic resin on the surface on the adhesive side is melted is embedded in the adhesive.

また、上記目的を達成する本発明に係る接着方法は、強化基材に熱可塑性樹脂を含浸させた複合材料及び被接着部材を、接着剤を介して接着する接着方法である。接着方法は、前記接着剤側の表面における前記熱可塑性樹脂が溶融された前記複合材料の、前記表面における前記強化基材を、前記接着剤内に埋設する。   In addition, the bonding method according to the present invention that achieves the above object is a bonding method in which a composite material in which a reinforced base material is impregnated with a thermoplastic resin and a member to be bonded are bonded via an adhesive. In the bonding method, the reinforced substrate on the surface of the composite material in which the thermoplastic resin on the surface on the adhesive side is melted is embedded in the adhesive.

上記の接着構造体及び接着方法によれば、複合材料の強化基材が、接着剤内に埋設されるため、複合材料の接着剤に対する接着性を向上させることができる。また、接着剤には、先行技術文献の誘電加熱媒体のような別材料が混合されないため、コストの増加や製造工程の煩雑化を抑制することができる。したがって、コストの増加や製造工程の煩雑化を抑制しつつ、強化基材に熱可塑性樹脂を含浸させた複合材料の接着剤に対する接着性を向上させることのできる接着構造体及び接着方法を提供することができる。   According to the bonding structure and the bonding method described above, since the reinforced base material of the composite material is embedded in the adhesive, the adhesion of the composite material to the adhesive can be improved. Moreover, since another material like the dielectric heating medium of a prior art document is not mixed with an adhesive agent, the increase in cost and complication of a manufacturing process can be suppressed. Therefore, it is possible to provide an adhesion structure and an adhesion method capable of improving the adhesiveness to an adhesive of a composite material in which a reinforced base material is impregnated with a thermoplastic resin while suppressing an increase in cost and complication of a manufacturing process. be able to.

本発明の実施形態に係る接着構造体を示す斜視図である。It is a perspective view showing the adhesion structure concerning the embodiment of the present invention. 本実施形態に係る接着構造体の内部の様子を示す概略図である。It is the schematic which shows the mode of the inside of the adhesion structure concerning this embodiment. 第1実施形態に係る接着方法を用いる際の接合装置を示す図である。It is a figure which shows the joining apparatus at the time of using the adhesion | attachment method which concerns on 1st Embodiment. 第1実施形態に係る接着方法のフローチャートである。It is a flowchart of the adhesion | attachment method which concerns on 1st Embodiment. 複合材料の表面の熱可塑性樹脂を溶融する様子を示す図である。It is a figure which shows a mode that the thermoplastic resin of the surface of a composite material is fuse | melted. 複合材料の表面に接着剤を配置する様子を示す図である。It is a figure which shows a mode that an adhesive agent is arrange | positioned on the surface of a composite material. 接着剤の複合材料が設けられる側と反対側の面に他の複合材料を配置する様子を示す図である。It is a figure which shows a mode that another composite material is arrange | positioned on the surface on the opposite side to the side in which the composite material of an adhesive agent is provided. 第2実施形態に係る接着方法を用いる際の接合装置を示す図である。It is a figure which shows the joining apparatus at the time of using the adhesion | attachment method which concerns on 2nd Embodiment. 第2実施形態に係る接着方法のフローチャートである。It is a flowchart of the adhesion | attachment method which concerns on 2nd Embodiment. 複合材料、接着剤、及び他の複合材料の順に積層する様子を示す図である。It is a figure which shows a mode that a composite material, an adhesive agent, and another composite material are laminated | stacked in order. 複合材料、接着剤、及び他の複合材料を加熱しつつ、複合材料及び他の複合材料を互いに向かう方向に押圧する様子を示す図である。It is a figure which shows a mode that a composite material and another composite material are pressed in the direction toward each other, heating a composite material, an adhesive agent, and another composite material. 複合材料の強化基材が、接着剤内に埋設する様子を示す図である。It is a figure which shows a mode that the reinforcement base material of a composite material is embed | buried in an adhesive agent. 接着剤が離散的に配置される様子を示す図である。It is a figure which shows a mode that an adhesive agent is arrange | positioned discretely. 比較例に係る接着構造体のせん断試験の結果を示す図である。It is a figure which shows the result of the shear test of the adhesion structure which concerns on a comparative example. 実施例に係る接着構造体のせん断試験の結果を示す図である。It is a figure which shows the result of the shear test of the adhesion structure which concerns on an Example.

以下、添付した図面を参照しながら、本発明の実施形態を説明する。なお、図面の説明において同一の要素には同一の符号を付し、重複する説明を省略する。図面の寸法比率は、説明の都合上誇張されており、実際の比率とは異なる場合がある。   Hereinafter, embodiments of the present invention will be described with reference to the accompanying drawings. In the description of the drawings, the same elements are denoted by the same reference numerals, and redundant description is omitted. The dimensional ratios in the drawings are exaggerated for convenience of explanation, and may differ from actual ratios.

図1は、本発明の実施形態に係る接着構造体1を示す斜視図である。図2は、本実施形態に係る接着構造体の内部の様子を示す概略図である。なお、図1において、複合材料10,30及び接着剤20は簡略化して示す。また、図2において、理解の容易のため、強化基材11は黒丸で示し規則正しく構成されているが、実際は不規則に構成されている。以下の図面においても同様に、理解の容易のため、強化基材11は黒丸で示し規則正しく構成されている。   FIG. 1 is a perspective view showing an adhesive structure 1 according to an embodiment of the present invention. FIG. 2 is a schematic view showing an internal state of the bonded structure according to the present embodiment. In FIG. 1, the composite materials 10 and 30 and the adhesive 20 are shown in a simplified manner. In FIG. 2, for the sake of easy understanding, the reinforced base material 11 is indicated by black circles and is regularly configured, but actually, it is irregularly configured. Similarly, in the following drawings, the reinforcing base material 11 is indicated by a black circle and is configured regularly for easy understanding.

まず、図1及び図2を参照して、本実施形態に係る接着構造体1の構成について説明する。   First, with reference to FIG.1 and FIG.2, the structure of the adhesion structure 1 which concerns on this embodiment is demonstrated.

本実施形態に係る接着構造体1は、概説すると、図1及び図2に示すように、強化基材11に熱可塑性樹脂12を含浸させた複合材料10及び強化基材31に熱可塑性樹脂32を含浸させた複合材料(被接着部材)30が、接着剤20を介して接着されてなる。そして、接着剤20側の表面13,33における熱可塑性樹脂12,32が溶融した複合材料10,30の、表面13,33における強化基材11A,31Aが、接着剤20内に埋設されてなる。複合材料10及び複合材料30は同様の構成を備えるため、以下、複合材料10の説明を行い、複合材料30の説明は省略する。   In summary, the bonded structure 1 according to the present embodiment, as shown in FIGS. 1 and 2, includes a composite material 10 in which a reinforced base material 11 is impregnated with a thermoplastic resin 12 and a reinforced base material 31 with a thermoplastic resin 32. A composite material (bonded member) 30 impregnated with is bonded via an adhesive 20. Then, the reinforcing base materials 11A and 31A on the surfaces 13 and 33 of the composite materials 10 and 30 in which the thermoplastic resins 12 and 32 on the surfaces 13 and 33 on the adhesive 20 side are melted are embedded in the adhesive 20. . Since the composite material 10 and the composite material 30 have the same configuration, the composite material 10 will be described below, and the description of the composite material 30 will be omitted.

複合材料10は、強化基材11及び熱可塑性樹脂12が組み合わされることによって、熱可塑性樹脂12単体に比べて高い強度及び剛性を備える。   The composite material 10 has higher strength and rigidity than the thermoplastic resin 12 alone by combining the reinforced base material 11 and the thermoplastic resin 12.

強化基材11は、炭素繊維、ガラス繊維、有機繊維などの織物シートによって形成される。   The reinforced substrate 11 is formed of a woven fabric sheet such as carbon fiber, glass fiber, or organic fiber.

熱可塑性樹脂12は、例えば、ポリエチレン、ポリプロピレン、フェノール樹脂などを用いることができる。   As the thermoplastic resin 12, for example, polyethylene, polypropylene, phenol resin, or the like can be used.

接着剤20は、熱硬化性接着剤であって、例えば、エポキシ樹脂系接着剤等を適宜用いることができる。   The adhesive 20 is a thermosetting adhesive, and for example, an epoxy resin adhesive can be used as appropriate.

次に、図3〜図7を参照して、本発明の第1実施形態に係る接合装置100及び接着方法について説明する。   Next, with reference to FIGS. 3-7, the joining apparatus 100 and the adhesion | attachment method which concern on 1st Embodiment of this invention are demonstrated.

<第1実施形態>
図3は、第1実施形態に係る接着方法を用いる際の接合装置100を示す図である。図4は、第1実施形態に係る接着方法のフローチャートである。図5は、複合材料10の表面13の熱可塑性樹脂12を溶融する様子を示す図である。図6は、複合材料10の表面13に接着剤20を配置する様子を示す図である。図7は、接着剤20の複合材料10が設けられる側と反対側の面に他の複合材料30を配置する様子を示す図である。なお、図5〜図7において、レーザーヘッド110、複合材料10、接着剤20、及び複合材料30は簡略化して示す。
<First Embodiment>
FIG. 3 is a diagram illustrating the bonding apparatus 100 when using the bonding method according to the first embodiment. FIG. 4 is a flowchart of the bonding method according to the first embodiment. FIG. 5 is a diagram illustrating a state in which the thermoplastic resin 12 on the surface 13 of the composite material 10 is melted. FIG. 6 is a diagram illustrating a state in which the adhesive 20 is disposed on the surface 13 of the composite material 10. FIG. 7 is a diagram illustrating a state in which another composite material 30 is disposed on the surface of the adhesive 20 opposite to the side on which the composite material 10 is provided. 5-7, the laser head 110, the composite material 10, the adhesive agent 20, and the composite material 30 are simplified and shown.

まず、図3を参照して、接合装置100の構成について説明する。図3において、理解の容易のため、レーザーL、スキャナミラー112、及びレンズ113は実線で示す。図3では、フロントシートである複合材料10に、リアシートである複合材料30を接合する場合を例に挙げて説明する。   First, the configuration of the bonding apparatus 100 will be described with reference to FIG. In FIG. 3, for easy understanding, the laser L, the scanner mirror 112, and the lens 113 are shown by solid lines. In FIG. 3, the case where the composite material 30 which is a rear seat is joined to the composite material 10 which is a front seat will be described as an example.

接合装置100は、レーザーヘッド110と、第1ハンドロボット120と、第2ハンドロボット130と、接着剤塗布ガン140と、第3ハンドロボット150と、を有する。   The joining apparatus 100 includes a laser head 110, a first hand robot 120, a second hand robot 130, an adhesive application gun 140, and a third hand robot 150.

レーザーヘッド110は、複合材料10の表面13にレーザーLを照射することによって、表面13における熱可塑性樹脂12を溶融させる。レーザーヘッド110は、レーザーLが出射される照射部111と、レーザーLを走査するスキャナミラー112と、レーザーLを集光するレンズ113と、を有する。スキャナミラー112は、複合材料10の表面13のうち接着剤20が塗布される位置にレーザーLが照射されるように、不図示の制御部によって制御される。レーザーLは、例えばCOレーザーであるが、これに限定されない。また、レーザーLは、高出力にしやすいという観点から、パルス波であることが好ましい。 The laser head 110 melts the thermoplastic resin 12 on the surface 13 by irradiating the surface 13 of the composite material 10 with the laser L. The laser head 110 includes an irradiation unit 111 from which the laser L is emitted, a scanner mirror 112 that scans the laser L, and a lens 113 that collects the laser L. The scanner mirror 112 is controlled by a control unit (not shown) so that the laser L is applied to a position where the adhesive 20 is applied on the surface 13 of the composite material 10. The laser L is, for example, a CO 2 laser, but is not limited thereto. Moreover, it is preferable that the laser L is a pulse wave from the viewpoint of easily achieving high output.

第1ハンドロボット120は、レーザーヘッド110を把持する。第1ハンドロボット120は、不図示の制御部に制御されることによって、レーザーヘッド110を複合材料10上の所定の位置に移動する。   The first hand robot 120 holds the laser head 110. The first hand robot 120 moves the laser head 110 to a predetermined position on the composite material 10 by being controlled by a control unit (not shown).

第2ハンドロボット130は、複合材料30を把持する。第2ハンドロボット130は、複合材料10の表面13における熱可塑性樹脂12が溶融した後に、不図示の制御部に制御されることによって、複合材料30を複合材料10上に移動する。   The second hand robot 130 holds the composite material 30. The second hand robot 130 moves the composite material 30 onto the composite material 10 by being controlled by a control unit (not shown) after the thermoplastic resin 12 on the surface 13 of the composite material 10 is melted.

接着剤塗布ガン140は、複合材料10の表面13における熱可塑性樹脂12が溶融した複合材料10の表面13に、接着剤20を塗布する。   The adhesive application gun 140 applies the adhesive 20 to the surface 13 of the composite material 10 in which the thermoplastic resin 12 on the surface 13 of the composite material 10 is melted.

第3ハンドロボット150は、接着剤塗布ガン140を把持する。第3ハンドロボット150は、不図示の制御部に制御されることによって、接着剤塗布ガン140を複合材料10上の所定の位置に移動する。   The third hand robot 150 holds the adhesive application gun 140. The third hand robot 150 moves the adhesive application gun 140 to a predetermined position on the composite material 10 by being controlled by a control unit (not shown).

次に、図4のフローチャートを参照して、第1実施形態に係る接着方法を説明する。   Next, the bonding method according to the first embodiment will be described with reference to the flowchart of FIG.

本発明の第1実施形態に係る接着方法は、概説すると、強化基材11に熱可塑性樹脂12を含浸させた複合材料10及び強化基材31に熱可塑性樹脂32を含浸させた複合材料30を、接着剤20を介して接着する方法である。また、接着剤20側の表面13,33における熱可塑性樹脂12,32が溶融された複合材料10,30の、表面13,33における強化基材11A,31Aを、接着剤20内に埋設する接着方法である。以下、第1実施形態に係る接着方法について、詳述する。   In summary, the bonding method according to the first embodiment of the present invention includes a composite material 10 in which a reinforced base material 11 is impregnated with a thermoplastic resin 12 and a composite material 30 in which a reinforced base material 31 is impregnated with a thermoplastic resin 32. This is a method of bonding through the adhesive 20. Further, the bonding material 10 and 30 in which the thermoplastic resins 12 and 32 on the surfaces 13 and 33 on the adhesive 20 side are melted is bonded to the adhesive 20 so that the reinforcing base materials 11A and 31A on the surfaces 13 and 33 are embedded in the adhesive 20. Is the method. Hereinafter, the bonding method according to the first embodiment will be described in detail.

まず、図5に示すように、複合材料10の接着剤20が配置される側の表面13に、レーザーヘッド110の照射部111によってレーザーLを照射して、表面13における熱可塑性樹脂12を溶融する(S01)。レーザーLを表面13に照射する際、スキャナミラー112によってレーザーLを走査して、表面13の適切な位置にレーザーLを照射する。このように、複合材料10の表面13にレーザーLが照射されることによって、表面13における熱可塑性樹脂12が溶融される。   First, as shown in FIG. 5, the surface 13 on the side where the adhesive 20 of the composite material 10 is disposed is irradiated with the laser L by the irradiation unit 111 of the laser head 110 to melt the thermoplastic resin 12 on the surface 13. (S01). When irradiating the surface L with the laser L, the laser L is scanned by the scanner mirror 112, and the laser L is irradiated to an appropriate position on the surface 13. In this manner, the surface L of the composite material 10 is irradiated with the laser L, whereby the thermoplastic resin 12 on the surface 13 is melted.

次に、図6に示すように、表面13における熱可塑性樹脂12が溶融された複合材料10の表面13に接着剤20を塗布する(S02)。接着剤20は、接着剤塗布ガン140によって、塗布される。このように、表面13における熱可塑性樹脂12が溶融された複合材料10の表面13に接着剤20を塗布することによって、表面13における強化基材11Aが、接着剤20内に埋設される。したがって、複合材料10の接着剤20に対する接着性が向上する。   Next, as shown in FIG. 6, the adhesive 20 is applied to the surface 13 of the composite material 10 in which the thermoplastic resin 12 on the surface 13 is melted (S02). The adhesive 20 is applied by an adhesive application gun 140. In this way, the reinforcing base 11 </ b> A on the surface 13 is embedded in the adhesive 20 by applying the adhesive 20 to the surface 13 of the composite material 10 in which the thermoplastic resin 12 on the surface 13 is melted. Therefore, the adhesiveness of the composite material 10 to the adhesive 20 is improved.

次に、図7に示すように、塗布された接着剤20の複合材料10が設けられる側と反対側の面に複合材料30を配置する(S03)。複合材料30は、第2ハンドロボット130によって配置される。複合材料30は、複合材料10と同様に、接着剤20側の表面33において、熱可塑性樹脂32が溶融されていることが好ましい。熱可塑性樹脂32が溶融された状態で、接着剤20上に配置することによって、接着剤20側の表面33における強化基材31Aが、接着剤20内に埋設される。したがって、複合材料30の接着剤20に対する接着性が向上する。なお、接着剤20の上面に配置される部材は、複合材料30に限定されず、金属材料等であってもよい。   Next, as shown in FIG. 7, the composite material 30 is disposed on the surface of the applied adhesive 20 opposite to the side on which the composite material 10 is provided (S03). The composite material 30 is arranged by the second hand robot 130. In the composite material 30, like the composite material 10, the thermoplastic resin 32 is preferably melted on the surface 33 on the adhesive 20 side. By disposing the thermoplastic resin 32 on the adhesive 20 in a melted state, the reinforcing base 31 </ b> A on the surface 33 on the adhesive 20 side is embedded in the adhesive 20. Therefore, the adhesiveness of the composite material 30 to the adhesive 20 is improved. In addition, the member arrange | positioned on the upper surface of the adhesive agent 20 is not limited to the composite material 30, A metal material etc. may be sufficient.

以上の工程によって、複合材料10及び複合材料30は、接着剤20を介して接合され、図1に示す接着構造体1が製造される。   Through the above steps, the composite material 10 and the composite material 30 are joined via the adhesive 20, and the bonded structure 1 shown in FIG. 1 is manufactured.

以上説明したように、本実施形態に係る接着構造体1は、強化基材11に熱可塑性樹脂12を含浸させた複合材料10及び強化基材31に熱可塑性樹脂32を含浸させた複合材料30が、接着剤20を介して接着されてなる。接着構造体1は、接着剤20側の表面13における熱可塑性樹脂12が溶融した複合材料10の、表面13における強化基材11が、接着剤20内に埋設されてなる。この接着構造体1によれば、複合材料10の強化基材11が、接着剤20内に埋設されるため、複合材料10の接着剤20に対する接着性を向上させることができる。また、接着剤20には、先行技術文献の誘電加熱媒体のような別材料が混合されないため、コストの増加や製造工程の煩雑化を抑制することができる。したがって、コストの増加や製造工程の煩雑化を抑制しつつ、強化基材11に熱可塑性樹脂12を含浸させた複合材料10の接着剤20に対する接着性を向上させることのできる接着構造体1を提供することができる。   As described above, the adhesive structure 1 according to this embodiment includes the composite material 10 in which the reinforced base material 11 is impregnated with the thermoplastic resin 12 and the composite material 30 in which the reinforced base material 31 is impregnated with the thermoplastic resin 32. Is bonded via an adhesive 20. The bonding structure 1 is formed by embedding the reinforcing base material 11 on the surface 13 of the composite material 10 in which the thermoplastic resin 12 on the surface 13 on the adhesive 20 side is melted in the adhesive 20. According to the adhesion structure 1, the reinforcing base material 11 of the composite material 10 is embedded in the adhesive 20, so that the adhesion of the composite material 10 to the adhesive 20 can be improved. Moreover, since another material like the dielectric heating medium of a prior art document is not mixed with the adhesive agent 20, the increase in cost and complication of a manufacturing process can be suppressed. Therefore, the adhesive structure 1 capable of improving the adhesion of the composite material 10 in which the reinforced base material 11 is impregnated with the thermoplastic resin 12 to the adhesive 20 is suppressed while suppressing an increase in cost and complication of the manufacturing process. Can be provided.

また、接着構造体1は、強化基材11に熱可塑性樹脂12を含浸させた複合材料10及び強化基材31に熱可塑性樹脂32を含浸させた複合材料30が、接着剤20を介して接着されてなる。このため、複合材料10,30同士を接着することができ、複合材料同士を接合されてなる自動車部品にも適用できる。   Further, the bonded structure 1 includes a composite material 10 in which a reinforced base material 11 is impregnated with a thermoplastic resin 12 and a composite material 30 in which a reinforced base material 31 is impregnated with a thermoplastic resin 32 are bonded via an adhesive 20. Being done. For this reason, the composite materials 10 and 30 can be bonded to each other, and the present invention can also be applied to automobile parts formed by bonding composite materials.

また、以上説明したように、本実施形態に係る接着方法は、強化基材11に熱可塑性樹脂12を含浸させた複合材料10及び強化基材31に熱可塑性樹脂32を含浸させた複合材料30を、接着剤20を介して接着する接着方法である。また、接着剤20側の表面13における熱可塑性樹脂12が溶融された複合材料10の、表面13における強化基材11を、接着剤20内に埋設する。この接着方法によれば、複合材料10の強化基材11が、接着剤20内に埋設されるため、複合材料10の接着剤20に対する接着性を向上させることができる。また、接着剤20には、先行技術文献の誘電加熱媒体のような別材料が混合されないため、コストの増加や製造工程の煩雑化を抑制することができる。したがって、コストの増加や製造工程の煩雑化を抑制しつつ、強化基材11に熱可塑性樹脂12を含浸させた複合材料10の接着剤20に対する接着性を向上させることのできる接着構造体1を提供することができる。   In addition, as described above, the bonding method according to this embodiment includes the composite material 10 in which the reinforced base material 11 is impregnated with the thermoplastic resin 12 and the composite material 30 in which the reinforced base material 31 is impregnated with the thermoplastic resin 32. Is an adhesive method in which the adhesive is bonded via the adhesive 20. Further, the reinforcing base material 11 on the surface 13 of the composite material 10 in which the thermoplastic resin 12 on the surface 13 on the adhesive 20 side is melted is embedded in the adhesive 20. According to this bonding method, since the reinforcing base material 11 of the composite material 10 is embedded in the adhesive 20, the adhesiveness of the composite material 10 to the adhesive 20 can be improved. Moreover, since another material like the dielectric heating medium of a prior art document is not mixed with the adhesive agent 20, the increase in cost and complication of a manufacturing process can be suppressed. Therefore, the adhesive structure 1 capable of improving the adhesion of the composite material 10 in which the reinforced base material 11 is impregnated with the thermoplastic resin 12 to the adhesive 20 is suppressed while suppressing an increase in cost and complication of the manufacturing process. Can be provided.

また、強化基材11に熱可塑性樹脂12を含浸させた複合材料10及び強化基材31に熱可塑性樹脂32を含浸させた複合材料30が、接着剤20を介して接着されてなる。このため、複合材料10,30同士を接着することができ、複合材料同士を接合されてなる自動車部品にも適用できる。   Further, the composite material 10 in which the reinforced base material 11 is impregnated with the thermoplastic resin 12 and the composite material 30 in which the reinforced base material 31 is impregnated with the thermoplastic resin 32 are bonded via the adhesive 20. For this reason, the composite materials 10 and 30 can be bonded to each other, and the present invention can also be applied to automobile parts formed by bonding composite materials.

また、複合材料10の接着剤20側の表面13における熱可塑性樹脂12を溶融させ、熱可塑性樹脂12が溶融された表面13に、接着剤20を配置することによって、強化基材11を接着剤20内に埋設する。この方法によれば、熱可塑性樹脂12が溶融された表面13に、接着剤20を配置するだけで、強化基材11を接着剤20内に埋設することができるため、より容易に強化基材11を接着剤20内に埋設することができる。   Moreover, the thermoplastic resin 12 on the surface 13 on the adhesive 20 side of the composite material 10 is melted, and the adhesive 20 is disposed on the surface 13 on which the thermoplastic resin 12 is melted, whereby the reinforced base material 11 is bonded to the adhesive. It is buried in 20. According to this method, the reinforcing substrate 11 can be embedded in the adhesive 20 simply by disposing the adhesive 20 on the surface 13 on which the thermoplastic resin 12 has been melted. 11 can be embedded in the adhesive 20.

<第2実施形態>
次に、図8〜図12を参照して、本発明の第2実施形態に係る接合装置200及び接着方法について説明する。
Second Embodiment
Next, with reference to FIGS. 8-12, the joining apparatus 200 and the adhesion | attachment method which concern on 2nd Embodiment of this invention are demonstrated.

図8は、第2実施形態に係る接着方法を用いる際の接合装置200を示す図である。図9は、第2実施形態に係る接着方法のフローチャートである。図10は、複合材料10、接着剤20、及び複合材料30の順に積層する様子を示す図である。図11は、複合材料10、接着剤20、及び複合材料30を加熱しつつ、複合材料10及び複合材料30を互いに向かう方向に押圧する様子を示す図である。図12は、複合材料10,30の強化基材11A,31Aが、接着剤20内に埋設する様子を示す図である。   FIG. 8 is a diagram illustrating a bonding apparatus 200 when using the bonding method according to the second embodiment. FIG. 9 is a flowchart of the bonding method according to the second embodiment. FIG. 10 is a diagram illustrating a state in which the composite material 10, the adhesive 20, and the composite material 30 are stacked in this order. FIG. 11 is a diagram illustrating a state in which the composite material 10, the adhesive 20, and the composite material 30 are heated and the composite material 10 and the composite material 30 are pressed toward each other. FIG. 12 is a diagram illustrating a state in which the reinforcing base materials 11 </ b> A and 31 </ b> A of the composite materials 10 and 30 are embedded in the adhesive 20.

まず、図8を参照して、接合装置200の構成について説明する。図8において、複合材料10,30及び接着剤20は簡略化して示す。   First, the configuration of the bonding apparatus 200 will be described with reference to FIG. In FIG. 8, the composite materials 10 and 30 and the adhesive 20 are shown in a simplified manner.

接合装置200は、プレス加工成形型210と、恒温槽220と、第1ハンドロボット120と、第2ハンドロボット130と、接着剤塗布ガン140と、第3ハンドロボット150と、を有する。第1ハンドロボット120、第2ハンドロボット130、接着剤塗布ガン140、及び第3ハンドロボット150は、第1実施形態と同様の構成であるため説明は省略する。   The joining apparatus 200 includes a press working mold 210, a thermostatic chamber 220, a first hand robot 120, a second hand robot 130, an adhesive application gun 140, and a third hand robot 150. Since the first hand robot 120, the second hand robot 130, the adhesive application gun 140, and the third hand robot 150 have the same configuration as that of the first embodiment, the description thereof is omitted.

プレス加工成形型210は、表面13における熱可塑性樹脂12が溶融した複合材料10及び表面33における熱可塑性樹脂32が溶融した複合材料30を、接着剤20を介して互いに向かう方向に押圧する。プレス加工成形型210は、図8に示すように、上型211と、下型212と、を有する。上型211及び下型212は互いに向かう方向に相対的に移動可能に構成される。なお、プレス成形加工型210が設けられず、第2ハンドロボット130が、複合材料30を複合材料10に対して押圧してもよい。   The press working mold 210 presses the composite material 10 in which the thermoplastic resin 12 on the surface 13 is melted and the composite material 30 in which the thermoplastic resin 32 on the surface 33 is melted in the direction toward each other via the adhesive 20. As illustrated in FIG. 8, the press working mold 210 includes an upper mold 211 and a lower mold 212. The upper mold 211 and the lower mold 212 are configured to be relatively movable in the direction toward each other. Note that the press mold 210 may not be provided, and the second hand robot 130 may press the composite material 30 against the composite material 10.

恒温槽220は、内部空間の温度を調整することができる。より具体的には、内部空間の温度を調整することによって、複合材料10の表面13における熱可塑性樹脂12及び複合材料30の表面33における熱可塑性樹脂32を溶融させる(図11参照)。   The thermostat 220 can adjust the temperature of the internal space. More specifically, the thermoplastic resin 12 on the surface 13 of the composite material 10 and the thermoplastic resin 32 on the surface 33 of the composite material 30 are melted by adjusting the temperature of the internal space (see FIG. 11).

次に、図9のフローチャートを参照して、第2実施形態に係る接着方法を説明する。   Next, an adhesion method according to the second embodiment will be described with reference to the flowchart of FIG.

まず、図10に示すように、複合材料10、接着剤20、及び複合材料30の順に積層する(S11)。より具体的には、複合材料10の表面13に、接着剤塗布ガン140によって、接着剤20を塗布し、接着剤20の表面に第3ハンドロボット130によって複合材料30を配置する。   First, as shown in FIG. 10, the composite material 10, the adhesive 20, and the composite material 30 are laminated in this order (S11). More specifically, the adhesive 20 is applied to the surface 13 of the composite material 10 by the adhesive application gun 140, and the composite material 30 is placed on the surface of the adhesive 20 by the third hand robot 130.

次に、図11に示すように、恒温槽220の温度を制御して、複合材料10、接着剤20、及び複合材料30を加熱しつつ、プレス成型加工型210によって、複合材料10及び複合材料30を互いに向かう方向に押圧する(S12)。恒温槽220の内部空間における温度は、例えば、170度であるが、特に限定されない。このとき、接着剤20が増粘してきたタイミングで、熱可塑性樹脂12の融点まで加熱し、同時に押圧することが好ましい。この結果、複合材料10,30の表面13,33における熱可塑性樹脂12,32が溶融し、図12に示すように、表面13,33における強化基材11A,31Aが接着剤20内に埋設される。したがって、複合材料10,30の接着剤20に対する接着性が向上する。   Next, as shown in FIG. 11, the composite material 10 and the composite material are controlled by the press mold 210 while heating the composite material 10, the adhesive 20, and the composite material 30 by controlling the temperature of the thermostatic chamber 220. 30 are pressed in the direction toward each other (S12). Although the temperature in the internal space of the thermostat 220 is 170 degree | times, for example, it is not specifically limited. At this time, it is preferable that the adhesive 20 is heated to the melting point of the thermoplastic resin 12 at the timing when the viscosity of the adhesive 20 is increased, and pressed simultaneously. As a result, the thermoplastic resins 12 and 32 on the surfaces 13 and 33 of the composite materials 10 and 30 are melted, and the reinforcing base materials 11A and 31A on the surfaces 13 and 33 are embedded in the adhesive 20 as shown in FIG. The Therefore, the adhesiveness of the composite materials 10 and 30 to the adhesive 20 is improved.

以上、説明したように、第2実施形態に係る接着方法は、複合材料10、接着剤20、及び複合材料30の順に積層し、複合材料10、接着剤20、及び複合材料30を加熱しつつ、複合材料10及び複合材料30を互いに向かう方向に押圧する。これによって、強化基材11A,31Aを接着剤20内に埋設する。この接着方法によれば、複合材料10及び複合材料30を互いに向かう方向に押圧することによって、複合材料10の表面13における強化基材11A及び複合材料30の表面33における強化基材31Aを、一度に接着剤20内に埋設することができる。したがって、容易に複合材料10,30同士を接着することができる。   As described above, in the bonding method according to the second embodiment, the composite material 10, the adhesive 20, and the composite material 30 are stacked in this order, and the composite material 10, the adhesive 20, and the composite material 30 are heated. The composite material 10 and the composite material 30 are pressed toward each other. In this way, the reinforcing base materials 11A and 31A are embedded in the adhesive 20. According to this bonding method, the reinforced base material 11A on the surface 13 of the composite material 10 and the reinforced base material 31A on the surface 33 of the composite material 30 are once pressed by pressing the composite material 10 and the composite material 30 in the direction toward each other. It can be embedded in the adhesive 20. Therefore, the composite materials 10 and 30 can be easily bonded to each other.

以下、上述した実施形態の改変例を例示する。   Hereinafter, modifications of the above-described embodiment will be exemplified.

上述した第1実施形態では、複合材料10の表面13における熱可塑性樹脂12を溶融させる手段として、レーザーLを挙げたが、これに限定されず、赤外線ランプや誘導加熱などであってもよい。さらに上述の加熱による溶融に限定されず、複合材料10の表面13に有機溶剤を塗布することによって化学的に溶融してもよい。   In 1st Embodiment mentioned above, although the laser L was mentioned as a means to fuse the thermoplastic resin 12 in the surface 13 of the composite material 10, it is not limited to this, An infrared lamp, induction heating, etc. may be sufficient. Furthermore, it is not limited to the above-mentioned melting by heating, and may be chemically melted by applying an organic solvent to the surface 13 of the composite material 10.

有機溶剤としては、例えば、二硫化炭素、四塩化炭素、グリセリン、エチレングリコール、ギ酸、氷酢酸、シュウ酸、ベンゼン、トルエン、キシレン、n−ヘキサン、n−ヘプタン、メタノール、エタノール、プロパノール、ブタノール、シクロヘキサン、クロロベンゼン、ピリジン、アニリン、デカリン、クロロホルム、エチルエーテル、酢酸エチル、アセトン、石油ベンジン、石油エーテル、メチルエチルケトンなどが挙げられる。   Examples of the organic solvent include carbon disulfide, carbon tetrachloride, glycerin, ethylene glycol, formic acid, glacial acetic acid, oxalic acid, benzene, toluene, xylene, n-hexane, n-heptane, methanol, ethanol, propanol, butanol, Examples include cyclohexane, chlorobenzene, pyridine, aniline, decalin, chloroform, ethyl ether, ethyl acetate, acetone, petroleum benzine, petroleum ether, and methyl ethyl ketone.

また、上述した第2実施形態では、恒温槽220によって、複合材料10、接着剤20、及び複合材料30を全体的に加熱した。しかしながら、プレス加工成形型210が熱プレス可能な構成からなり熱プレスによって加熱及び押圧を行ってもよい。この方法によれば、第2実施形態と比較して、複合材料10,30を全体的に加熱することを防止でき、部分的に加熱することができるため、複合材料10,30の変形を抑制できる。   Moreover, in 2nd Embodiment mentioned above, the composite material 10, the adhesive agent 20, and the composite material 30 were heated entirely by the thermostat 220. FIG. However, the press working mold 210 may be configured to be hot pressed and may be heated and pressed by hot pressing. According to this method, compared to the second embodiment, the composite materials 10 and 30 can be prevented from being heated entirely and partially heated, so that deformation of the composite materials 10 and 30 is suppressed. it can.

また、上述した第2実施形態では、図11に示すように、複合材料10,30の表面13,33に、接着剤20が一様に配置された。しかしながら、図13に示すように、複合材料10,30の表面13,33に、接着剤20が離散的に配置されてもよい。この構成によれば、複合材料10及び複合材料30を互いに向かう方向に押圧する際に、接着剤20が一様に配置される場合と比較して接着剤20が配置される箇所が高圧となる。このため、強化繊維11,31が接着剤20に対してより深く埋設することとなり、複合材料10及び複合材料30の接着性がより向上する。   Moreover, in 2nd Embodiment mentioned above, as shown in FIG. 11, the adhesive agent 20 was arrange | positioned uniformly on the surfaces 13 and 33 of the composite materials 10 and 30. As shown in FIG. However, as shown in FIG. 13, the adhesive 20 may be discretely disposed on the surfaces 13 and 33 of the composite materials 10 and 30. According to this configuration, when the composite material 10 and the composite material 30 are pressed in the direction toward each other, the place where the adhesive 20 is disposed is higher than the case where the adhesive 20 is disposed uniformly. . For this reason, the reinforcing fibers 11 and 31 are buried deeper into the adhesive 20, and the adhesiveness of the composite material 10 and the composite material 30 is further improved.

<実施例>
以下、実施例を挙げて本発明を具体的に説明するが、本発明はこれらに限定されるものではない。
<Example>
EXAMPLES Hereinafter, the present invention will be specifically described with reference to examples, but the present invention is not limited thereto.

一般的に接着しにくいポリプロピレン(熱可塑性樹脂12)をマトリクスとするカーボン繊維強化プラスチック(強化基材11)において、汎用的なエポキシ系の接着剤(接着剤20)を使用して複合材料10,30同士を接着し、せん断試験を行った。その結果、接着強度は2MPaと低く、その破壊モードは、図14に示すように、接着剤20と複合材料10の界面剥離であった。   In a carbon fiber reinforced plastic (reinforced base material 11), which is generally made of polypropylene (thermoplastic resin 12) that is difficult to bond, a composite material 10, using a general-purpose epoxy adhesive (adhesive 20). 30 were bonded together and the shear test was done. As a result, the adhesive strength was as low as 2 MPa, and the failure mode was interface peeling between the adhesive 20 and the composite material 10 as shown in FIG.

これに対して、上述した第2実施形態において、恒温槽220の温度を170度にして接着した接着構造体1に対して、同様にせん断試験を行った。その結果、接着強度は11.7MPaと高くなり、その破壊モードは、図15に示すように、接着剤20内における母材破断であった。   On the other hand, in the second embodiment described above, a shear test was similarly performed on the bonded structure 1 bonded with the temperature of the thermostat 220 set at 170 degrees. As a result, the adhesive strength was as high as 11.7 MPa, and the fracture mode was a base material fracture in the adhesive 20 as shown in FIG.

この結果、複合材料10,30の表面13,33における強化基材11A,31Aを接着剤20内に埋設することによって、複合材料10,30の接着剤20に対する接着性が向上した。さらに、複合材料10,30同士の接着強度が向上した。   As a result, the adhesiveness of the composite materials 10 and 30 to the adhesive 20 was improved by embedding the reinforcing base materials 11A and 31A on the surfaces 13 and 33 of the composite materials 10 and 30 in the adhesive 20. Furthermore, the adhesive strength between the composite materials 10 and 30 was improved.

1 接着構造体、
10 複合材料、
11,31 強化基材、
11A,31A 表面における強化基材、
12,32 熱可塑性樹脂、
13,33 表面、
20 接着剤、
30 複合材料(被接着部材)。
1 Adhesive structure,
10 composite materials,
11, 31 reinforced base material,
11A, 31A Reinforced substrate on the surface,
12, 32 thermoplastic resin,
13,33 surface,
20 Adhesive,
30 Composite material (bonded member).

Claims (7)

強化基材に熱可塑性樹脂を含浸させた複合材料及び被接着部材が、接着剤を介して接着されてなる接着構造体であって、
前記接着剤側の表面における前記熱可塑性樹脂が溶融した前記複合材料の、前記表面における前記強化基材が、前記接着剤内に埋設されてなる接着構造体。
A composite material in which a reinforced base material is impregnated with a thermoplastic resin and a member to be bonded are bonded via an adhesive,
An adhesive structure in which the reinforcing base material on the surface of the composite material in which the thermoplastic resin on the surface on the adhesive side is melted is embedded in the adhesive.
前記被接着部材は、強化基材に熱可塑性樹脂を含浸させた複合材料である請求項1に記載の接着構造体。   The bonded structure according to claim 1, wherein the member to be bonded is a composite material in which a reinforced base material is impregnated with a thermoplastic resin. 強化基材に熱可塑性樹脂を含浸させた複合材料及び被接着部材を、接着剤を介して接着する接着方法であって、
前記接着剤側の表面における前記熱可塑性樹脂が溶融された前記複合材料の、前記表面における前記強化基材を、前記接着剤内に埋設する接着方法。
A bonding method in which a composite material in which a reinforced substrate is impregnated with a thermoplastic resin and a member to be bonded are bonded via an adhesive,
A bonding method in which the reinforcing base material on the surface of the composite material in which the thermoplastic resin on the surface on the adhesive side is melted is embedded in the adhesive.
前記被接着部材は、強化基材に熱可塑性樹脂を含浸させた複合材料である請求項3に記載の接着方法。   The bonding method according to claim 3, wherein the member to be bonded is a composite material in which a reinforced base material is impregnated with a thermoplastic resin. 前記複合材料の前記接着剤側の表面における前記熱可塑性樹脂を溶融させ、
前記熱可塑性樹脂が溶融された前記表面に、前記接着剤を配置することによって、前記強化基材を前記接着剤内に埋設する請求項3または4に記載の接着方法。
Melting the thermoplastic resin on the adhesive-side surface of the composite material;
The bonding method according to claim 3 or 4, wherein the reinforcing base is embedded in the adhesive by disposing the adhesive on the surface where the thermoplastic resin is melted.
前記複合材料、前記接着剤、及び前記被接着部材の順に積層し、
少なくとも前記複合材料の前記接着剤側の表面を加熱しつつ、前記複合材料及び前記被接着部材を互いに向かう方向に押圧することによって、前記強化基材を前記接着剤内に埋設する請求項3または4に記載の接着方法。
Laminate in order of the composite material, the adhesive, and the adherend,
The reinforced substrate is embedded in the adhesive by pressing the composite material and the member to be bonded in a direction toward each other while heating at least the surface of the composite material on the adhesive side. 4. The bonding method according to 4.
前記接着剤を、前記複合材料の表面に離散的に配置する請求項6に記載の接着方法。   The adhesion method according to claim 6, wherein the adhesive is discretely disposed on a surface of the composite material.
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