The invention relates to a method for treating an interface between a resin-based
composite material and an
aviation alloy. The method comprises the following steps: firstly,
processing a micro inverted taper hole in a to-be-bonded surface of an
alloy, then carrying out surface treatment, then
coating a
thermoplastic elastic adhesive on the to-be-bonded surface, putting the to-be-bonded surface into a vacuum oven for treatment, taking out the to-be-bonded surface, and carrying out heating, pressurizing and co-curing with a
composite material. The micro inverted cone hole can remarkably increase the bonding area of the resin-based
composite material and the
alloy, and the inverted cone structure can effectively prevent debonding caused by mismatching of
thermal expansion coefficients of an
adhesive and a
metal interface in the temperature change process; the
thermal expansion coefficient of the
thermoplastic elastic adhesive is between the
thermal expansion coefficient of the resin-based composite material and the thermal expansion coefficient of the alloy material, the
thermoplastic elastic adhesive has certain flexibility, a buffer layer is formed between the
fiber-reinforced resin-based composite material and an alloy interface through the
adhesive, and the probability that in the cooling process of the
fiber-reinforced resin-based composite material and the alloy, the thermal expansion coefficient of the
fiber-reinforced resin-based composite material and the alloy is lowered can be effectively lowered. And the interface
thermal residual stress is caused due to the large difference between the thermal expansion coefficients of the two.