Methods, systems, and header structures for tooling fixture and post-cure fixture calibration
AssigneeThe Boeing Company
InventorClifford D. Borowicz
Life of this patent
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AssigneeThe Boeing Company
InventorClifford D. Borowicz
Estimating the term…
Systems and methods provide for the determination and correction of tooling deviation by comparing two different three-dimensional surface scans of a composite panel after curing. Such methods and systems may allow for less accurate post-cure fixturing (e.g., holding the panel in a less constrained state, as compared to prior art techniques), while still maintaining a sufficient amount of precision for predictive shimming and shimless techniques. Methods include performing a first three-dimensional surface scan, performing a second three-dimensional surface scan, and comparing the two to determine a deformation function corresponding to tooling deviation. In some systems, a header structure is used to hold the composite panel in a nominal configuration for the second three-dimensional surface scan. In some systems, scanning devices perform mirrored scanning on either side of the composite panel, using a common reference frame.
A method of tooling fixture calibration for determining deviation introduced into a panel during manufacturing, wherein the panel comprises an outer surface and an inner surface, the method comprising:
Dependencies are inferred from the claim text.