Semi-conformable pressure application system and method for joining composite parts
AssigneeSpirit AeroSystems, Inc.
InventorKerrick Robert Dando
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AssigneeSpirit AeroSystems, Inc.
InventorKerrick Robert Dando
Estimating the term…
A system and method for fusing at least two thermoplastic composite components together may include placing faying surfaces of the thermoplastic composite components in contact with each other, placing a separation layer over and against one of the thermoplastic composite components, and placing a multi-layer composite pressure pad over and in contact with the separation layer. The method may also include placing an activated inductor against the multi-layer composite pressure pad for induction welding the two thermoplastic composite components to each other. The thermoplastic composite components may comprise conductive fibers while the multi-layer composite pressure pad may comprise a first layer and a second layer with non-conductive fibers. The first layer may at least partially melt during induction welding of the two thermoplastic composite components while the second layer may remain rigid throughout this welding.
A system for fusing at least two thermoplastic composite components together, the system comprising:
A method for fusing at least two thermoplastic composite components together, the method comprising:
A method for step-welding at least two thermoplastic composite components together, the method comprising:
Dependencies are inferred from the claim text.