Aircraft floor and interior panels using edge coated honeycomb
View Patent ↗Aircraft floor and interior panels where core-skin bonding is improved between honeycomb and composite face sheets (skins) by applying a polyamide and/or rubber-containing adhesive to the edge of the honeycomb prior to bonding. Edge coating of the honeycomb allows one to reduce panel weight without reducing the performance parameters that are required for different types of aircraft floor and interior panels.
1. A method for making an aircraft interior or floor panel comprising the steps of:
providing a first uncured face sheet comprising an interior surface and an exterior surface, said first uncured face sheet comprising at least one fiber layer and an uncured thermosetting resin matrix;
providing a second face sheet comprising an interior surface and an exterior surface;
providing a honeycomb having walls that define a plurality of honeycomb cells wherein said walls have a first edge for bonding to the interior surface of said first uncured face sheet and a second edge for bonding to the interior surface of said second face sheet;
applying an adhesive only to said first edge to form an edge-coated honeycomb wherein said adhesive comprises a rubber-modified thermosetting resin; and
bonding said uncured first face sheets and said second face sheet to said edge-coated honeycomb, said bonding comprising the step of curing said uncured thermosetting resin matrix.
2. A method for making an aircraft interior panel according to claim 1 wherein said aircraft interior panel is selected from the group consisting of overhead storage bin panels, ceiling panels, bulkhead panels, lavatory panels, wardrobe panels, galley panels, partition panels and side wall panels.
3. A method for making an aircraft interior panel according to claim 2 wherein the density of said honeycomb is from 1.5 pound per cubic foot to 5.0 pounds per cubic foot.
4. A method for making an aircraft interior panel according to claim 2 wherein said rubber-modified thermosetting resin comprises a thermosetting resin selected from the group consisting of epoxy resin, phenolic resin, cyanate esters and bismaleimides.
5. A method for making an aircraft interior panel according to claim 2 wherein the amount of said adhesive that is present on said first edge of said edge-coated honeycomb ranges from 0.5 to 2.0 grams per square meter.
6. A method for making an aircraft interior or floor panel according to claim 1 wherein said second face sheet is an uncured face sheet that comprises at least one fiber layer and an uncured thermosetting resin matrix and wherein said method includes the steps of :
applying an adhesive only to said second edge of said honeycomb wherein said adhesive comprises a rubber-modified thermosetting resin; and
bonding said uncured second face sheet to said edge-coated honeycomb, said bonding comprising the step of curing said uncured thermosetting resin matrix.
7. A method for making an aircraft interior panel according to claim 6 wherein said aircraft interior panel is selected from the group consisting of overhead storage bin panels, ceiling panels, bulkhead panels, lavatory panels, wardrobe panels, galley panels, partition panels and side wall panels.
8. A method for making an aircraft interior panel according to claim 7 wherein the density of said honeycomb is from 1.5 pound per cubic foot to 5.0 pounds per cubic foot.
9. A method for making an aircraft interior panel according to claim 7 wherein said rubber-modified thermosetting resin comprises a thermosetting resin selected from the group consisting of epoxy resin, phenolic resin, cyanate esters and bismaleimides.
10. A method for making an aircraft interior panel according to claim 7 wherein the amount of said adhesive that is present on said second edge of said edge-coated honeycomb ranges from 0.5 to 2.0 grams per square meters.
11. A method for making an aircraft floor panel according to claim 1 wherein said aircraft floor panel is selected from the group consisting of aisle floor panels, under seat floor panels, galley floor panels and high load floor panels.
12. A method for making an aircraft floor panel according to claim 11 wherein the density of said honeycomb is from 5 pounds per cubic foot to 15 pounds per cubic foot.
13. A method for making an aircraft floor panel according to claim 11 wherein said rubber-modified thermosetting resin comprises a thermosetting resin selected from the group consisting of epoxy resin, phenolic resin, cyanate esters and bismaleimides.
14. A method for making an aircraft floor panel according to claim 11 wherein the amount of said adhesive that is present on said first edge of said edge-coated honeycomb ranges from 0.5 to 2.0 grams per square meter.
15. A method for making an aircraft floor panel according to claim 6 wherein said aircraft floor panel is selected from the group consisting of aisle floor panels, under seat floor panels, galley floor panels and high load floor panels.
16. A method for making an aircraft floor panel according to claim 15 wherein the density of said honeycomb is from 5 pounds per cubic foot to 15 pounds per cubic foot.
17. A method for making an aircraft floor panel according to claim 15 wherein said rubber-modified thermosetting resin comprises a thermosetting resin selected from the group consisting of epoxy resin, phenolic resin, cyanate esters and bismaleimides.
18. A method for making an aircraft floor panel according to claim 15 wherein the amount of said adhesive that is present on said second edge of said edge-coated honeycomb ranges from 0.5 to 2.0 grams per square meter.
19. A method for making an aircraft interior panel according to claim 1 wherein said rubber-modified thermosetting resin comprises acrylonitrile-butadiene copolymer rubber.
20. A method for making an aircraft floor panel according to claim 6 wherein said rubber-modified thermosetting resin comprises acrylonitrile-butadiene copolymer rubber.