Method for correcting hole sites on basis of framework scanning measurement
A hole position and skeleton technology, which is applied in the field of hole position correction based on skeleton scanning measurement, can solve problems such as the inability to measure the distance between the hole position of the wall plate and the edge of the skeleton, the failure to meet the requirements of the hole making process, the deformation of the wing skeleton and the wall plate, etc. , to achieve the effect of solving the difficult measurement of edge distance, improving the efficiency of hole making and high degree of automation
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[0044] The present invention will be described in detail below in conjunction with specific embodiments.
[0045] The hole position correction method based on skeleton scanning measurement in this embodiment relies on the following aircraft automatic assembly system for implementation. Before correcting the hole position, the following preparatory work should be carried out:
[0046] Lift the skeleton of the wing of the aircraft to the positioning tool;
[0047] Connect the measurement control computer, measurement automation interface box, and laser tracker, adjust the direction of the laser tracker to capture and lock the laser scanner, establish a complete measurement data transmission channel, and prepare for scanning measurement;
[0048] Set the scanning route to the CNC machine tool through the control system. The scanning path is based on the principle of reducing redundant measurement data and avoiding space obstacles, and can scan the skeleton completely.
[0049] A...
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