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Abstract
Adhesion is a technology for assembling carbon fiber (CF) reinforced polymer (CFRP), enabling them to maintain their lightweight and high-stiffness properties. Despite the importance of adhesion, the lack of a molecular-level understanding of the adhesion mechanisms has limited the reliability of adhesion for use in next-generation aircraft and automobiles. Here, we focused on the chemical-state distribution at a practical adhesive interface composed of an epoxy-based adhesive film bonded to an epoxy-based CF matrix. By fluorinating the OH group, we succeeded in visualizing the chemical state at the CF-matrix/adhesive interface using soft X-ray microscopy. The soft X-ray images exhibited a decrease in OH-related signals at the interface due to the local chemical interaction at the epoxy-epoxy adhesive interface. We also found that the N and O Kα signals were observable at the CF's surface, indicating the presence of nitrogen- and oxygen-containing functional groups. Based on these observations, we discuss the molecular-level adhesion mechanism at the CF-matrix/adhesive interface.
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1 RIKEN SPring-8 Center, RIKEN, Sayo, Japan (GRID:grid.472717.0); Photon Science Innovation Center, NanoTerasu, Sendai, Japan (GRID:grid.472717.0)
2 RIKEN SPring-8 Center, RIKEN, Sayo, Japan (GRID:grid.472717.0)
3 Mitsubishi Heavy Industries, Ltd., Chemical Research Department, Research and Innovation Center, Yokohama, Japan (GRID:grid.471153.5) (ISNI:0000 0001 2180 8453)
4 RIKEN SPring-8 Center, RIKEN, Sayo, Japan (GRID:grid.472717.0); Protein Crystal Analysis Division, JASRI, Sayo, Japan (GRID:grid.410592.b) (ISNI:0000 0001 2170 091X)
5 Mitsubishi Heavy Industries, Ltd., Manufacturing Technology Research Department, Research and Innovation Center, Nagoya, Japan (GRID:grid.471153.5) (ISNI:0000 0001 2180 8453)
6 Mitsubishi Heavy Industries, Ltd., Fixed Wing Aircraft Engineering Department, Integrated Defense and Space Systems, Nishikasugai, Japan (GRID:grid.471153.5) (ISNI:0000 0001 2180 8453)