The invention relates to the technical field of aircraft part
processing, testing or inspection and the like, and provides an aircraft aluminum
alloy plate aging evaluation method based on an
equivalent circuit model, and the method comprises the following steps: collecting electrochemical impedance spectrums of samples with different
exposure age limits, and extracting electrochemical
impedance spectrum characteristics of the samples; establishing an
equivalent circuit model comprising solution resistance,
coating resistance,
coating capacitance, Warburg impedance,
anodic oxide film
charge transfer resistance, interface
capacitance, aluminum
alloy matrix
charge transfer resistance, interface electric double-layer
capacitance,
inductance and corresponding resistance of the
inductance based on the characteristics, wherein the
equivalent circuit model comprises the solution resistance, the
coating resistance, the coating capacitance, the Warburg impedance, the
anodic oxide film
charge transfer resistance, the interface capacitance, the aluminum
alloy matrix charge transfer resistance and the interface electric double-layer capacitance; and analyzing a resistance curve and a capacitance curve obtained by fitting the model to complete the evaluation of the
corrosion and aging degree. According to the method, systematicness and accuracy of aging evaluation are improved, an electrochemical mechanism in the
corrosion process can be disclosed,
time correlation modeling of the aging process can be achieved, and the method is suitable for long-term service
performance monitoring and service life prediction of the
aviation aluminum alloy structure.