B - Operations – Transporting – 29 – C
Patent
B - Operations, Transporting
29
C
B29C 53/04 (2006.01) B32B 3/12 (2006.01)
Patent
CA 2213795
A process for bending a thermoplastic skinned honeycomb core panel includes clamping a planar portion of the panel to hold the panel against movement parallel to the plane of the planar portion. A linear band of a face sheet on one side of the panel is heated to soften resin and disbond adhesive holding the face sheet to the honeycomb core. The heat is removed, forming a bubble separated from the core. A distal leg of the panel is bent around a heated anvil along an axis parallel to the linear band to form a bend having an inside radius. The bubble collapses around the inside radius and forms an overlapping flap of face sheet. The flap is pressed in a fold between the anvil and the bent leg of the panel, and the leg is held in the bent position while resin in the flap solidifies.
Banks David P.
Olive Ronald M.
Struve Richard G.
Van Laeken Howard J.
Wilde Rinhold E.
Bull Housser & Tupper Llp
The Boeing Company
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