Gap filling for thermoplastic welds
AssigneeThe Boeing Company
InventorsRobert C. Anderson, Stephen Christensen, Todd R. Peterson
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AssigneeThe Boeing Company
InventorsRobert C. Anderson, Stephen Christensen, Todd R. Peterson
Estimating the term…
Thermoplastic welding is an emerging technology targeted at significantly reducing the cast of manufacture of aerospace structure by eliminating fasteners and the touch labor associated with fasteners to prepare, install, and inspect the assemblies. Thermoplastic welds, however, suffer from significant residual tensile strain caused by differences in the coefficient of thermal expansion between the carbon fiber reinforced composite laminates and the unreinforced weld. Holding fiber reinforcement to the weld using a structural susceptor which is a laminate of alternating layers of thermoplastic resin and fiber reinforcement sandwiching a conventional metal susceptor alleviates this strain. The structural susceptor can be peeled in selected locations to fill the gap between the laminates, eliminating costly profilometry of the faying surfaces and the associated problem of resin depletion where machining occurred to match the faying surfaces. The peeled susceptor is complementary in contour to the gap it will fill.
A method for thermoplastic welding to join two fiber-reinforced composite laminates with a susceptor encased in a thermoplastic resin, comprising the steps of:
A method for filling gaps along a bondline between faying surfaces of fiber-reinforced resin composite laminates prior to their joined with a thermoplastic weld, the weld containing a susceptor having metal sheet encased in fiber-reinforced, thermoplastic resin, the method comprising the steps of:
A method for thermoplastic welding to join at least two prefabricated resin composite laminates using a susceptor along a bondline, the susceptor being capable of heating to a temperature at which a welding resin in the bondline melts, comprising the steps of:
Dependencies are inferred from the claim text.