Comparative multiscale evaluation of the temperature-dependent interfacial strength in aluminum alloy/carbon fiber-reinforced thermoplastic joints

Lightweight structural systems increasingly rely on dissimilar joints between aluminum alloys and carbon fiber-reinforced thermoplastics (CFRTPs); however, their mechanical reliability remains highly sensitive to the bonding temperature and the length scale of fracture. In this study, a comparative multiscale framework was established to elucidate the temperature-dependent evolution of strength and fracture mechanisms in dissimilar 6061 aluminum alloy (A6061)/polyamide 6 (PA6)-CFRTP joints. A6061 surfaces were nanostructured via hydrochloric acid etching to enhance mechanical interlocking, and thermocompression bonding was performed at temperatures ranging from 230 to 350 °C. Mechanical characterization was conducted across three scales: macroscopic tensile-shear, sub-millimeter-scale miniature tensile, and microscale tensile testing. These were complemented by thermal analysis, microscopy, X-ray nano-computed tomography, and nanoindentation. The tensile-shear strength increased moderately from near the melting point of PA6 to approximately 330 °C (reaching ≈ 8 kN), but declined to ∼ 6 kN at 350 °C. Cross-sectional observations revealed numerous voids within ∼ 1 mm of the interface above 300 °C, which was consistent with the onset of thermal decomposition of PA6. Miniature-scale specimens exhibited an earlier onset of strength loss than joint-scale specimens, which was attributed to void-induced stress concentration under a loading axis nearly perpendicular to the in-plane fiber orientation. Microtensile tests were used to isolate the intrinsic degradation region of PA6 adjacent to the interface. Nanoindentation confirmed a near-interfacial hardness reduction of ≈ 200 MPa at 350 °C. These findings elucidate the scale-dependent and temperature-driven fracture transition from interfacial to CFRTP-side failure and define an optimized process window.

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Publication Details

Journal
Composites Part B Engineering
Published
2026-03-13
DOI
https://doi.org/10.1016/j.compositesb.2026.113607
Primary Topic
Mechanical Behavior of Composites
Type
article
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article

Comparative multiscale evaluation of the temperature-dependent interfacial strength in aluminum alloy/carbon fiber-reinforced thermoplastic joints

Akihisa Takeuchi, Tomokazu Sano, Akio Hirose, Masahiro Yasutake et al.
Composites Part B Engineering
Mechanical Behavior of Composites
article

Comparative multiscale evaluation of the temperature-dependent interfacial strength in aluminum alloy/carbon fiber-reinforced thermoplastic joints

Akihisa Takeuchi, Tomokazu Sano, Akio Hirose, Masahiro Yasutake, Kentaro Uesugi, Tomoki Matsuda, Ren Sato, Kazuma Shimizu
article en

Abstract

Lightweight structural systems increasingly rely on dissimilar joints between aluminum alloys and carbon fiber-reinforced thermoplastics (CFRTPs); however, their mechanical reliability remains highly sensitive to the bonding temperature and the length scale of fracture. In this study, a comparative multiscale framework was established to elucidate the temperature-dependent evolution of strength and fracture mechanisms in dissimilar 6061 aluminum alloy (A6061)/polyamide 6 (PA6)-CFRTP joints. A6061 surfaces were nanostructured via hydrochloric acid etching to enhance mechanical interlocking, and thermocompression bonding was performed at temperatures ranging from 230 to 350 °C. Mechanical characterization was conducted across three scales: macroscopic tensile-shear, sub-millimeter-scale miniature tensile, and microscale tensile testing. These were complemented by thermal analysis, microscopy, X-ray nano-computed tomography, and nanoindentation. The tensile-shear strength increased moderately from near the melting point of PA6 to approximately 330 °C (reaching ≈ 8 kN), but declined to ∼ 6 kN at 350 °C. Cross-sectional observations revealed numerous voids within ∼ 1 mm of the interface above 300 °C, which was consistent with the onset of thermal decomposition of PA6. Miniature-scale specimens exhibited an earlier onset of strength loss than joint-scale specimens, which was attributed to void-induced stress concentration under a loading axis nearly perpendicular to the in-plane fiber orientation. Microtensile tests were used to isolate the intrinsic degradation region of PA6 adjacent to the interface. Nanoindentation confirmed a near-interfacial hardness reduction of ≈ 200 MPa at 350 °C. These findings elucidate the scale-dependent and temperature-driven fracture transition from interfacial to CFRTP-side failure and define an optimized process window.

Composites Part B EngineeringVol. 318
SPring-8 (JP), Japan Synchrotron Radiation Research Institute (JP), The University of Osaka (JP)
Openalex Percentile: Top 22%
Mechanical Behavior of Composites
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