Propeller blade
US-2024109645-A1 · Apr 4, 2024 · US
US9452587B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9452587-B2 |
| Application number | US-201313957708-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 2, 2013 |
| Priority date | Aug 6, 2012 |
| Publication date | Sep 27, 2016 |
| Grant date | Sep 27, 2016 |
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Material composites are provided that have improved shock and impact resistance.
Opening claim text (preview).
What is claimed is: 1. A fiber reinforced elastic composite material comprising: a multiplicity of fiber ply layers, each fiber of each layer being rotated along the longitudinal axis at a desired angle relative to the next adjacent layer, each extending longitudinally over the composite, wherein the fiber ply layers are substantially left-handed helicoidal, substantially right-handed helicoidal, or where a portion are substantially left-handed helicoidal while another portion are substantially right-handed helicoidal; and a matrix comprising an elastic material having a modulus of elasticity that is lower than that of the fiber that substantially fills the interstitial spaces between the fibers. 2. The composite material of claim 1 , wherein the composite comprises between 2 to 100 independently orientated fiber ply layers. 3. The composite material of claim 1 , wherein said fibers comprise 20 to 80 percent by weight of the composite material. 4. The composite material of claim 1 , wherein the composite material comprises 2,000 to 70,000,000 fibers. 5. The composite material of claim 1 , wherein the fiber ply layers comprise carbon fibers, nylon fibers, acrylic fibers, wood fibers, basalt fibers, glass fibers, aramid fibers, polyethylene fibers, polyparaphenylene fibers, benzobisoxazole fibers, polybenzamidazole fibers, or any combination thereof. 6. The composite material of claim 1 , wherein the fiber ply layers comprise fibers having a length between 0.5 mm to 33 mm. 7. The composite material of claim 1 , wherein the fibers of the fiber ply layers are treated by sizing, additives, and/or curing. 8. The composite material of claim 1 , wherein the elastic material can form crosslinks. 9. The composite material of claim 1 , wherein the elastic material is selected from the group consisting of ceramics, thermoset resins, and thermoplastic resins. 10. The composite material of claim 9 , wherein the thermoset resin is an epoxy. 11. The composite material of claim 9 , wherein the thermoset resins or the thermoplastic resins further comprise one or more fillers so as to reduce cost, control shrinkage, improve mechanical and physical properties, provide ultra violet (UV) protection, weathering protection, surface smoothness, temperature resistance, impact strength, and/or provide fire resistance. 12. The composite material of claim 1 , wherein the matrix or the elastic material further comprises microspheres. 13. The composite material of claim 12 , wherein the microspheres introduce micropores throughout the matrix. 14. The composite material of claim 12 , wherein the microspheres are expandable polymeric microspheres. 15. The composite material of claim 12 , wherein the microspheres are from about 10 μm to about 100 μm in diameter. 16. The composite material of claim 1 , wherein the matrix further comprises one or more additives selected from the group consisting of accelerators, flexibilizers, release agents, plasticizers, viscosity control agents, hardeners, air release agents, toughness agents, electrical conductivity agents, antistatic agents, and antioxidants. 17. The composite material of claim 1 , wherein the composite material further comprises a thermal barrier coating, impact resistant coating, wear resistant coating, corrosion resistant coating, and/or electrically conductive coating. 18. A garment comprising the composite material of claim 1 . 19. Sporting or work safety equipment comprising the composite material of claim 1 .
Inorganic fibres · CPC title
Impact strength, toughness · CPC title
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