Digitizing correction method for aircraft panel assembling deformation based on triaxial numerical control locator
A technology of numerical control positioner and aircraft panel, which is applied in the field of digital correction and assembly deformation of aircraft panel, to reduce assembly stress and improve assembly quality
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[0082] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments.
[0083] Such as figure 1 As shown, a large aircraft panel 1 is mainly composed of a skin 2, a stringer 3, a bulkhead 4, and a corner piece 5.
[0084] Such as figure 2 As shown in the figure, the process joint 6 of a large aircraft panel is mainly composed of a process ball joint 7 and a joint body 8 .
[0085] Such as image 3 As shown, the three-axis numerical control positioner 9 includes an X-direction movement axis 10, a Y-direction movement axis 11, and a Z-direction movement axis 12, each of which moves independently, and is manipulated and controlled by a control system computer 14. (wherein the coordinate system formed by the X-direction movement axis 10, the Y-direction movement axis 11, and the Z-direction movement axis 12 is as follows image 3 and Figure 4 shown. )
[0086] The process ball head 7 is spherically hinged at...
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