CFRP接着構造の強度を数値解析で予測するマルチスケール解析モデルを構築 ―航空機構造の軽量化に向けた接着剤設計の効率化へ―

2026-06-26 東北大学

東北大学の研究グループは、航空機などに用いられるCFRP(炭素繊維強化プラスチック)接着構造の強度を高精度に予測できるマルチスケール解析モデルを開発した。航空機の軽量化には、ボルトやリベットによる機械的締結を減らし、接着剤による接合を活用することが期待されているが、接着剤に添加するゴム粒子などの改質剤が強度やじん性に及ぼす影響は予測が難しく、従来は試作と実験を繰り返して最適条件を決めていた。本研究では、改質剤周辺で発生する微視的な損傷や変形と、CFRP接着構造全体の破壊挙動を結び付けるマルチスケール解析モデルを構築し、改質剤の添加によって接着剤のじん性が向上し、接着構造全体の強度が高まるメカニズムを実験と数値解析の両面から明らかにした。この成果は、接着剤設計の試行錯誤を大幅に削減するとともに、高信頼性・軽量な航空機構造や輸送機器の効率的な設計・開発への応用が期待される。

CFRP接着構造の強度を数値解析で予測するマルチスケール解析モデルを構築 ―航空機構造の軽量化に向けた接着剤設計の効率化へ―
図1. 本研究で実施した接着強度試験。破壊後の接着面にはCSR粒子の痕がみられる。

<関連情報>

微視的損傷モデルに基づく熱硬化性樹脂の強化に関するマルチスケールモデリング:接着CFRP構造への応用 Multiscale modeling of toughening in thermosetting resins based on a microscopic damage model: Application to bonded CFRP structures

Yamato Hoshikawa, Sera Koo, Yoshiaki Kawagoe, Shoko Mishima, Kazuki Ryuzono, Tomonaga Okabe
International Journal of Solids and Structures  Available online: 15 June 2026
DOI:https://doi.org/10.1016/j.ijsolstr.2026.114159

Highlights

  • SLS strength of thermosetting resin reinforced with CSR particles was investigated.
  • Bottom-up multiscale analysis demonstrated the underlying strengthening mechanism.
  • Top-down analysis elucidated fracture processes around CSR particles in SLS tests.

Abstract

In this study, the toughening mechanisms induced by the addition of nanoparticles to an epoxy resin were modeled using a multiscale modeling framework, and a strategy was proposed to predict the bonding strength of structural adhesives containing toughening agents. An epoxy adhesive modified with core–shell rubber (CSR) particles was investigated through tensile and compressive tests of the resin and single-lap shear (SLS) tests using carbon-fiber-reinforced plastic (CFRP) adherends. The experimental results demonstrated a significant improvement in SLS strength despite reductions in the resin stiffness and strength, with the maximum shear strength observed at 5 wt% CSR content.

To elucidate the underlying strengthening mechanism, a bottom-up multiscale analysis was conducted by combining a microscale continuous damage mechanics (CDM) model with a macroscale enhanced smeared crack model (SCM). At the microscale, void growth and plastic deformation in the epoxy matrix surrounding CSR particles were modeled using periodic unit cell (PUC) analysis. The resulting homogenized elastic–plastic properties and fracture toughness were incorporated into a macroscale finite element model of the SLS test. Furthermore, a top-down approach was employed to map the macroscopic strain history within the adhesive layer onto the microscale analysis, enabling a detailed evaluation of the process zone formation. The proposed framework reasonably captured the overall changes in the stress–strain response of the resin and the SLS strength associated with CSR addition. The results demonstrated that the toughness enhancement was primarily governed by plastic deformation and void coalescence in the epoxy matrix.

These findings establish a methodology for predicting the mechanical properties that explicitly accounts for inclusion-induced toughening mechanisms in adhesives, thereby contributing to the development of tailored adhesive design strategies for bonded structures.

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