摘要：
Load-bearing composite panels, materials, and products made by surrounding with a long fiber and/or fiber cloth reinforced polyurethane resin, an assembly containing one or more load- bearing members, graphene, a structural polyurethane/resin sandwich composite and/or spider silk protein fiber-cloth-continuous fibers. The composite structures can provide stronger, lighter- weight structural items such as vehicle floor and body panels, bullet-proof anti-ballistic panel products, vehicle bullet-proof anti-ballistic body panel structures and floors, bullet-proof vests, vehicle chassis, monocoque chassis, motor homes chassis-bodies, fuselage floors and frames for aircraft and/or UAV's, bicycle and motorcycle frames, wind turbine blades frames and structures, ship or boat haul body structures, shipment containers, pre-fabricated walls of buildings, train structure body or floor panels, solar panel supports, battery housings, mobile home walls, roof modules, truck beds, and truck trailer floors. Such composite panels, materials, and products can also be utilized in artificial organs, ligaments or tendons, artificial disc vertebrae, ropes, and 3D printing parts.
权利要求：
CLAIMS
1. A silk fibroin composite comprising: a plurality of coupled layers wherein at least one of the layers includes a composite matrix of at least one non-silk polymer and silk fibroin material derived at least in part from expression of one or more spider silk genes within at least one living organism, the plurality of coupled layers comprising: at least one backing or surface layer; at least one layer including a plurality of cells, the at least one layer coupled to the at least one backing or surface layer; and wherein the at least one of the plurality of coupled layers includes a material that is fibrous.
2. The composite of claim 1, wherein the silk fibroin material includes at least one of silk fiber and silk polypeptides in a non-fibrous form.
3. The composite of claim 1, wherein the at least one non-silk polymer includes at least one of a thermoplastic polymer and a thermoset polymer.
4. The composite of claim 1, wherein the plurality of coupled layers includes at least one of a polyurethane polymer, a polycarbonate polymer, a polypropylene polymer, an acrylonitrile butadiene styrene (ABS) polymer, a polylactic acid (PLA) polymer, a polyamide (nylon) polymer, a glass-filled polyamide polymer, an epoxy resin, silver, gold, titanium, steel, stainless steel, wax, a photopolymer, high density polyethylene (HDPE), polycarbonate-acrylonitrile butadiene styrene (PC/ABS) polymer, and polyphenylsulfone (PPSU) polymer.
5. The composite of claim 1, wherein the at least one non-silk polymer comprises polyurethane reaction product of one or more isocyanates and at least one isocyanate-reactive component.
6. The composite of claim 1, wherein the silk fibroin material forms at least a portion of the composite matrix of at least one of the at least one backing or surface layer and the at least one layer.
7. The composite of claim 1, wherein the silk fibroin material includes at least one of a plurality of long fibers of varying lengths and a plurality of short fibers comprised of a variety of lengths; and wherein the long fibers have lengths of more than 3mm and the short fibers have lengths less than the shortest of any of the lengths of the plurality of long fibers.
8. The composite of claim 7, wherein the long fibers make up 0.5 wt.% to 99 wt. % of the combined weight of the plurality of coupled layers.
9. The composite of claim 1, wherein the silk fibroin material comprises electro-spun silk.
10. The composite of claim 1, wherein the silk fibroin material includes silk weave or cloth, silk fiber, silk mat.
11. The composite of claim 1, wherein the plurality of cells comprises a honeycomb-like structure.
12. The composite of claim 1, wherein at least a portion of the composite matrix is derived by injection molding, reaction-injection molding, chopped-fiber injection, extrusion, molding, film casting, web coating, spray-coating, weaving, vacuum injection, or 3D printing.
13. The composite of claim 1, wherein at least a portion of the plurality of coupled layers includes a fibrous material that includes at least one of a silk fiber, a silk weave or cloth, and a silk mat.
14. The composite of claim 1, wherein the plurality of coupled layers is an article of manufacture selected from a land vehicle frame, an air vehicle frame, a sea vehicle frame, a land vehicle panel, an air vehicle panel, and a sea vehicle panel.
15. The composite of claim 13, wherein the article of manufacture includes at least one of a load-bearing structure, non-load-bearing structure, and a decorative or aesthetic structure.
16. A method of making a silk fibroin composite comprising:
providing at least one non-silk polymer and silk fibroin material derived at least in part from expression of one or more spider silk genes in at least one living organism; combining at least a portion of the silk fibroin material and the at least one non-silk polymer material to form a mixture; forming a composite matrix from at least a portion of the mixture using a process of injection molding, reaction-injection molding, chopped-fiber injection, extrusion, molding, film casting, web coating, spray-coating, weaving, vacuum injection, and 3D printing; forming a plurality of coupled layers using at least a portion of the composite matrix, the plurality of layers comprising: at least one backing or surface layer and at least one layer including a plurality of cells, the at least one layer coupled to the at least one backing or surface layer; and wherein the at least one of the plurality of coupled layers includes a material that is fibrous.
17. The method of claim 16, wherein the silk fibroin material includes at least one of a plurality of long fibers of varying lengths and a plurality of short fibers comprised of a variety of lengths.
18. The method of claim 17, wherein the long fibers have lengths of more than 3mm and the short fibers have lengths less than the shortest of any of the lengths of the plurality of long fibers.
19. The method of claim 17, wherein the long or short fibers include at least one of a silk fiber, a silk weave or cloth, and a silk mat.
20. The method of claim 16, wherein the plurality of coupled layers is an article of manufacture selected from a land vehicle frame, an air vehicle frame, a sea vehicle frame, a land vehicle panel, an air vehicle panel, and a sea vehicle panel.
21. The composite of claim 20, wherein the article of manufacture includes at least one of a load-bearing structure, non-load-bearing structure, and a decorative or aesthetic structure.
22. A method of making a silk fibroin composite comprising: feeding a silk fibroin material into an extruder, the silk fibroin material derived at least in part from expression of one or more spider silk genes in at least one living organism; extruding a silk fiber precursor from the silk fibroin material; passing the silk fiber precursor through a coagulation bath at one end of the coagulation bath; forming a silk fiber from the silk fiber precursor through coagulation in the coagulation bath; stretching at least a portion of the silk fiber using at least one set of godets; combining at least a portion of the silk fiber with at least one non-silk polymer material to form a feedstock; using the feedstock, forming a composite matrix using at least one of injection molding, reaction-injection molding, chopped-fiber injection, extrusion, molding, film casting, web coating, spray-coating, batch mixing, weaving, vacuum injection, and 3D printing.
23. The method of claim 22, further comprising: forming a plurality of coupled layers using at least a portion of the composite matrix, the plurality of layers comprising: at least one backing or surface layer and at least one layer including a plurality of cells, the at least one layer coupled to the at least one backing or surface layer.
24. The method of claim 22, wherein the composite matrix includes at least one of a plurality of long fibers of varying lengths and a plurality of short fibers comprised of a variety of lengths; and wherein the long fibers have lengths of more than 3mm and the short fibers have lengths less than the shortest of any of the lengths of the plurality of long fibers.
25. The method of claim 24, wherein the long fibers make up 0.5 wt.% to 99 wt. % of the combined weight of the composite matrix.
26. The method of claim 23, wherein the plurality of cells comprises a honeycomb-like structure.
27. The method of claim 26, wherein the honeycomb-like structure includes a structural core including at least one of an aluminum core, a foam core, a wood core, and a carbon-fiber core.
28. The method of claim 23, further comprising mixing the feedstock with another feedstock selected from a soap material, a cosmetic material, or a paint material.