Method of joining composite honeycomb sections

Metal working – Method of mechanical manufacture – Assembling or joining

Reexamination Certificate

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Details

C029S514000, C261S112200

Reexamination Certificate

active

07954224

ABSTRACT:
The invention includes a method of joining edges of adjacent honeycomb core panel sections. In one embodiment, the method includes forming a first edge along a first cellular core panel section. The first edge includes a first plurality of edge cell walls along the first edge. The method further includes forming a second edge along a second cellular core panel section, wherein the second edge includes a second plurality of edge cell walls along the second edge. The first edge is positioned proximate to the second edge. At least a portion of at least one of the first plurality of edge cell walls is mechanically interlocked with at least a portion of at least one of the second plurality of edge cell walls to form a joint therebetween. The invention also includes a composite structure at least partially produced by such a method.

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European Extended Search Report (EP Appln. No. 07014222.9, filed Jul. 19, 2007) mailed Feb. 4, 2011, pp. 1-6.

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