Method for fabricating large dimension bonds using reactive multilayer joining
A method for joining component bodies of material over bonding regions of large dimensions by disposing a plurality of substantially contiguous sheets of reactive composite materials between the bodies and adjacent sheets of fusible material. The contiguous sheets of the reactive composite material are operatively connected by an ignitable bridging material so that an igniting reaction in one sheet will cause an igniting reaction in the other. An application of uniform pressure and an ignition of one or more of the contiguous sheets of reactive composite material causes an exothermic thermal reaction to propagate through the bonding region, fusing any adjacent sheets of fusible material and forming a bond between the component bodies.
1. A method of bonding a first component body to at least one additional component body over a large dimension bonding region, comprising the steps of:
disposing at least one sheet of reactive composite material between the first component body and each additional component body;
initiating an exothermic reaction in said sheet of reactive composite material, said exothermic reaction resulting in the formation of a bond between said first component body and said at least one additional component body over the lame dimension bonding region;
wherein said large dimension bonding region has a surface area greater than the surface area of a single sheet of reactive composite material;
wherein said step of disposing includes disposing a plurality of horizontally adjacent and non-overlapping sheets of reactive composite material in a plane of said bonding region between the first component body and each additional component body; and
wherein said exothermic reaction is initiated in each of said plurality of horizontally adjacent sheets.
2. The method of claim 1 wherein said exothermic reaction in a plurality of said horizontally adjacent sheets of reactive composite material is initiated at one or more discrete locations in each sheet substantially simultaneously.
3. The method of claim 1 further including the step of disposing at least one ignition bridge between said plurality of horizontally adjacent sheets of reactive composite material, and wherein said ignition bridge conveys an initiated exothermic reaction across a spaced gap between said horizontally adjacent sheets of reactive composite material.
4. The method of claim 3 wherein said ignition bridges comprise at least one of a reactive composite material, a multilayer wire, a loose mixture of reactive compounds, and a compact mixture of reactive compounds.
5. The method of claim 1 further including the step of securing each of said plurality of horizontally adjacent sheets of reactive composite material into a planar assembly of spaced apart sheets of reactive composite material.
6. The method of claim 5 further including the step of securing at least one structural support tab between said plurality of horizontally adjacent sheets of reactive composite material to maintain said spaced apart planar assembly.
7. The method of claim 6 wherein said at least one structural support tab consists of a fusible material.
8. The method of claim 6 wherein said at least one structural support tab conveys an initiated exothermic reaction between said adjacent sheets of reactive composite material.
9. The method of claim 1 further including the step of bonding abutting contiguous edges of horizontally adjacent sheets of reactive composite material to form said planar assembly.
10. The method of claim 9 wherein said contiguous edges are bonded with an organic adhesive.
11. The method of claim 9 wherein said contiguous edges are bonded with a fusible material.
12. A method for initiating an exothermic reaction within an assembly of a plurality of horizontally adjacent and non-overlapping reactive composite material sheets, comprising:
coupling at least one ignition bridge between each horizontally adjacent and spaced apart reactive composite material sheet within the assembly, providing an ignition pathway between each of said plurality of reactive composite material sheets;
initiating the exothermic reaction in at least a first reactive composite material sheet within the assembly; and
conducting the exothermic reaction between adjacent reactive composite material sheets within the assembly over said ignition bridges.
13. The method of claim 12 wherein said exothermic reaction is initiated in said first reactive composite material sheet from ignition of an ignition bridge coupled to said first reactive composite material sheet.
14. The method of claim 12 wherein said ignition bridges each comprise at least one of a reactive composite material, a multilayer wire, a loose mixture of reactive compounds, and a compact mixture of reactive compounds.
15. The method of claim 12 wherein said step of initiating the exothermic reaction includes initiating the exothermic reaction substantially simultaneously in a plurality of discrete locations on said sheets of horizontally adjacent reactive composite material.
16. The method of claim 12 wherein said step of initiating the exothermic reaction includes initiating the exothermic reaction substantially simultaneously at a plurality of separate and independent points within a sheet of reactive composite material.