Appeal No. 1996-2703 Application 08/339,637 comprise at least about 10 wt% of the composition (col. 2, line 69 - col. 3, line 12). Fell discloses an adhesive for use on the face sheets of honeycomb sandwich panels in applications such as aerospace assemblies (col. 1, lines 17-24). Fell teaches that the curing time of thermosetting resins such as epoxy resins generally is several hours, and that the cycle time for bonding face sheets to honeycomb cores can be reduced to only seconds by use of a thermoplastic adhesive or an adhesive generally containing no more than about 20 wt% thermosetting resin, the remainder being thermoplastic resin (col. 1, lines 23-24 and 33-43; col. 3, lines 15-27; col. 3, line 66 - col. 4, line 2). Lynam discloses that when honeycomb sandwich panels are made for applications such as aircraft assemblies, forming adhesive fillets at the junctions of the facing panels and the honeycomb cores increases the bond strength because the bonding area extends beyond the edges of the core material up the walls of the cells and partially onto the inner face of the panels (col. 1, lines 7-20 and 30-35). The adhesive may 5Page: Previous 1 2 3 4 5 6 7 8 9 10 NextLast modified: November 3, 2007