The application relates to the technical field of
aviation equipment maintenance, and particularly discloses an aircraft wing carbon
fiber skin ultrasonic automatic scanning
system and method, which comprises a movable gantry frame and an industrial mechanical arm. The movable gantry frame comprises a plurality of stands and two
bed bodies, the plurality of stands are respectively arranged at the bottom ends of the two
bed bodies, the top portions of the two
bed bodies are jointly provided with a movable cross beam, the top portion of the movable cross beam is provided with a horizontal sliding table, the top portion of the horizontal sliding table is provided with a vertical sliding
saddle, the industrial mechanical arm is arranged at the bottom end of the vertical sliding
saddle, the bottom end of the industrial mechanical arm is provided with a scanning probe, a limiting mechanism and a transfer trolley are arranged below the movable cross beam, and a control box is arranged below one of the bed bodies. In the application, the automatic lifting type automatic loading and unloading of the
composite material wing component is realized through the
automatic control technical means of the detection rack and the movable platform, the manual lifting risk is reduced, the labor intensity of the personnel is greatly reduced, and the risk of occupational diseases is reduced.