JP7187378B2 - Adhesive member, method for forming adhesive member, and method for forming adhesive layer - Google Patents

Adhesive member, method for forming adhesive member, and method for forming adhesive layer Download PDF

Info

Publication number
JP7187378B2
JP7187378B2 JP2019082173A JP2019082173A JP7187378B2 JP 7187378 B2 JP7187378 B2 JP 7187378B2 JP 2019082173 A JP2019082173 A JP 2019082173A JP 2019082173 A JP2019082173 A JP 2019082173A JP 7187378 B2 JP7187378 B2 JP 7187378B2
Authority
JP
Japan
Prior art keywords
adhesive layer
crack growth
adhesive
crack
growth suppression
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
JP2019082173A
Other languages
Japanese (ja)
Other versions
JP2020180626A (en
Inventor
一輝 大橋
清嘉 ▲高▼木
直昭 藤原
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Heavy Industries Ltd
Original Assignee
Mitsubishi Heavy Industries Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Mitsubishi Heavy Industries Ltd filed Critical Mitsubishi Heavy Industries Ltd
Priority to JP2019082173A priority Critical patent/JP7187378B2/en
Publication of JP2020180626A publication Critical patent/JP2020180626A/en
Application granted granted Critical
Publication of JP7187378B2 publication Critical patent/JP7187378B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Description

本発明は、接着部材、接着部材の形成方法および接着層の形成方法に関する。 The present invention relates to an adhesive member, a method for forming an adhesive member, and a method for forming an adhesive layer.

従来、2つの部材を接着層によって接着して接着部材を形成することが知られている。例えば、特許文献1には、第1部材と第2部材との間に、第1繊維部および第2繊維部を配置し、第1繊維部と第2繊維部との間に接着部を設けて接着する接着構造が開示されている。この接着構造では、第1部材と第2部材との間で、第1繊維部および第2繊維部が面外方向に延在するように配置されている。 Conventionally, it is known to bond two members together with an adhesive layer to form an adhesive member. For example, in Patent Document 1, a first fiber portion and a second fiber portion are arranged between a first member and a second member, and a bonding portion is provided between the first fiber portion and the second fiber portion. An adhesive structure is disclosed that adheres to In this bonding structure, the first fiber portion and the second fiber portion are arranged to extend in the out-of-plane direction between the first member and the second member.

国際公開第2016/129570号WO2016/129570

第1部材および第2部材と接着層(接着部)とを接着する接着構造では、荷重が作用したとき、接着層にき裂(特に第1部材および第2部材と接着層との界面における剥離)が発生する可能性がある。上記特許文献1に記載の接着構造は、第1部材と第2部材との間で第1繊維部および第2繊維部が面外方向に延在することで、接着部に発生するき裂の進展を第1繊維部および第2繊維部で抑制している。しかしながら、接着層において繊維を面外方向に延在するように配置した場合、面内方向への引張荷重に対する耐性が低下する等、接着部材の面内特性に影響が生じる可能性がある。 In an adhesive structure in which the first member and the second member are bonded to the adhesive layer (adhesive portion), when a load is applied, the adhesive layer cracks (particularly, peeling at the interface between the first member and the second member and the adhesive layer). ) may occur. In the bonded structure described in Patent Document 1, the first fiber portion and the second fiber portion extend in the out-of-plane direction between the first member and the second member, thereby preventing cracks occurring in the bonded portion. The extension is suppressed by the first fiber portion and the second fiber portion. However, if the fibers are arranged to extend in the out-of-plane direction in the adhesive layer, the in-plane properties of the adhesive member may be affected, such as a decrease in resistance to tensile loads in the in-plane direction.

本発明は、上記に鑑みてなされたものであって、接着部材の面内特性に影響を与えないようにしながら、接着層で発生するき裂の進展を抑制することを目的とする。 SUMMARY OF THE INVENTION The present invention has been made in view of the above, and an object of the present invention is to suppress the propagation of cracks occurring in the adhesive layer without affecting the in-plane characteristics of the adhesive member.

上述した課題を解決し、目的を達成するために、本発明は、第1部材と、第2部材と、前記第1部材と前記第2部材とを接着する接着剤を含む接着層と、前記接着層内に配置され、前記接着層内で面内方向に向かうき裂の進展を抑制するき裂進展抑制部材と、を備え、前記き裂進展抑制部材は、前記第1部材側から前記第2部材側にかけて前記面内方向に凸形状を呈する進展抑制部を有し、前記接着層との界面の接着強度が前記接着層と前記第1部材および前記第2部材との界面の接着強度よりも弱いことを特徴とする。 In order to solve the above-described problems and achieve the object, the present invention provides a first member, a second member, an adhesive layer containing an adhesive for bonding the first member and the second member, and a crack growth suppression member disposed in the adhesive layer and configured to suppress propagation of a crack in the in-plane direction in the adhesive layer, wherein the crack growth suppression member extends from the first member side to the second crack growth suppression member; It has a progress suppressing portion that exhibits a convex shape in the in-plane direction toward the two member side, and the adhesive strength at the interface with the adhesive layer is greater than the adhesive strength at the interface between the adhesive layer and the first member and the second member. is also weak.

この構成により、接着層とき裂進展抑制部材との界面の接着強度が、接着層と第1部材および第2部材との界面の接着強度よりも弱いため、接着層で発生して面内方向に向かうき裂を接着層とき裂進展抑制部材との界面へと誘導することができる。そして、き裂進展抑制部材の進展抑制部へと誘導されたき裂は、進展抑制部の凸形状によって面外方向に進展することになる。その結果、き裂の面内方向への進展抵抗が大きくなり、き裂の進展が抑制される。すなわち、接着層内において繊維を面外方向に延在するように配置することなく、き裂の進展を抑制することが可能となる。したがって、本発明によれば、接着部材の面内特性に影響を与えないようにしながら、接着層で発生するき裂の進展を抑制することが可能となる。 With this configuration, the adhesive strength at the interface between the adhesive layer and the crack growth suppressing member is weaker than the adhesive strength at the interface between the adhesive layer and the first member and the second member. A directed crack can be induced to the interface between the adhesive layer and the crack growth restraint member. Then, the crack guided to the growth restraining portion of the crack growth restraining member propagates in the out-of-plane direction due to the convex shape of the growth restraining portion. As a result, the crack propagation resistance in the in-plane direction is increased, and the crack propagation is suppressed. In other words, it is possible to suppress the propagation of cracks without arranging the fibers in the adhesive layer so as to extend in the out-of-plane direction. Therefore, according to the present invention, it is possible to suppress the propagation of cracks generated in the adhesive layer without affecting the in-plane properties of the adhesive member.

また、前記進展抑制部は、前記凸形状を呈する湾曲部であることが好ましい。この構成により、進展抑制部によってき裂をスムーズに誘導しつつ、き裂の面内方向への進展抵抗を増加させることができる。 Moreover, it is preferable that the progress suppressing portion is a curved portion having the convex shape. With this configuration, it is possible to increase the resistance to crack propagation in the in-plane direction while smoothly inducing the crack by the propagation suppressing portion.

また、前記き裂進展抑制部材は、前記進展抑制部の端部から前記面内方向に沿って延びる誘導部をさらに有することが好ましい。この構成により、接着層で発生して面内方向に向かうき裂を誘導部へとより確実に誘導させることができる。 Moreover, it is preferable that the crack growth suppression member further includes a guiding portion extending along the in-plane direction from an end portion of the crack growth suppression portion. With this configuration, a crack occurring in the adhesive layer and extending in the in-plane direction can be more reliably guided to the guiding portion.

また、前記き裂進展抑制部材は、前記面内方向に沿って複数配置されることが好ましい。この構成により、複数のき裂進展抑制部材をより広い範囲に配置することができるため、接着層で面内方向へと向かうき裂の進展を、より確実に抑制することができる。 Further, it is preferable that a plurality of crack growth suppression members be arranged along the in-plane direction. With this configuration, it is possible to arrange a plurality of crack growth suppression members over a wider range, so that it is possible to more reliably suppress the propagation of cracks in the in-plane direction in the adhesive layer.

また、隣り合う前記き裂進展抑制部材の少なくとも一部は、前記進展抑制部の前記凸形状が互いに反対方向を向いて配置されることが好ましい。この構成により、互いに反対方向を向いて配置されるき裂進展抑制部材により、き裂が2方向のいずれに向かう場合でも、その進展をより確実に抑制することができる。 Moreover, it is preferable that at least some of the adjacent crack growth suppression members are arranged such that the convex shapes of the crack growth suppression portions face opposite directions to each other. With this configuration, the crack propagation suppression members arranged facing opposite directions can more reliably suppress the propagation of the crack regardless of which of the two directions the crack faces.

また、前記き裂進展抑制部材は、前記進展抑制部が環状に連続して形成されることが好ましい。この構成により、接着層内において、き裂が面内方向のいずれに進展するものであっても、その進展をより確実に抑制することができる。 Further, it is preferable that the crack growth suppression member is formed such that the crack growth suppression portion is continuously formed in an annular shape. With this configuration, even if a crack propagates in any in-plane direction in the adhesive layer, the propagation can be more reliably suppressed.

また、前記き裂進展抑制部材は、連結部を介して複数が連結されていることが好ましい。この構成により、複数のき裂進展抑制部材を一つの部材として取り扱うことができる。また、例えば第1部材、第2部材および接着層を接着する際に接着層内に含まれる樹脂が軟化しても、複数のき裂進展抑制部材の間に連結部が存在することで、き裂進展抑制部材が接着層内で流動することを抑制することができる。 Moreover, it is preferable that a plurality of the crack growth suppression members are connected via a connecting portion. With this configuration, a plurality of crack growth suppression members can be handled as one member. Further, for example, even if the resin contained in the adhesive layer is softened when the first member, the second member and the adhesive layer are adhered, the existence of the connecting portion between the plurality of crack growth suppressing members prevents cracks from forming. It is possible to suppress the crack growth suppression member from flowing within the adhesive layer.

上述した課題を解決し、目的を達成するために、本発明は、第1部材を準備する第1部材準備ステップと、第2部材を準備する第2部材準備ステップと、前記第1部材と前記第2部材とを接着剤を含む接着層により接着する接着ステップと、を備え、前記接着層内には、前記接着層内で面内方向に向かうき裂の進展を抑制するき裂進展抑制部材が配置されており、前記き裂進展抑制部材は、前記第1部材側から前記第2部材側にかけて前記面内方向に凸形状を呈する進展抑制部を有し、前記接着層との界面の接着強度が前記接着層と前記第1部材および前記第2部材との界面の接着強度よりも弱いことを特徴とする。 In order to solve the above-described problems and achieve the object, the present invention provides a first member preparing step of preparing a first member, a second member preparing step of preparing a second member, the first member and the and a bonding step of bonding the second member with an adhesive layer containing an adhesive, wherein the adhesive layer includes a crack growth suppression member that suppresses the propagation of a crack in the in-plane direction within the adhesive layer. is arranged, and the crack growth suppression member has a growth suppression portion having a convex shape in the in-plane direction from the first member side to the second member side, and the interface adhesion with the adhesive layer The adhesive strength is weaker than the adhesive strength of the interface between the adhesive layer and the first member and the second member.

この構成により、接着層とき裂進展抑制部材との界面の接着強度が、接着層と第1部材および第2部材との界面の接着強度よりも弱いため、接着層で発生して面内方向に向かうき裂を接着層とき裂進展抑制部材との界面へと誘導することができる。そして、き裂進展抑制部材の進展抑制部へと誘導されたき裂は、進展抑制部の凸形状によって面外方向に進展することになる。その結果、き裂の面内方向への進展抵抗が大きくなり、き裂の進展が抑制される。すなわち、接着層内において繊維を面外方向に延在するように配置することなく、き裂の進展を抑制することが可能となる。したがって、本発明によれば、接着部材の面内特性に影響を与えないようにしながら、接着層で発生するき裂の進展を抑制することが可能となる。 With this configuration, the adhesive strength at the interface between the adhesive layer and the crack growth suppressing member is weaker than the adhesive strength at the interface between the adhesive layer and the first member and the second member. A directed crack can be induced to the interface between the adhesive layer and the crack growth restraint member. Then, the crack guided to the growth restraining portion of the crack growth restraining member propagates in the out-of-plane direction due to the convex shape of the growth restraining portion. As a result, the crack propagation resistance in the in-plane direction is increased, and the crack propagation is suppressed. In other words, it is possible to suppress the propagation of cracks without arranging the fibers in the adhesive layer so as to extend in the out-of-plane direction. Therefore, according to the present invention, it is possible to suppress the propagation of cracks generated in the adhesive layer without affecting the in-plane properties of the adhesive member.

上述した課題を解決し、目的を達成するために、本発明は、第1部材と第2部材とを接着する接着剤を含む接着層を形成する接着層の形成方法であって、基材を複数の切り込み線に沿って切り込み、複数の折り曲げ線に沿って折り曲げて、前記接着層内で面内方向に向かうき裂の進展を抑制するき裂進展抑制部材を、連結部を介して複数連結して形成し、前記き裂進展抑制部材に前記接着剤を含む樹脂を含浸して前記接着層を形成し、前記き裂進展抑制部材は、前記第1部材側から前記第2部材側にかけて面内方向に凸形状を呈する進展抑制部を有し、前記接着層との界面の接着強度が前記接着層と前記第1部材および前記第2部材との界面の接着強度よりも弱いことを特徴とする。 In order to solve the above-described problems and achieve the object, the present invention provides a method for forming an adhesive layer for forming an adhesive layer containing an adhesive for bonding a first member and a second member, comprising: A plurality of crack growth suppression members are connected via connecting portions by cutting along a plurality of cut lines and bending along a plurality of folding lines to suppress the propagation of cracks in the in-plane direction in the adhesive layer. The crack growth suppression member is impregnated with a resin containing the adhesive to form the adhesive layer, and the crack growth suppression member extends from the first member side to the second member side. It has an inwardly convex expansion suppressing portion, and the adhesive strength of the interface with the adhesive layer is weaker than the adhesive strength of the interfaces between the adhesive layer and the first member and the second member. do.

この構成により、複数が連結されたき裂進展抑制部材を含む接着層を容易に形成することができる。また、複数のき裂進展抑制部材を一つの部材として取り扱うことができる。また、例えば第1部材、第2部材および接着層を接着する際に接着層内に含まれる樹脂が軟化しても、複数のき裂進展抑制部材の間に連結部が存在することで、き裂進展抑制部材が接着層内で流動することを抑制することができる。 With this configuration, it is possible to easily form an adhesive layer including a plurality of connected crack growth suppression members. Also, a plurality of crack growth suppression members can be handled as one member. Further, for example, even if the resin contained in the adhesive layer is softened when the first member, the second member and the adhesive layer are adhered, the existence of the connecting portion between the plurality of crack growth suppressing members prevents cracks from forming. It is possible to suppress the crack growth suppression member from flowing within the adhesive layer.

上述した課題を解決し、目的を達成するために、本発明は、第1部材と第2部材とを接着する接着剤を含む接着層を形成する接着層の形成方法であって、前記接着層内で面内方向に向かうき裂の進展を抑制するき裂進展抑制部材の周囲に、前記接着剤を含む複数のフィルム状部材を接着して前記接着層を形成し、前記き裂進展抑制部材は、前記第1部材側から前記第2部材側にかけて前記面内方向に凸形状を呈する進展抑制部を有し、前記接着層との界面の接着強度が前記接着層と前記第1部材および前記第2部材との界面の接着強度よりも弱いことを特徴とする。 In order to solve the above-described problems and achieve the object, the present invention provides a method for forming an adhesive layer for forming an adhesive layer containing an adhesive for bonding a first member and a second member, wherein the adhesive layer A plurality of film-like members containing the adhesive are adhered around the crack growth suppression member that suppresses the propagation of a crack in the in-plane direction to form the adhesive layer, and the crack growth suppression member has a progress suppressing portion that exhibits a convex shape in the in-plane direction from the first member side to the second member side, and the adhesive strength at the interface with the adhesive layer is the adhesive layer, the first member, and the It is characterized by being weaker than the adhesive strength of the interface with the second member.

この構成により、き裂進展抑制部材を含む接着層を容易に形成することができる。 With this configuration, it is possible to easily form the adhesive layer including the crack growth suppressing member.

図1は、実施形態にかかる接着部材としての複合材を示す断面図である。FIG. 1 is a cross-sectional view showing a composite material as an adhesive member according to an embodiment. 図2は、実施形態にかかる接着部材としての複合材の要部を拡大して示す拡大断面図である。FIG. 2 is an enlarged cross-sectional view showing an enlarged main part of a composite material as an adhesive member according to the embodiment. 図3は、実施形態の変形例にかかる複合材を示す断面図である。FIG. 3 is a cross-sectional view showing a composite material according to a modification of the embodiment; 図4は、第1の変形例にかかるき裂進展抑制部材を含む複合材を示す断面図である。FIG. 4 is a cross-sectional view showing a composite material including a crack growth suppression member according to a first modification. 図5は、第1の変形例にかかるき裂進展抑制部材を含む複合材を示す断面図である。FIG. 5 is a cross-sectional view showing a composite material including a crack growth suppression member according to a first modification. 図6は、第2の変形例にかかるき裂進展抑制部材を示す正面図である。FIG. 6 is a front view showing a crack growth suppression member according to a second modification. 図7は、図6のA-A線に沿った端面図である。7 is an end view along line AA of FIG. 6. FIG. 図8は、第2の変形例にかかるき裂進展抑制部材の他の構成例を示す断面図である。FIG. 8 is a cross-sectional view showing another configuration example of the crack growth suppression member according to the second modification. 図9は、第3の変形例にかかるき裂進展抑制部材を示す断面図である。FIG. 9 is a cross-sectional view showing a crack growth suppression member according to a third modification. 図10は、第4の変形例にかかるき裂進展抑制部材を示す説明図である。FIG. 10 is an explanatory diagram showing a crack growth suppression member according to a fourth modification. 図11は、き裂進展抑制部材の基材を示す説明図である。FIG. 11 is an explanatory diagram showing the base material of the crack growth suppression member. 図12は、き裂進展抑制部材の周囲に樹脂フィルムを配置する様子を示す説明図である。FIG. 12 is an explanatory diagram showing how a resin film is arranged around the crack growth suppression member.

以下に、本発明にかかる接着部材、接着部材の形成方法および接着層の形成方法の実施形態を図面に基づいて詳細に説明する。なお、この実施形態によりこの発明が限定されるものではない。 BEST MODE FOR CARRYING OUT THE INVENTION Embodiments of an adhesive member, a method for forming an adhesive member, and a method for forming an adhesive layer according to the present invention will be described below in detail with reference to the drawings. In addition, this invention is not limited by this embodiment.

図1は、実施形態にかかる接着部材としての複合材を示す断面図である。実施形態にかかる接着部材としての複合材100は、例えば航空機といった種々の分野において用いられる複合材である。複合材100は、第1部材としての第1複合部材10Aと、第2部材としての第2複合部材10Bと、接着層20を備えている。第1複合部材10Aと第2複合部材10Bとは、接着層20を介して接着される。以下の説明では、第1複合部材10A、第2複合部材10Bおよび接着層20が並ぶ方向(図1に示す上下方向)を複合材100の「面外方向Z」と称し、面外方向Zと直交する方向(図1に示す左右方向)を複合材100の「第1面内方向X」と称し、第1面内方向Xおよび面外方向Zと直交する方向を複合材100の「第2面内方向Y」と称する。 FIG. 1 is a cross-sectional view showing a composite material as an adhesive member according to an embodiment. A composite material 100 as an adhesive member according to the embodiment is a composite material used in various fields such as aircraft. The composite material 100 includes a first composite member 10A as a first member, a second composite member 10B as a second member, and an adhesive layer 20. As shown in FIG. The first composite member 10A and the second composite member 10B are adhered via the adhesive layer 20 . In the following description, the direction in which the first composite member 10A, the second composite member 10B, and the adhesive layer 20 are arranged (vertical direction shown in FIG. 1) is referred to as the "out-of-plane direction Z" of the composite material 100. The direction orthogonal to the composite material 100 (the left-right direction shown in FIG. 1) is called the “first in-plane direction X” of the composite material 100, and the direction orthogonal to the first in-plane direction X and the out-of-plane direction Z is the “second direction” of the composite material 100. In-plane direction Y”.

第1複合部材10Aおよび第2複合部材10Bは、例えば炭素繊維といった強化繊維に樹脂を含浸した複合材料層11を複数積層した積層体である。接着層20は、第1複合部材10Aと第2複合部材10Bとの間に配置され、第1複合部材10Aと第2複合部材10Bとを接着する。接着層20は、例えば接着剤を含む樹脂材料により形成される。 The first composite member 10A and the second composite member 10B are laminates obtained by laminating a plurality of composite material layers 11 in which reinforcing fibers such as carbon fibers are impregnated with resin. The adhesive layer 20 is arranged between the first composite member 10A and the second composite member 10B, and adheres the first composite member 10A and the second composite member 10B. The adhesive layer 20 is made of, for example, a resin material containing an adhesive.

実施形態にかかる複合材100は、第1複合部材10Aを準備する第1部材準備ステップと、第2複合部材10Bを準備する第2部材準備ステップと、第1複合部材10Aと第2複合部材10Bとを接着層20で接着する接着ステップとを実行することで形成される。本実施形態では、第1部材準備ステップ、第2部材準備ステップにおいて、複合材料層11を複数積層し、樹脂を硬化させた第1複合部材10A、第2複合部材20Bを準備する。そして、接着ステップにおいて、樹脂硬化後の第1複合部材10Aと第2複合部材20Bとの間に接着層20を配置して、第1複合材部10Aと第2複合部材10Bとを接着層20で接着する。なお、第1部材準備ステップ、第2部材準備ステップで樹脂硬化前(プリプレグの状態)の第1複合部材10Aおよび第2複合部材10Bを準備し、接着ステップで第1複合部材10Aおよび第2複合部材10Bの間に接着層20を配置して、加熱を伴いながら接着させることで、接着と同時に第1複合部材10Aおよび第2複合部材10Bを硬化させてもよい。 The composite material 100 according to the embodiment includes a first member preparation step of preparing the first composite member 10A, a second member preparation step of preparing the second composite member 10B, the first composite member 10A and the second composite member 10B are formed by performing a bonding step of bonding and bonding with the bonding layer 20 . In this embodiment, in the first member preparing step and the second member preparing step, a first composite member 10A and a second composite member 20B are prepared by laminating a plurality of composite material layers 11 and curing the resin. Then, in the bonding step, the adhesive layer 20 is arranged between the first composite member 10A and the second composite member 20B after the resin has been cured, and the first composite member 10A and the second composite member 10B are bonded together by the adhesive layer 20. Glue with Note that the first composite member 10A and the second composite member 10B before resin curing (prepreg state) are prepared in the first member preparation step and the second member preparation step, and the first composite member 10A and the second composite member 10B are prepared in the bonding step. The first composite member 10A and the second composite member 10B may be cured at the same time as the bonding by disposing the adhesive layer 20 between the members 10B and bonding the members 10B together with heating.

ここで、複合材100に対して荷重が作用すると、接着層20内において、第1面内方向Xまたは第2面内方向Yへと向かうき裂が発生することがある。き裂は、特に第1複合部材10Aまたは第2複合部材10Bと接着層20との界面の剥離として発生しやすい。そのため、実施形態にかかる複合材100は、接着層20で発生したき裂の進展を抑制するために、上記構成に加えて、き裂進展抑制部材30を備えている。 Here, when a load acts on the composite material 100 , cracks in the first in-plane direction X or the second in-plane direction Y may occur in the adhesive layer 20 . Cracks are particularly likely to occur as delamination at the interface between the first composite member 10A or the second composite member 10B and the adhesive layer 20 . Therefore, the composite material 100 according to the embodiment includes a crack propagation suppression member 30 in addition to the above configuration in order to suppress propagation of cracks generated in the adhesive layer 20 .

き裂進展抑制部材30は、例えば金属箔により形成され、接着層20内に配置される。き裂進展抑制部材30は、複合材100において、き裂が発生しやすく、き裂の進展を停止させるべき箇所に配置される。複合材100において、き裂が発生しやすく、き裂の進展を停止させるべき箇所は、複合材100の設計段階において特定される。同様に、第1面内方向Xおよび第2面内方向Yのいずれの方向にき裂が進展するかは、複合材100の設計段階において特定される。以下、き裂が第1面内方向Xの一方向(図2の右方向)に進展する場合を例として、き裂進展抑制部材30の構成について説明する。 The crack growth suppression member 30 is formed of, for example, metal foil and arranged in the adhesive layer 20 . The crack growth suppression member 30 is arranged in the composite material 100 at a location where a crack is likely to occur and where crack growth should be stopped. In the composite material 100 , locations where cracks are likely to occur and crack growth should be stopped are specified in the design stage of the composite material 100 . Similarly, which direction, the first in-plane direction X or the second in-plane direction Y, the crack propagates is specified in the design stage of the composite material 100 . The configuration of the crack growth suppression member 30 will be described below, taking as an example a case where a crack propagates in one of the first in-plane directions X (to the right in FIG. 2).

図2は、実施形態にかかる接着部材としての複合材の要部を拡大して示す拡大断面図である。き裂進展抑制部材30は、図示するように、2つの誘導部31と、進展抑制部32とを有している。2つの誘導部31は、接着層20内で、互いに対向しながら、第1面内方向Xに沿って延在する。なお、図1に示す例では、模式的に、誘導部31を直線状に示しているが、誘導部31の形状はこれに限られない。「第1面内方向Xに沿った方向に延在する」とは、誘導部31が主として第1面内方向Xに沿って延在することを意味し、第1面内方向Xに対して傾斜して延在してもよいし、完全に直線状でなくてもよい。 FIG. 2 is an enlarged cross-sectional view showing an enlarged main part of a composite material as an adhesive member according to the embodiment. The crack growth suppression member 30 has two guiding portions 31 and a growth suppression portion 32 as illustrated. The two guide portions 31 extend along the first in-plane direction X while facing each other within the adhesive layer 20 . In addition, in the example shown in FIG. 1 , the guiding portion 31 is schematically shown in a linear shape, but the shape of the guiding portion 31 is not limited to this. “Extending in the direction along the first in-plane direction X” means that the guide portion 31 extends mainly along the first in-plane direction X, and It may extend obliquely and may not be perfectly straight.

進展抑制部32は、2つの誘導部31の一方側の端部に設けられ、2つの誘導部31の間に延在する。言い換えると、2つの誘導部31は、進展抑制部32の端部から第1面内方向Xに沿って延びる。進展抑制部32は、図1に示すように、2つの誘導部31の間を第1面内方向Xのき裂Cが進展する側に向けて凸形状を呈して延びる。すなわち、進展抑制部32は、第1複合部材10A側から第2複合部材10B側にかけて、第1面内方向Xに向けて凸形状を呈する。本実施形態では、進展抑制部32は、所定の曲率半径で凸形状を呈する半円状の湾曲部である。進展抑制部32が半円状である場合、その曲率半径の上限は、接着層20の厚みの半分よりもわずかに小さい値とされる。ただし、進展抑制部32は、半円状に限らず、所定の曲率半径で形成される円弧状の凸部であってもよい。また、進展抑制部32は、途中で曲率半径が変化するものであってもよい。これにより、き裂進展抑制部材30は、図1に示すように、2つの誘導部31と進展抑制部32とで断面U字形状を呈する。なお、き裂進展抑制部材30の第2面内方向Yにおける幅は、複合材100のサイズ、き裂の進展を止めるべき箇所の範囲等にあわせて、適宜決定されればよい。 The progress suppressing portion 32 is provided at one end of the two guiding portions 31 and extends between the two guiding portions 31 . In other words, the two guiding portions 31 extend along the first in-plane direction X from the end portion of the progression suppressing portion 32 . As shown in FIG. 1 , the propagation suppressing portion 32 extends between the two guide portions 31 in a convex shape toward the side where the crack C in the first in-plane direction X propagates. That is, the progress suppressing portion 32 has a convex shape in the first in-plane direction X from the first composite member 10A side to the second composite member 10B side. In the present embodiment, the progression suppressing portion 32 is a semicircular curved portion having a convex shape with a predetermined radius of curvature. When the progress suppressing portion 32 is semicircular, the upper limit of the radius of curvature is slightly smaller than half the thickness of the adhesive layer 20 . However, the progress suppressing portion 32 is not limited to a semicircular shape, and may be an arc-shaped convex portion formed with a predetermined radius of curvature. Further, the progression suppressing portion 32 may have a radius of curvature that changes in the middle. Thereby, as shown in FIG. 1 , the crack growth suppression member 30 exhibits a U-shaped cross section with the two guiding portions 31 and the growth suppression portion 32 . The width of the crack growth suppression member 30 in the second in-plane direction Y may be appropriately determined in accordance with the size of the composite material 100, the range of locations where crack growth should be stopped, and the like.

そして、き裂進展抑制部材30は、接着層20との界面、すなわち表面33における接着層20との接着強度が、接着層20と第1複合部材10Aおよび第2複合部材10Bとの界面の接着強度よりも弱く設定されている。き裂進展抑制部材30の表面33における接着層20との接着強度は、例えば、材料構成を調整したり、表面33に例えば化学的な処理を施したりすることで、調整することができる。本実施形態では、き裂進展抑制部材30は、金属箔により形成される。なお、表面33における接着層20との接着強度を適切なものとすることができれば、き裂進展抑制部材30は、金属材料以外の材料で形成されてもよい。 In the crack growth suppression member 30, the adhesion strength between the interface with the adhesive layer 20, that is, the surface 33 with the adhesive layer 20 is the adhesion of the interface between the adhesive layer 20 and the first composite member 10A and the second composite member 10B. It is set weaker than strength. The adhesive strength of the surface 33 of the crack growth suppression member 30 to the adhesive layer 20 can be adjusted, for example, by adjusting the material composition or chemically treating the surface 33 . In this embodiment, the crack growth suppression member 30 is made of metal foil. Note that the crack growth suppression member 30 may be formed of a material other than a metal material as long as the adhesive strength between the surface 33 and the adhesive layer 20 can be made appropriate.

次に、実施形態にかかる接着部材としての複合材100の作用について説明する。いま、複合材100に対して荷重が作用し、例えば第1複合部材10Aと接着層20との界面でき裂C(剥離)が生じたとする。このとき、き裂Cは、第1面内方向Xに沿って進展していくことになる。上述したように、表面33における接着層20との接着強度が、接着層20と第1複合部材10Aおよび第2複合部材10Bとの界面の接着強度よりも弱い。そのため、接着層20に生じたき裂Cは、図2に示すように、より接着強度が弱い表面33へと誘導される。このとき、誘導部31が第1面内方向Xに沿って延在するため、き裂Cを誘導する部分を比較的に長い範囲に設けることができ、き裂Cを誘導部31の表面33へと、より確実に誘導させることができる。 Next, the action of the composite material 100 as an adhesive member according to the embodiment will be described. Assume that a load is applied to the composite material 100 and a crack C (peeling) occurs at the interface between the first composite member 10A and the adhesive layer 20, for example. At this time, the crack C propagates along the first in-plane direction X. As described above, the adhesive strength between the surface 33 and the adhesive layer 20 is weaker than the adhesive strength at the interface between the adhesive layer 20 and the first composite member 10A and the second composite member 10B. Therefore, the crack C generated in the adhesive layer 20 is guided to the surface 33 with weaker adhesive strength, as shown in FIG. At this time, since the guide portion 31 extends along the first in-plane direction X, the portion that guides the crack C can be provided in a relatively long range, and the crack C is formed on the surface 33 of the guide portion 31. can be guided more reliably.

誘導部31に誘導されたき裂Cは、さらに、進展抑制部32の表面33へと誘導されていく。そして、進展抑制部32に誘導されたき裂Cは、進展抑制部32に沿って、面外方向Z側に向かうように誘導される。その結果、き裂Cの先端が大きな曲げ半径を持つ形状となり、応力集中度が低下することで、き裂Cの第1面内方向Xへの進展抵抗が増加して進展が抑制される。それにより、き裂Cの進展は、進展抑制部32の中途で停止することになる。 The crack C guided to the guiding portion 31 is further guided to the surface 33 of the growth suppressing portion 32 . Then, the crack C guided to the propagation suppressing portion 32 is guided along the propagation suppressing portion 32 toward the out-of-plane direction Z side. As a result, the tip of the crack C has a shape with a large bending radius, and the degree of stress concentration is reduced, thereby increasing the resistance to propagation of the crack C in the first in-plane direction X and suppressing its propagation. As a result, the propagation of the crack C is stopped halfway through the propagation suppressing portion 32 .

ここで、進展抑制部32が誘導部31から急峻に変化しすぎる場合、き裂Cは、誘導部31から進展抑制部32へとスムーズに誘導されず、第1面内方向Xに沿って進展する可能性がある。一方で、進展抑制部32が誘導部31から緩やかに変化しすぎる場合、言い換えると、凸形状が先鋭な形状となりすぎる場合、き裂Cの第1面内方向Xへの進展抵抗が十分に増加しない。そのため、結果的にき裂Cの進展を停止させられない可能性がある。したがって、進展抑制部32は、誘導部31の表面33に沿って進展してきたき裂Cを表面33に沿って面外方向Zへと誘導することができ、かつ、き裂Cの第1面内方向Xへの進展抵抗の増加によって、その進展を停止させることができる角度で形成される。 Here, when the growth suppressing portion 32 changes too steeply from the guide portion 31, the crack C is not smoothly guided from the guide portion 31 to the progress suppressing portion 32, and propagates along the first in-plane direction X. there's a possibility that. On the other hand, if the growth suppressing portion 32 changes too gently from the guiding portion 31, in other words, if the convex shape becomes too sharp, the resistance to propagation of the crack C in the first in-plane direction X increases sufficiently. do not do. Therefore, there is a possibility that the growth of the crack C cannot be stopped as a result. Therefore, the propagation suppressing portion 32 can guide the crack C, which has propagated along the surface 33 of the guiding portion 31, along the surface 33 in the out-of-plane direction Z, and It is formed at an angle whose progress can be stopped by increasing resistance to progress in direction X.

なお、図2では、き裂進展抑制部材30の一方側の表面33にき裂Cが誘導される例を説明した。ただし、き裂進展抑制部材30の他方側の表面34においても、接着層20との接着強度が接着層20と第1複合部材10Aおよび第2複合部材10Bとの界面の接着強度よりも弱ければ、他方側の表面34にき裂Cが誘導されることもあり得る。この場合にも、他方側の表面34に誘導されたき裂Cは、進展抑制部32に至ることで、第1面内方向Xへの進展抵抗が増加し、その進展が停止される。なお、表面33と接着層20との接着強度と、表面34と接着層20との接着強度とは、異なる値とされてもよく、少なくともいずれか一方が、接着層20と第1複合部材10Aおよび第2複合部材10Bとの界面の接着強度より弱く設定されればよい。さらに、表面33、34の任意の位置で、接着層20との接着強度に分布を持たせてもよい。 Note that FIG. 2 describes an example in which the crack C is induced on the surface 33 on one side of the crack growth suppression member 30 . However, even on the surface 34 on the other side of the crack growth suppression member 30, if the adhesive strength with the adhesive layer 20 is weaker than the adhesive strength at the interface between the adhesive layer 20 and the first composite member 10A and the second composite member 10B , a crack C may be induced in the surface 34 on the other side. In this case as well, the crack C induced to the surface 34 on the other side reaches the growth suppressing portion 32 , so that the resistance to growth in the first in-plane direction X increases and the growth is stopped. Note that the adhesive strength between the surface 33 and the adhesive layer 20 and the adhesive strength between the surface 34 and the adhesive layer 20 may be different values, and at least one of them may be the adhesive layer 20 and the first composite member 10A. and the adhesive strength of the interface with the second composite member 10B. Furthermore, the adhesive strength with the adhesive layer 20 may be distributed at arbitrary positions on the surfaces 33 and 34 .

以上説明したように、実施形態にかかる接着部材としての複合材100は、第1複合部材(第1部材)10Aと、第2複合部材(第2部材)10Bと、第1複合部材10Aと第2複合部材10Bとを接着する接着剤を含む接着層20と、接着層20内に配置され、接着層20内で第1面内方向Xに向かうき裂Cの進展を抑制するき裂進展抑制部材30と、を備え、き裂進展抑制部材30は、第1複合部材10A側から第2複合部材10B側にかけて第1面内方向Xに凸形状を呈する進展抑制部32を有し、接着層20との界面、すなわち表面33の接着強度が接着層20と第1複合部材10Aおよび第2複合部材10Bとの界面の接着強度よりも弱い。 As described above, the composite material 100 as the adhesive member according to the embodiment includes the first composite member (first member) 10A, the second composite member (second member) 10B, the first composite member 10A and the second An adhesive layer 20 containing an adhesive that bonds the two composite members 10B together, and a crack growth suppression that is disposed in the adhesive layer 20 and suppresses the propagation of the crack C in the adhesive layer 20 in the first in-plane direction X. and a member 30, the crack growth suppressing member 30 has a convex shape in the first in-plane direction X from the first composite member 10A side to the second composite member 10B side, and has an adhesive layer 20, that is, the adhesive strength of the surface 33 is weaker than the adhesive strength of the interfaces between the adhesive layer 20 and the first composite member 10A and the second composite member 10B.

この構成により、接着層20とき裂進展抑制部材30との界面の接着強度が、接着層20と第1複合部材10Aおよび第2複合部材10Bとの界面の接着強度よりも弱いため、接着層20で発生して第1面内方向Xに向かうき裂Cを接着層20とき裂進展抑制部材30との界面へと誘導することができる。そして、き裂進展抑制部材30の進展抑制部32へと誘導されたき裂は、進展抑制部32の凸形状によって面外方向Zに進展することになる。その結果、き裂Cの第1面内方向Xへの進展抵抗が大きくなり、き裂Cの進展が抑制される。すなわち、接着層20内において繊維を面外方向に延在するように配置することなく、き裂Cの進展を抑制することが可能となる。したがって、実施形態によれば、複合材(接着部材)100の面内特性に影響を与えないようにしながら、接着層20で発生するき裂Cの進展を抑制することが可能となる。 With this configuration, the adhesive strength at the interface between the adhesive layer 20 and the crack growth suppressing member 30 is weaker than the adhesive strength at the interface between the adhesive layer 20 and the first composite member 10A and the second composite member 10B. can be guided to the interface between the adhesive layer 20 and the crack growth suppressing member 30 . Then, the crack guided to the propagation suppressing portion 32 of the crack propagation suppressing member 30 propagates in the out-of-plane direction Z due to the convex shape of the propagation suppressing portion 32 . As a result, the resistance to propagation of the crack C in the first in-plane direction X increases, and propagation of the crack C is suppressed. That is, it is possible to suppress the propagation of the crack C without arranging the fibers in the adhesive layer 20 so as to extend in the out-of-plane direction. Therefore, according to the embodiment, it is possible to suppress the propagation of the crack C generated in the adhesive layer 20 while preventing the in-plane characteristics of the composite material (adhesive member) 100 from being affected.

また、複合材100について、複数のき裂進展抑制部材30を接着層20内に配置しておけば、き裂Cの進展度合いに応じた修復の必要性の判断を容易に行うことができる。すなわち、複数のき裂進展抑制部材30のうち、ある1つが配置される箇所まではき裂が進展しているが、他のき裂進展抑制部材30が配置される箇所まではき裂が進展していないといったように、き裂Cの進展度合いを確認することができ、その結果に応じて修復の必要性を判断することが可能となる。 In addition, if a plurality of crack growth suppression members 30 are arranged in the adhesive layer 20 of the composite material 100, it is possible to easily determine the necessity of repair according to the degree of crack C growth. That is, the crack propagates to the location where one of the plurality of crack growth suppression members 30 is arranged, but the crack propagates to the location where the other crack growth suppression members 30 are arranged. It is possible to confirm the degree of progress of the crack C, such as that the crack C has not occurred, and to judge the necessity of repair according to the result.

また、進展抑制部32は、凸形状を呈する湾曲部である。この構成により、進展抑制部32によってき裂Cをスムーズに誘導しつつ、き裂Cの第1面内方向Xへの進展抵抗を増加させることができる。 Further, the progress suppressing portion 32 is a curved portion having a convex shape. With this configuration, the crack C can be smoothly guided by the propagation suppressing portion 32, and the propagation resistance of the crack C in the first in-plane direction X can be increased.

また、き裂進展抑制部材30は、進展抑制部32の端部から第1面内方向Xに沿って延びる誘導部31をさらに有する。この構成により、接着層20で発生して第1面内方向Xに向かうき裂Cを誘導部31へとより確実に誘導させることができる。ただし、接着層20内で発生したき裂Cを進展抑制部32の表面33に誘導することができれば、誘導部31をき裂進展抑制部材30から省略してもよい。また、誘導部31をき裂進展抑制部材30から完全に省略するのではなく、図1に示す例に比べて、誘導部31の長さをより短くしてもよい。 Further, the crack growth suppressing member 30 further has a guiding portion 31 extending along the first in-plane direction X from the end portion of the crack propagation suppressing portion 32 . With this configuration, the crack C generated in the adhesive layer 20 and directed in the first in-plane direction X can be more reliably guided to the guiding portion 31 . However, if the crack C generated in the adhesive layer 20 can be guided to the surface 33 of the crack growth suppressing portion 32 , the guiding portion 31 may be omitted from the crack growth suppressing member 30 . Moreover, rather than completely omitting the guide portion 31 from the crack growth suppression member 30, the length of the guide portion 31 may be made shorter than in the example shown in FIG.

図1および図2では、き裂進展抑制部材30が接着層20内に1つ配置される例を示したが、き裂進展抑制部材30の配置構成はこれに限られない。図3は、実施形態の変形例にかかる複合材を示す断面図である。変形例にかかる複合材200の構成は、以下に説明するものを除き、複合材100と同様である。そのため、同一の構成については同一の符号を付し、説明を省略する。 1 and 2 show an example in which one crack growth suppression member 30 is arranged in the adhesive layer 20, but the arrangement configuration of the crack growth suppression member 30 is not limited to this. FIG. 3 is a cross-sectional view showing a composite material according to a modification of the embodiment; The configuration of the composite material 200 according to the modified example is the same as that of the composite material 100 except for what will be described below. Therefore, the same components are denoted by the same reference numerals, and the description thereof is omitted.

変形例にかかる複合材200は、図示するように、接着層20内において、き裂進展抑制部材30が第1面内方向Xに沿って複数配置されている。この構成により、複数のき裂進展抑制部材30をより広い範囲に配置することができるため、接着層20で第1面内方向Xへと向かうき裂Cの進展を、より確実に抑制することができる。また、複合材200において、隣り合うき裂進展抑制部材30は、進展抑制部32の凸形状が互いに反対方向を向いて配置されている。この構成により、き裂Cが第1面内方向Xの2方向のいずれに向かう場合でも、その進展をより確実に抑制することができる。 In the composite material 200 according to the modified example, a plurality of crack growth suppressing members 30 are arranged along the first in-plane direction X in the adhesive layer 20 as illustrated. With this configuration, the plurality of crack growth suppression members 30 can be arranged in a wider range, so that the growth of the crack C in the adhesive layer 20 in the first in-plane direction X can be suppressed more reliably. can be done. Further, in the composite material 200, the adjacent crack growth suppression members 30 are arranged such that the convex shapes of the crack growth suppression portions 32 face opposite directions to each other. With this configuration, even when the crack C is oriented in either of the two directions of the first in-plane direction X, the propagation of the crack can be suppressed more reliably.

なお、隣り合うき裂進展抑制部材30は、進展抑制部32の凸形状が同方向を向いて配置されてもよい。また、図3では、き裂進展抑制部材30を接着層20内に2つ配置する例を示しているが、き裂進展抑制部材30は、接着層20内で第1面内方向Xに沿って3つ以上配置されてもよい。その場合、隣り合うき裂進展抑制部材30の少なくとも一部が、進展抑制部32の凸形状が互いに反対方向を向いて配置されてもよいし、すべてのき裂進展抑制部材30が進展抑制部32の凸形状が同方向を向いて配置されてもよい。 Adjacent crack growth suppression members 30 may be arranged such that the convex shapes of the crack growth suppression portions 32 face the same direction. 3 shows an example in which two crack growth suppression members 30 are arranged in the adhesive layer 20, the crack growth suppression members 30 are arranged in the first in-plane direction X in the adhesive layer 20. three or more may be arranged. In that case, at least some of the adjacent crack growth suppressing members 30 may be arranged such that the convex shapes of the crack growth suppressing portions 32 face opposite directions to each other, or all the crack growth suppressing members 30 may 32 convex shapes may be arranged facing the same direction.

図4および図5は、第1の変形例にかかるき裂進展抑制部材を含む複合材を示す断面図である。第1の変形例にかかるき裂進展抑制部材40は、図4に示すように、誘導部31の両側に進展抑制部32が設けられ、輪を描くように形成されている。この構成により、1つのき裂進展抑制部材40によって、き裂Cが第1面内方向Xの2方向のいずれに向かう場合でも、その進展をより確実に抑制することができる。なお、第2の変形例にかかるき裂進展抑制部材40は、図5に破線で囲んだ範囲に示すように、1枚のき裂進展抑制部材40となる基材を途中で折り返すことで、一部オーバーラップするオーバーラップ部41が形成されてもよい。 4 and 5 are cross-sectional views showing a composite material including a crack growth suppressing member according to a first modification. As shown in FIG. 4, a crack growth suppressing member 40 according to a first modified example is formed so as to draw a ring by providing the crack propagation suppressing portions 32 on both sides of the guiding portion 31 . With this configuration, one crack propagation suppression member 40 can more reliably suppress the propagation of the crack C regardless of which of the two directions of the first in-plane direction X the crack C faces. In addition, the crack growth suppression member 40 according to the second modification is obtained by folding back the base material that becomes one crack growth suppression member 40 in the middle, as shown in the range surrounded by the broken line in FIG. An overlapping portion 41 that partially overlaps may be formed.

図6は、第2の変形例にかかるき裂進展抑制部材を示す正面図であり、図7は、図6のA-A線に沿った端面図である。第2の変形例にかかるき裂進展抑制部材50は、進展抑制部32のみを有する。ただし、き裂進展抑制部材60は、進展抑制部32が環状に連続して形成された筒状部材として形成されている。図7に示す例では、環状の進展抑制部32は、筒状のき裂進展抑制部材60の外側に向かって凸形状を呈する。この構成により、接着層20内において、き裂Cが第1面内方向Xおよび第2面内方向Yのいずれに進展するものであっても、その進展をより確実に抑制することができる。特に、複数のき裂進展抑制部材50を接着層20内に散りばめて配置しておけば、より効果的にき裂Cの進展を抑制することができる。 FIG. 6 is a front view showing a crack growth suppressing member according to a second modification, and FIG. 7 is an end view along line AA of FIG. A crack growth suppression member 50 according to the second modification has only the crack growth suppression portion 32 . However, the crack growth suppressing member 60 is formed as a cylindrical member in which the crack progress suppressing portion 32 is continuously formed in an annular shape. In the example shown in FIG. 7 , the annular crack growth suppressing portion 32 has a convex shape toward the outside of the tubular crack growth suppressing member 60 . With this configuration, regardless of whether the crack C propagates in the first in-plane direction X or the second in-plane direction Y in the adhesive layer 20, the propagation can be more reliably suppressed. In particular, if a plurality of crack growth suppression members 50 are scattered in the adhesive layer 20 and arranged, the growth of the crack C can be suppressed more effectively.

なお、き裂進展抑制部材50の構成は、これに限られない。図8は、第2の変形例にかかるき裂進展抑制部材の他の構成例を示す端面図である。図示するように、き裂進展抑制部材50は、環状の進展抑制部32が、筒状のき裂進展抑制部材50の内側に向かって凸形状を呈するものであってもよい。また、き裂進展抑制部材50は、環状に連続して形成された誘導部31をさらに備えるものであってもよい。 Note that the configuration of the crack growth suppression member 50 is not limited to this. FIG. 8 is an end view showing another configuration example of the crack growth suppression member according to the second modification. As shown in the figure, the crack growth suppression member 50 may have an annular crack growth suppression portion 32 that protrudes toward the inner side of the tubular crack growth suppression member 50 . Moreover, the crack growth suppression member 50 may further include a guiding portion 31 that is continuously formed in an annular shape.

図9は、第3の変形例にかかるき裂進展抑制部材を示す断面図である。第3の変形例にかかるき裂進展抑制部材60は、進展抑制部32が湾曲部ではなく、複数の直線部32Aによって多角形状に形成されている。このように、進展抑制部32を複数の直線部32Aによって構成し、凸形状を呈するようにしてもよい。なお、図9に示す直線部32Aの数は例示であり、より多くの直線部32Aで進展抑制部32を形成してもよいし、より少ない直線部32Aで進展抑制部32を形成してもよい。 FIG. 9 is a cross-sectional view showing a crack growth suppression member according to a third modification. In the crack growth suppressing member 60 according to the third modified example, the crack growth suppressing portion 32 is formed in a polygonal shape by a plurality of straight portions 32A instead of curved portions. In this manner, the progression suppressing portion 32 may be configured by a plurality of linear portions 32A to have a convex shape. Note that the number of straight portions 32A shown in FIG. 9 is an example, and the progress suppressing portion 32 may be formed with more straight portions 32A, or the spread suppressing portion 32 may be formed with fewer straight portions 32A. good.

図10は、第4の変形例にかかるき裂進展抑制部材を示す説明図である。第4の変形例にかかるき裂進展抑制部材70は、図示するように、複数のき裂進展抑制部材30が第1面内方向Xおよび第2面内方向Yに沿って複数並んで配置される。なお、図10に示す例では、き裂進展抑制部材30の進展抑制部32が平坦部321を含んでいるが、これは後述する形成方法によるものである。複数のき裂進展抑制部材30は、連結部71を介して連結されている。連結部71は、進展抑制部32の平坦部321と平行に並び、平坦部321に連結される段部711と、段部711同士の間を第1面内方向Xに沿って延びる保持部712とを有する。この構成により、複数のき裂進展抑制部材30を一つの部材として取り扱うことができる。また、第1複合部材10A、第2複合部材10Bおよび接着層20を接着する際に、例えば接着に加熱が伴う場合等に接着層20内に含まれる樹脂が軟化しても、複数のき裂進展抑制部材30間に連結部71(保持部712)が存在することで、き裂進展抑制部材70が接着層20内で流動することを抑制することができる。 FIG. 10 is an explanatory diagram showing a crack growth suppression member according to a fourth modification. A crack growth suppressing member 70 according to a fourth modification includes a plurality of crack growth suppressing members 30 arranged side by side along the first in-plane direction X and the second in-plane direction Y, as shown in the figure. be. In addition, in the example shown in FIG. 10, the crack growth restraining portion 32 of the crack growth restraining member 30 includes the flat portion 321, but this is due to the formation method described later. The plurality of crack growth suppression members 30 are connected via connecting portions 71 . The connecting portion 71 is arranged in parallel with the flat portion 321 of the progression suppressing portion 32 and includes a stepped portion 711 connected to the flat portion 321 and a holding portion 712 extending between the stepped portions 711 along the first in-plane direction X. and With this configuration, the plurality of crack growth suppression members 30 can be handled as one member. Further, when bonding the first composite member 10A, the second composite member 10B, and the adhesive layer 20, even if the resin contained in the adhesive layer 20 is softened, for example, when the bonding is accompanied by heating, a plurality of cracks may occur. The presence of the connecting portions 71 (holding portions 712 ) between the crack growth suppression members 30 can suppress the crack growth suppression members 70 from flowing within the adhesive layer 20 .

次に、実施形態にかかる接着層20の形成方法について説明する。まず、図10に示す第4の変形例にかかるき裂進展抑制部材70を含む接着層20の形成方法について、図10および図11を参照しながら説明する。図11は、き裂進展抑制部材の基材を示す説明図である。図11に示すように、き裂進展抑制部材70の基材80を準備する。基材80は、本実施形態では金属箔であるが、上述したように、接着層20との界面の接着強度を適切に調節することができれば、金属材料以外の材料であってもよい。 Next, a method for forming the adhesive layer 20 according to the embodiment will be described. First, a method of forming an adhesive layer 20 including a crack growth suppression member 70 according to the fourth modification shown in FIG. 10 will be described with reference to FIGS. 10 and 11. FIG. FIG. 11 is an explanatory diagram showing the base material of the crack growth suppression member. As shown in FIG. 11, the base material 80 of the crack growth suppression member 70 is prepared. Although the base material 80 is a metal foil in this embodiment, it may be a material other than a metal material as long as the adhesive strength of the interface with the adhesive layer 20 can be appropriately adjusted as described above.

まず、基材80に、き裂進展抑制部材70に含まれる各き裂進展抑制部材30および連結部71を形成するための複数の切り込み線L1、複数の第1折り曲げ線L2および複数の第2折り曲げ線L3を規定して描画する。図11中において実線で示す複数の切り込み線L1は、基材80を切り込むための線である。図11中において破線で示す複数の第1折り曲げ線L2は、基材80を図中紙面方向の奥側へと折り曲げるための線である。図11中において一点鎖線で示す複数の第2折り曲げ線L3は、基材80を図中紙面方向の手前側へと折り曲げるための線である。 First, a plurality of cut lines L1, a plurality of first bending lines L2 and a plurality of second bending lines L1 for forming the crack growth suppressing members 30 and the connecting portions 71 included in the crack growth suppressing member 70 are formed in the base material 80. A folding line L3 is defined and drawn. A plurality of cutting lines L1 indicated by solid lines in FIG. 11 are lines for cutting the base material 80 . A plurality of first bending lines L2 indicated by dashed lines in FIG. 11 are lines for bending the base material 80 toward the back side in the paper surface direction of the drawing. A plurality of second bending lines L3 indicated by dashed lines in FIG. 11 are lines for bending the base material 80 toward the front side in the direction of the plane of the drawing.

次に、基材80を切り込み線L1に沿って切り込む。ここで、図11で斜線を付した範囲の面91が、図10のき裂進展抑制部材30Aとなり、図11で斜線を付した範囲の面92が、図10のき裂進展抑制部材30Bとなるものとする。また、図11に例示するように、切り込み線L1の一つを「切り込み線L11」と称し、切り込み線L1の一つを「切り込み線L11」と称する。このとき、切り込み線L11で切り込まれた部分は、図10に示すように、第1面内方向Xに沿って並ぶ2つのき裂進展抑制部材30A、30Bに含まれる誘導部31の端部の辺となる。また、切り込み線L12で切り込まれた部分は、図10に示すように、き裂進展抑制部材30A、30Bの側部の辺となると共に、連結部71の保持部712の側部の辺となる。このように、各切り込み線L1をすべて切り込むことで、複数のき裂進展抑制部材30および連結部71の保持部712の輪郭となる辺が形成される。 Next, the base material 80 is cut along the cut line L1. Here, the surface 91 in the shaded range in FIG. 11 is the crack growth suppression member 30A in FIG. 10, and the surface 92 in the shaded range in FIG. 11 is the crack growth suppression member 30B in FIG. shall be. Moreover, as illustrated in FIG. 11, one of the cut lines L1 is called "cut line L11", and one of the cut lines L1 is called "cut line L11". At this time, as shown in FIG. 10, the portion cut by the cut line L11 is the end portion of the guide portion 31 included in the two crack growth suppression members 30A and 30B arranged along the first in-plane direction X. becomes the side of In addition, as shown in FIG. 10, the portions cut by the cut lines L12 become the sides of the crack growth suppression members 30A and 30B, and the sides of the holding portion 712 of the connecting portion 71. Become. In this way, by cutting all of the cut lines L1, the sides forming the contours of the plurality of crack growth suppression members 30 and the holding portion 712 of the connecting portion 71 are formed.

さらに、基材80を複数の第1折り曲げ線L2に沿って紙面方向の奥側へと折り曲げ、複数の第2折り曲げ線L3に沿って紙面方向の手前側へと折り曲げる。その結果、図10に示すように第1折り曲げ線L2に囲まれた範囲が、き裂進展抑制部材30の平坦部321となる。このとき、き裂進展抑制部材30の平坦部321の周囲が湾曲部となるように折り曲げることで、平坦部321を含んで進展抑制部32が形成される。また、第1折り曲げ線L2と第2折り曲げ線L3とに囲まれた範囲が連結部71の保持部712となる。これにより、き裂進展抑制部材70が形成される。 Further, the base material 80 is bent toward the back side in the paper surface direction along the plurality of first bending lines L2, and is bent toward the front side in the paper surface direction along the plurality of second bending lines L3. As a result, as shown in FIG. 10 , the area surrounded by the first bending line L2 becomes the flat portion 321 of the crack growth suppression member 30 . At this time, by bending the periphery of the flat portion 321 of the crack growth suppression member 30 so as to form a curved portion, the growth suppression portion 32 including the flat portion 321 is formed. A holding portion 712 of the connecting portion 71 is a range surrounded by the first bending line L2 and the second bending line L3. Thereby, the crack growth suppression member 70 is formed.

そして、上述の手順で形成したき裂進展抑制部材70に、接着剤を含む樹脂を含浸させることで、接着層20を形成する。き裂進展抑制部材70への樹脂の含浸は、周知の含浸手法により実行されればよい。 Then, the adhesive layer 20 is formed by impregnating the crack growth suppression member 70 formed by the above procedure with a resin containing an adhesive. The resin impregnation of the crack growth suppression member 70 may be performed by a well-known impregnation method.

この構成により、複数が連結されたき裂進展抑制部材30を含む接着層20を容易に形成することができる。また、上述したように、複数のき裂進展抑制部材30を一つの部材として取り扱うことができる。また、上述したように、第1複合部材10A、第2複合部材10Bおよび接着層20を接着する際に、接着層20内に含まれる樹脂が軟化しても、複数のき裂進展抑制部材30間に連結部71(保持部712)が存在することで、き裂進展抑制部材70が接着層20内で流動することを抑制することができる。 With this configuration, it is possible to easily form the adhesive layer 20 including a plurality of crack growth suppression members 30 that are connected to each other. Moreover, as described above, the plurality of crack growth suppression members 30 can be handled as one member. Further, as described above, when the first composite member 10A, the second composite member 10B, and the adhesive layer 20 are adhered, even if the resin contained in the adhesive layer 20 softens, the crack growth suppression members 30 The presence of the connecting portion 71 (holding portion 712 ) therebetween can suppress the crack growth suppression member 70 from flowing within the adhesive layer 20 .

なお、接着剤を含む樹脂を含浸させる手法は、図6から図8に示す筒状のき裂進展抑制部材50が配置された接着層20を形成する際にも適用される。 The technique of impregnating resin containing adhesive is also applied when forming the adhesive layer 20 on which the cylindrical crack growth suppression member 50 shown in FIGS. 6 to 8 is arranged.

次に、図1のき裂進展抑制部材30を含む接着層20の形成方法について、図12を参照しながら説明する。図12は、き裂進展抑制部材の周囲に樹脂フィルムを配置する様子を示す説明図である。図示するように、断面U字形状に形成されたき裂進展抑制部材30の内側、すなわち他方の表面34側に、接着剤を含む樹脂フィルム25を複数(例えば2層)重ねて配置し、隙間ができないように表面34に接着させる。また、き裂進展抑制部材30の外側すなわち一方の表面33側に、接着剤を含む樹脂フィルム25を複数(例えば2層)重ねて配置し、表面33に接着させる。これにより、図12に示す例では、き裂進展抑制部材30の内側および外側にあわせて4層の樹脂フィルム25が接着される。そして、き裂進展抑制部材30の内側および外側に接着された樹脂フィルム25と同数(図12に示す例では、4層)の樹脂フィルム25を、進展抑制部32側からき裂進展抑制部材30に隙間ができないように接着する。これにより、図1に示す接着層20が形成される。なお、樹脂フィルム25は、接着剤を含むフィルム状部材であればよく、接着シート、接着テープ等であってもよい。 Next, a method for forming the adhesive layer 20 including the crack growth suppressing member 30 of FIG. 1 will be described with reference to FIG. FIG. 12 is an explanatory diagram showing how a resin film is arranged around the crack growth suppression member. As shown in the figure, a plurality (for example, two layers) of resin films 25 containing an adhesive are stacked inside the crack growth suppression member 30 formed to have a U-shaped cross section, that is, on the other surface 34 side, and the gap is formed. It adheres to the surface 34 so that it cannot. Also, a plurality of (eg, two layers) of resin films 25 containing an adhesive are stacked on the outside of the crack growth suppression member 30 , that is, on one surface 33 side, and adhered to the surface 33 . As a result, in the example shown in FIG. 12 , four layers of resin films 25 are adhered to the inside and outside of the crack growth suppression member 30 . Then, the resin films 25 of the same number (four layers in the example shown in FIG. 12) as the resin films 25 adhered to the inside and outside of the crack growth suppression member 30 are attached to the crack growth suppression member 30 from the crack growth suppression portion 32 side. Glue so that there are no gaps. Thereby, the adhesive layer 20 shown in FIG. 1 is formed. Note that the resin film 25 may be a film-like member containing an adhesive, and may be an adhesive sheet, an adhesive tape, or the like.

この構成により、き裂進展抑制部材30を含む接着層20を容易に形成することができる。図3に示すように、接着層20にき裂進展抑制部材30が複数配置される場合には、図12に示す形成方法で形成した接着層20を複数つなぎあわせればよい。また、本形成方法は、図4および図5のき裂進展抑制部材40、図9のき裂進展抑制部材60を含む接着層20を形成する際にも適用することができる。なお、き裂進展抑制部材30、40、60を含む接着層20についても、き裂進展抑制部材30に接着剤を含む樹脂を含浸させて形成してもよい。 With this configuration, the adhesive layer 20 including the crack growth suppression member 30 can be easily formed. As shown in FIG. 3, when a plurality of crack growth suppression members 30 are arranged on the adhesive layer 20, a plurality of adhesive layers 20 formed by the formation method shown in FIG. 12 may be connected. Further, this forming method can also be applied when forming the adhesive layer 20 including the crack growth suppressing member 40 of FIGS. 4 and 5 and the crack growth suppressing member 60 of FIG. The adhesive layer 20 including the crack growth suppression members 30, 40, and 60 may also be formed by impregnating the crack growth suppression member 30 with a resin containing an adhesive.

本実施形態では、第1部材として第1複合部材10A、第2部材として第2複合部材10Bを備えた複合材100を例として、実施形態にかかる接着部材について説明した。ただし、接着部材は、第1部材および第2部材のいずれか一方または双方が、例えば金属材、発泡コア材、ハニカムコア材、樹脂材等で形成された非複合材であってもよい。 In this embodiment, the adhesive member according to the embodiment has been described by taking as an example the composite material 100 including the first composite member 10A as the first member and the second composite member 10B as the second member. However, the adhesive member may be a non-composite material in which one or both of the first member and the second member are made of, for example, a metal material, a foam core material, a honeycomb core material, a resin material, or the like.

10A 第1複合部材
10B 第2複合部材
11 複合材料層
20 接着層
25 樹脂フィルム
30,30A,30B,40,50,60,70 き裂進展抑制部材
31 誘導部
32 進展抑制部
321 平坦部
32A 直線部
33,34 表面
41 オーバーラップ部
71 連結部
711 段部
712 保持部
80 基材
91,92 面
100,200 複合材
C き裂
L1,L11,L12 切り込み線
L2 第1折り曲げ線
L3 第2折り曲げ線
X 第1面内方向
Y 第2面内方向
Z 面外方向
10A First composite member 10B Second composite member 11 Composite material layer 20 Adhesive layer 25 Resin film 30, 30A, 30B, 40, 50, 60, 70 Crack growth suppression member 31 Guidance part 32 Growth suppression part 321 Flat part 32A Straight line Part 33, 34 Surface 41 Overlap Part 71 Connection Part 711 Stepped Part 712 Holding Part 80 Base Material 91, 92 Surface 100, 200 Composite Material C Crack L1, L11, L12 Slit Line L2 First Fold Line L3 Second Fold Line X First in-plane direction Y Second in-plane direction Z Out-of-plane direction

Claims (10)

第1部材と、
第2部材と、
前記第1部材と前記第2部材とを接着する接着剤を含む接着層と、
前記接着層内に配置され、前記接着層内で面内方向に向かうき裂の進展を抑制するき裂進展抑制部材と、
を備え、
前記き裂進展抑制部材は、前記第1部材側から前記第2部材側にかけて前記面内方向に凸形状を呈する進展抑制部を有し、前記接着層との界面の接着強度が前記接着層と前記第1部材および前記第2部材との界面の接着強度よりも弱いことを特徴とする接着部材。
a first member;
a second member;
an adhesive layer containing an adhesive that bonds the first member and the second member;
a crack growth suppressing member disposed in the adhesive layer and suppressing crack propagation in the in-plane direction in the adhesive layer;
with
The crack growth suppression member has a crack growth suppression portion having a convex shape in the in-plane direction from the first member side to the second member side, and the adhesive strength of the interface with the adhesive layer is the same as that of the adhesive layer. An adhesive member, wherein the adhesive strength is weaker than the adhesive strength of the interface between the first member and the second member.
前記進展抑制部は、前記凸形状を呈する湾曲部であることを特徴とする請求項1に記載の接着部材。 2. The adhesive member according to claim 1, wherein the progress suppressing portion is a curved portion presenting the convex shape. 前記き裂進展抑制部材は、前記進展抑制部の端部から前記面内方向に沿って延びる誘導部をさらに有することを特徴とする請求項1または請求項2に記載の接着部材。 3. The adhesive member according to claim 1, wherein the crack growth suppressing member further has a guiding portion extending along the in-plane direction from an end portion of the crack growth suppressing portion. 前記き裂進展抑制部材は、前記面内方向に沿って複数配置されることを特徴とする請求項1から請求項3のいずれか一項に記載の接着部材。 The bonding member according to any one of claims 1 to 3, wherein a plurality of crack growth suppression members are arranged along the in-plane direction. 隣り合う前記き裂進展抑制部材の少なくとも一部は、前記進展抑制部の前記凸形状が互いに反対方向を向いて配置されることを特徴とする請求項4に記載の接着部材。 5. The adhesive member according to claim 4, wherein at least some of the adjacent crack growth suppression members are arranged such that the convex shapes of the crack growth suppression portions face opposite directions to each other. 前記き裂進展抑制部材は、前記進展抑制部が環状に連続して形成されることを特徴とする請求項1から請求項4のいずれか一項に記載の接着部材。 The bonding member according to any one of claims 1 to 4, wherein the crack growth suppressing member is formed such that the crack growth suppressing portion is continuously formed in an annular shape. 前記き裂進展抑制部材は、連結部を介して複数が連結されていることを特徴とする請求項4に記載の接着部材。 5. The adhesive member according to claim 4, wherein a plurality of said crack growth suppressing members are connected via a connecting portion. 第1部材を準備する第1部材準備ステップと、
第2部材を準備する第2部材準備ステップと、
前記第1部材と前記第2部材とを接着剤を含む接着層により接着する接着ステップと、
を備え、
前記接着層内には、前記接着層内で面内方向に向かうき裂の進展を抑制するき裂進展抑制部材が配置されており、
前記き裂進展抑制部材は、前記第1部材側から前記第2部材側にかけて前記面内方向に凸形状を呈する進展抑制部を有し、前記接着層との界面の接着強度が前記接着層と前記第1部材および前記第2部材との界面の接着強度よりも弱いことを特徴とする接着部材の形成方法。
a first member preparing step of preparing a first member;
a second member preparation step of preparing a second member;
a bonding step of bonding the first member and the second member with an adhesive layer containing an adhesive;
with
A crack growth suppression member is arranged in the adhesive layer to suppress the propagation of a crack in the in-plane direction in the adhesive layer,
The crack growth suppression member has a crack growth suppression portion having a convex shape in the in-plane direction from the first member side to the second member side, and the adhesive strength of the interface with the adhesive layer is the same as that of the adhesive layer. A method of forming an adhesive member, wherein the adhesion strength of the interface between the first member and the second member is weaker than that of the interface.
第1部材と第2部材とを接着する接着剤を含む接着層を形成する接着層の形成方法であって、
基材を複数の切り込み線に沿って切り込み、複数の折り曲げ線に沿って折り曲げて、前記接着層内で面内方向に向かうき裂の進展を抑制するき裂進展抑制部材を、連結部を介して複数連結して形成し、前記き裂進展抑制部材に前記接着剤を含む樹脂を含浸して前記接着層を形成し、
前記き裂進展抑制部材は、前記第1部材側から前記第2部材側にかけて面内方向に凸形状を呈する進展抑制部を有し、前記接着層との界面の接着強度が前記接着層と前記第1部材および前記第2部材との界面の接着強度よりも弱いことを特徴とする接着層の形成方法。
A method for forming an adhesive layer for forming an adhesive layer containing an adhesive for bonding a first member and a second member, comprising:
The base material is cut along a plurality of cut lines and folded along a plurality of folding lines, and a crack growth suppressing member that suppresses the propagation of cracks in the in-plane direction in the adhesive layer is applied via the connecting portion. forming the crack growth suppression member by impregnating the resin containing the adhesive to form the adhesive layer,
The crack growth suppression member has a crack growth suppression portion having a convex shape in the in-plane direction from the first member side to the second member side, and the adhesive strength of the interface with the adhesive layer is the same as that of the adhesive layer. A method of forming an adhesive layer, wherein the adhesion strength of the interface between the first member and the second member is weaker than that of the interface.
第1部材と第2部材とを接着する接着剤を含む接着層を形成する接着層の形成方法であって、
前記接着層内で面内方向に向かうき裂の進展を抑制するき裂進展抑制部材の周囲に、前記接着剤を含む複数のフィルム状部材を接着して前記接着層を形成し、
前記き裂進展抑制部材は、前記第1部材側から前記第2部材側にかけて前記面内方向に凸形状を呈する進展抑制部を有し、前記接着層との界面の接着強度が前記接着層と前記第1部材および前記第2部材との界面の接着強度よりも弱いことを特徴とする接着層の形成方法。
A method for forming an adhesive layer for forming an adhesive layer containing an adhesive for bonding a first member and a second member, comprising:
forming the adhesive layer by adhering a plurality of film-like members containing the adhesive around the crack growth suppression member that suppresses the propagation of cracks in the in-plane direction in the adhesive layer;
The crack growth suppression member has a crack growth suppression portion having a convex shape in the in-plane direction from the first member side to the second member side, and the adhesive strength of the interface with the adhesive layer is the same as that of the adhesive layer. A method of forming an adhesive layer, wherein the adhesive strength is weaker than the adhesive strength of the interface between the first member and the second member.
JP2019082173A 2019-04-23 2019-04-23 Adhesive member, method for forming adhesive member, and method for forming adhesive layer Active JP7187378B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2019082173A JP7187378B2 (en) 2019-04-23 2019-04-23 Adhesive member, method for forming adhesive member, and method for forming adhesive layer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2019082173A JP7187378B2 (en) 2019-04-23 2019-04-23 Adhesive member, method for forming adhesive member, and method for forming adhesive layer

Publications (2)

Publication Number Publication Date
JP2020180626A JP2020180626A (en) 2020-11-05
JP7187378B2 true JP7187378B2 (en) 2022-12-12

Family

ID=73023768

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2019082173A Active JP7187378B2 (en) 2019-04-23 2019-04-23 Adhesive member, method for forming adhesive member, and method for forming adhesive layer

Country Status (1)

Country Link
JP (1) JP7187378B2 (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004262669A (en) 2003-01-14 2004-09-24 Ngk Insulators Ltd Ceramic honeycomb structure and its manufacturing method
JP2006282046A (en) 2005-04-01 2006-10-19 Kawasaki Heavy Ind Ltd Separation development prevention structure of sandwich panel
JP2009083551A (en) 2007-09-27 2009-04-23 Society Of Japanese Aerospace Co Inc Crack extension preventive structure of sandwich panel
WO2016129570A1 (en) 2015-02-13 2016-08-18 国立大学法人東京大学 Bonded structure

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0228046Y2 (en) * 1984-12-03 1990-07-27

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004262669A (en) 2003-01-14 2004-09-24 Ngk Insulators Ltd Ceramic honeycomb structure and its manufacturing method
JP2006282046A (en) 2005-04-01 2006-10-19 Kawasaki Heavy Ind Ltd Separation development prevention structure of sandwich panel
JP2009083551A (en) 2007-09-27 2009-04-23 Society Of Japanese Aerospace Co Inc Crack extension preventive structure of sandwich panel
WO2016129570A1 (en) 2015-02-13 2016-08-18 国立大学法人東京大学 Bonded structure

Also Published As

Publication number Publication date
JP2020180626A (en) 2020-11-05

Similar Documents

Publication Publication Date Title
US6544366B2 (en) Composite member having increased resistance to delamination and method of making same
US8992709B2 (en) Sandwich structure having arrestment feature and method of making the same
US20100296942A1 (en) Reinforced composite aerofoil blade
KR20110008201A (en) Composite laminate with self-healing layer
JP6448628B2 (en) Composite panel for floor or wall covering parts and method for manufacturing such a panel
JP6583966B2 (en) Panel made of laminate and method for producing the same
KR20120098433A (en) Bonding structure of fiber-reinforced resin and metal and bonding method of fiber-reinforced resin and metal
EP3018293A1 (en) Composite article with fibre-reinforced sandwich core
JP2020524230A (en) CROSS WAP MULTILAYER FIBER BATT, AND METHOD FOR PRODUCING THE CROSS WRAP MULTILAYER FIBER BATT
US11718063B2 (en) Splice joint in laminate composite structure
US11845236B2 (en) Composite structure splice and method
CN105667756A (en) Composite Blade Stringer Edge Protection and Visual Damage Indication
JP2010524767A (en) Fiber metal laminate panel
JP7187378B2 (en) Adhesive member, method for forming adhesive member, and method for forming adhesive layer
WO2019044161A1 (en) Composite material structure
EP3991955A1 (en) Composite component system, use of a composite component system and method for repairing a composite component system
WO2016129570A1 (en) Bonded structure
WO2022144998A1 (en) Layered body structure and method for manufacturing layered body structure
JP2020175626A (en) Fiber-reinforced plastic body and connection members

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20211224

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20221024

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20221101

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20221130

R150 Certificate of patent or registration of utility model

Ref document number: 7187378

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150