Methods of stamp-forming fiber-reinforced thermoplastic composite assemblies and related systems
AssigneeThe Boeing Company
InventorAdriana W. Blom-Schieber
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AssigneeThe Boeing Company
InventorAdriana W. Blom-Schieber
Estimating the term…
Stamp-forming a composite assembly includes applying a low-melt film on an interface surface of at least one spar, loading the spar onto at least one tooling segment such that the interface surface is exposed, and heating the tooling segment to a first temperature that is above a crystallization temperature of the low-melt film and below a melt temperature of a resin of the spar. A second low-melt film may be applied on a fiber-reinforced thermoplastic skin blank, and the skin blank is heated to a second temperature above a melt temperature of a resin of the skin blank. The skin blank is then draped around the tooling segment such that at least some of any second low-melt film contacts the low-melt film on the interface surface of the spar. The stamp press is then closed to co-consolidate the skin blank and the spar, thereby stamp-forming the composite assembly.
A method of stamp-forming a fiber-reinforced thermoplastic composite assembly, the method comprising:
Dependencies are inferred from the claim text.