Autonomic healing of carbon fiber/epoxy interfaces
Amanda R Jones1, Alicia Cintora, Scott R White
1Department of Mechanical Science and Engineering, ‡Department of Material Science and Engineering, §Department of Aerospace Engineering, and ⊥Beckman Institute of Science and Technology, University of Illinois at Urbana-Champaign.
Abstract:
A maximum of 91% recovery of interfacial shear strength (IFSS) is achieved for carbon fiber/epoxy interfaces functionalized with capsules containing reactive epoxy resin and ethyl phenyl acetate (EPA). We find a binder is necessary to improve the retention of capsules on the carbon fiber surface. Two different methods for applying the binder to the carbon fiber surface are investigated. Healing efficiency is assessed by recovery of IFSS of a single functionalized fiber embedded in a microdroplet of epoxy. Debonding of the fiber/matrix interface ruptures the capsules, releasing resin and EPA solvent into the crack plane. The solvent swells the matrix, initiating transport of residual amine functionality from the matrix for further curing with the epoxy resin delivered to the crack plane. The two binder protocols produce comparable results, both yielding higher recovery of IFSS than samples prepared without a binder.
