Abstract:
A composite sandwich structure which includes upper and lower skin structures (20, 22), first and second honeycomb core structures (24, 26), and an intermediate portion disposed between the first and second honeycomb core structures. The intermediate portion comprises a composite laminate (30), a barrier member (32) and a foaming adhesive layer (34) disposed between the composite laminate and the barrier member. The foaming adhesive layer is of a type designed to expand when exposed to an elevated temperature. The composite laminate and the barrier member operate to limit the expansion of the foaming adhesive layer into the open cells of the first and second honeycomb core structures. The foaming adhesive layer, upon expansion, applies pressure against the composite laminate. This pressure, acting concomitantly with the applied curing pressure and the elevated temperature, cures the laminate. Furthermore, the expansion of the foaming adhesive urges the composite laminate and the barrier member apart so as to fill any core discrepancies, i.e., mistrimmed or damaged core, thay may exist in the honeycomb core structures.
Abstract:
A duct cover (12) for use with a duct (4) within a vehicle, the duct cover (12) operative for directing a fluid flow. The duct cover being further operative for minimizing the entrance of foreign object debris into the duct (4). The duct cover (12) has a flow directing honeycomb portion (16) for conducting the passing fluid flow in a preferred direction. The flow directing honeycomb (16) comprises an array of continuous, polygon shaped open cells (20) which are biased with respect to the initial fluid flow direction. The periphery (17) of the flow directing honeycomb (12) is rigidized to stiffen the same for minimizing the displacements thereof. The rigidity is provided by a framing member comprising upper and lower skin structures (28, 29) affixed to a core material (30). The framing member is preferably adhesively bonded to the flow directing honeycomb (16) by means of a foaming adhesive (36) and a barrier member (38). The barrier member (38) is operative for minimizing the expansion of the foaming adhesive (36) into the open cells (20) of the honeycomb (16). In order to improve the low observability characteristics of the structure, the cells (20) of the flow directing honeycomb (16) are preferably coated with a radar absorbent material, such as carbon, which acts to minimize the amount of electromagnetic energy that is reflected therefrom.
Abstract:
A duct cover (12) for use with a duct (4) within a vehicle, the duct cover (12) operative for directing a fluid flow. The duct cover being further operative for minimizing the entrance of foreign object debris into the duct (4). The duct cover (12) has a flow directing honeycomb portion (16) for conducting the passing fluid flow in a preferred direction. The flow directing honeycomb (16) comprises an array of continuous, polygon shaped open cells (20) which are biased with respect to the initial fluid flow direction. The periphery (17) of the flow directing honeycomb (12) is rigidized to stiffen the same for minimizing the displacements thereof. The rigidity is provided by a framing member comprising upper and lower skin structures (28, 29) affixed to a core material (30). The framing member is preferably adhesively bonded to the flow directing honeycomb (16) by means of a foaming adhesive (36) and a barrier member (38). The barrier member (38) is operative for minimizing the expansion of the foaming adhesive (36) into the open cells (20) of the honeycomb (16). In order to improve the low observability characteristics of the structure, the cells (20) of the flow directing honeycomb (16) are preferably coated with a radar absorbent material, such as carbon, which acts to minimize the amount of electromagnetic energy that is reflected therefrom.
Abstract:
A composite sandwich structure which includes upper and lower skin structures (20, 22), first and second honeycomb core structures (24, 26), and an intermediate portion disposed between the first and second honeycomb core structures. The intermediate portion comprises a composite laminate (30), a barrier member (32) and a foaming adhesive layer (34) disposed between the composite laminate and the barrier member. The foaming adhesive layer is of a type designed to expand when exposed to an elevated temperature. The composite laminate and the barrier member operate to limit the expansion of the foaming adhesive layer into the open cells of the first and second honeycomb core structures. The foaming adhesive layer, upon expansion, applies pressure against the composite laminate. This pressure, acting concomitantly with the applied curing pressure and the elevated temperature, cures the laminate. Furthermore, the expansion of the foaming adhesive urges the composite laminate and the barrier member apart so as to fill any core discrepancies, i.e., mistrimmed or damaged core, thay may exist in the honeycomb core structures.
Abstract:
A composite sandwich structure which includes upper and lower skin structures (20, 22), first and second honeycomb core structures (24, 26), and an intermediate portion disposed between the first and second honeycomb core structures. The intermediate portion comprises a composite laminate (30), a barrier member (32) and a foaming adhesive layer (34) disposed between the composite laminate and the barrier member. The foaming adhesive layer is of a type designed to expand when exposed to an elevated temperature. The composite laminate and the barrier member operate to limit the expansion of the foaming adhesive layer into the open cells of the first and second honeycomb core structures. The foaming adhesive layer, upon expansion, applies pressure against the composite laminate. This pressure, acting concomitantly with the applied curing pressure and the elevated temperature, cures the laminate. Furthermore, the expansion of the foaming adhesive urges the composite laminate and the barrier member apart so as to fill any core discrepancies, i.e., mistrimmed or damaged core, thay may exist in the honeycomb core structures.
Abstract:
A duct cover (12) for use with a duct (4) within a vehicle, the duct cover (12) operative for directing a fluid flow. The duct cover being further operative for minimizing the entrance of foreign object debris into the duct (4). The duct cover (12) has a flow directing honeycomb portion (16) for conducting the passing fluid flow in a preferred direction. The flow directing honeycomb (16) comprises an array of continuous, polygon shaped open cells (20) which are biased with respect to the initial fluid flow direction. The periphery (17) of the flow directing honeycomb (12) is rigidized to stiffen the same for minimizing the displacements thereof. The rigidity is provided by a framing member comprising upper and lower skin structures (28, 29) affixed to a core material (30). The framing member is preferably adhesively bonded to the flow directing honeycomb (16) by means of a foaming adhesive (36) and a barrier member (38). The barrier member (38) is operative for minimizing the expansion of the foaming adhesive (36) into the open cells (20) of the honeycomb (16). In order to improve the low observability characteristics of the structure, the cells (20) of the flow directing honeycomb (16) are preferably coated with a radar absorbent material, such as carbon, which acts to minimize the amount of electromagnetic energy that is reflected therefrom.