Continuous fabrication of parts using in-feed spools of fiber reinforced thermoplastic
AssigneeThe Boeing Company
InventorsAlexander M. Rubin, James R. Fox, Randall D. Wilkerson
Life of this patent
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AssigneeThe Boeing Company
InventorsAlexander M. Rubin, James R. Fox, Randall D. Wilkerson
Estimating the term…
Thermoplastic composite laminate parts with tailored and varying thickness and/or curved sections are manufactured in a continuous process. Automated equipment or hand lay-up is used to collate parts or components into a multi-layer stack. Each stack contains all plies, including ply build-up areas, tacked in the proper location to maintain orientation and location. Some or all of the plies may be continuously fed from spools of single or multiply ply material. Ply consolidation tooling contains all necessary part features and is coordinated to the customized multiple ply stacks to form a single integrated thermoplastic composite laminate potentially having areas of differing thickness from the multiple ply stacks.
A method comprising:
A method of manufacturing a reinforced thermoplastic or laminate part in a continuous compression molding process, comprising the steps of:
Dependencies are inferred from the claim text.