The utility model discloses an aircraft panel structure
stringer overturning tool which comprises an overturning tool body, a first shaft body, a
stringer body and placing frames, the placing frames are arranged at the two ends of the interior of the overturning tool body through the first shaft body and a second shaft body respectively, and six-dimensional force sensors are arranged on the first shaft body and the second shaft body respectively. The turnover tool comprises a turnover tool body, a plurality of containing frames are arranged on the turnover tool body, a
stringer body is arranged between the containing frames, adjusting grooves are formed in the two sides of the lower portion of the turnover tool body correspondingly, lead screws are arranged in the adjusting grooves correspondingly, the lead screws are sleeved with driving blocks correspondingly, and balancing weights are arranged at the top ends of the driving blocks correspondingly. The turnover tool body, the stringer body, the placing frame, the first shaft body, the driving motor, the second shaft body, the six-dimensional
force sensor, the adjusting groove, the lead screw, the
servo motor, the driving block and the balancing weight are installed, the moment of force of the balancing weight to the turnover tool body can be changed by adjusting the horizontal position of the balancing weight, and the turnover tool body is kept balanced.