Method and system for wing-to-body joining
A joint method, wing technology, applied in the general control system, control/regulation system, fuselage, etc., can solve the problems of heavy, time-consuming gaskets, etc.
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[0021] Wing-to-body joining methods and systems according to the present disclosure allow for faster and more certain wing-to-body assembly of aircraft and assembly of other large structures. The method involves measuring the 3D (three-dimensional) locations of optical targets at the interface to be joined (eg, the aircraft's wing root and wing stub) and using these locations to track the position of the wing and body. The location of the optical target on the constructed interface can be determined by scanning the interface to generate a surface profile of the interface to identify the location of the optical target. The wings can move to the body in at least two stages with a series of waypoints. In the first stage, the wings and body are moved far enough apart to avoid contact between the parts as much as possible. The position of the airfoil at each waypoint is determined by measuring objects on the airfoil. The error between the actual position and the desired position ...
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