UV CURED CROSS-LINKED ABRASION RESISTANT LIQUID CERAMIC NANO-COMPOSITE
20220411641 · 2022-12-29
Inventors
Cpc classification
C04B35/00
CHEMISTRY; METALLURGY
C09D167/02
CHEMISTRY; METALLURGY
C09D167/06
CHEMISTRY; METALLURGY
C04B41/4572
CHEMISTRY; METALLURGY
C04B41/4572
CHEMISTRY; METALLURGY
C09D133/02
CHEMISTRY; METALLURGY
C09D4/06
CHEMISTRY; METALLURGY
C04B35/00
CHEMISTRY; METALLURGY
C04B41/5072
CHEMISTRY; METALLURGY
C04B41/0045
CHEMISTRY; METALLURGY
C09D7/70
CHEMISTRY; METALLURGY
C04B2111/00982
CHEMISTRY; METALLURGY
C04B41/5072
CHEMISTRY; METALLURGY
C04B41/0045
CHEMISTRY; METALLURGY
C09D167/06
CHEMISTRY; METALLURGY
International classification
C09D4/06
CHEMISTRY; METALLURGY
C04B41/00
CHEMISTRY; METALLURGY
C09D133/02
CHEMISTRY; METALLURGY
C09D167/02
CHEMISTRY; METALLURGY
C09D167/06
CHEMISTRY; METALLURGY
Abstract
A UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder, comprised of 30%-45% by weight resin, wherein the resin is at least one of 2-propenoic acid, homopolymer, isophthalic acid, 1,4-Dimethoxybenzene, saturated polyester resin, and maleic anhydride; 10%-20% by weight industrial ceramic inorganic nano-materials; 30%-45% by weight industrial ceramic inorganic abrasion-resistant powder; and styrene, wherein the styrene is less than 25% by weight of the UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder.
Claims
1. A UV-cured cross-linked liquid resin reinforced with ceramic inorganic nanoparticles and ceramic inorganic abrasion-resistant powder, comprising: 30%-45% by weight resin, wherein said resin is at least one of 2-propenoic acid, homopolymer, isophthalic acid, 1,4-Dimethoxybenzene, saturated polyester resin, and maleic anhydride; 10%-20% by weight industrial ceramic inorganic nanomaterials; 30%-45% by weight industrial ceramic inorganic abrasion-resistant powder; and styrene, wherein said styrene is less than 25% by weight of said UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder.
2. A UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder according to claim 1, wherein said UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder is comprises of 45% resin by weight.
3. A UV-cured cross-linked liquid resin reinforced with ceramic inorganic nanoparticles and ceramic inorganic abrasion-resistant powder according to claim 1, wherein said industrial ceramic inorganic nano-materials comprise aluminum hydroxide.
4. A UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder according to claim 1, wherein said industrial ceramic inorganic abrasion-resistant powder comprises at least one of silicon dioxide, amorphous, fumed silica and/or silica glass.
5. A UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder according to claim 1, wherein said industrial ceramic inorganic nano-materials and said industrial ceramic inorganic abrasion-resistant powder together make up 50-60% of said UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder by weight.
6. A UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder according to claim 1, wherein said industrial ceramic inorganic nano-materials and said industrial ceramic inorganic abrasion-resistant powder together make up 55% of said UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder by weight.
7. A UV-cured cross-linked liquid resin reinforced with ceramic inorganic nanoparticles and ceramic inorganic abrasion-resistant powder according to claim 1, further comprising a filler, wherein said filler comprises at least one of: chopped carbon fiber, continuous carbon fiber, kevlar, dyneema, woven reinforcements, multiaxial reinforcements, honeycomb, ceramic fibers, aluminum fibers, quartz fabric, man-made vitreous fiber, glass fiber mats, glass fiber chopped strand mats, polyamide fabrics, fiber reinforcements (fibers, whiskers, particles), rigid foam, wood, metal, paper honeycomb, nomex honeycomb, carbon honeycomb, fiberglass honeycomb, metal honeycomb, fiberglass cloth, nylon, cotton, nylon thermoplastic fibers, polyester thermoplastic fibers, e-glass, e-cr glass, s-glass, alumina-lime-borosilicate, aramid fibers, carbon fibers, graphite fibers, spider silk, man-made spider silk, aromatic polyamid, man-made organic fibers, aluminum oxide nano-particles, aluminum hydroxide nano-particles, graphene, halloysite, wollastonite, talc, mica, glass beads, hollow glass, roving mat, milled fiber mat, chopped strand mat, continuous fiber may, thermoform-able mat, multi-end rovings, single-end rovings filament winding applications, pultrusion applications, non-woven veils, soluble & insoluble fibers, unidirectional reinforcements, tapes, tows, unidirectional tow sheet and roving, monocrystalline whiskers, polymer-matrix-composites, metal-matrix-composites, ceramic-matrix-composites, silicon carbide, carbon nano tubes, titanium dioxide, titanium carbide, unidirectional tapes, non-crimp fabrics, dry carbon fabrics, yarns, petroleum pitch, polyacrylonitrile, rayon, phenolic micro-balloons, plastic micro-balloons, reactive carbon nano-fibers, nano-cellulose, and cellulose nano-crystal.
8. A method for repairing an industrial material comprising: preparing a surface of an industrial material; filling gaps in said prepared surface of said industrial material with a UV-cured cross-linked liquid resin reinforced with ceramic inorganic nanoparticles and ceramic inorganic abrasion-resistant powder, comprising: 30%-45% by weight resin, wherein said resin is at least one of 2-propenoic acid, homopolymer, isophthalic acid, 1,4-Dimethoxybenzene, saturated polyester resin, and maleic anhydride; 10%-20% by weight industrial ceramic inorganic nano-materials; 30%-45% by weight industrial ceramic inorganic abrasion-resistant powder; and styrene, wherein said styrene is less than 25% by weight of said UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder; applying ultra-violet light to said UV-cured cross-linked liquid resin reinforced with ceramic inorganic nanoparticles and ceramic inorganic abrasion-resistant powder.
9. A method for repairing an industrial material according to claim 8, wherein said industrial material comprises abrasion-resistant industrial ceramic tile.
10. A system for repairing an industrial material comprising; an applicator; and a UV-cured cross-linked liquid resin reinforced with ceramic inorganic nanoparticles and ceramic inorganic abrasion-resistant powder, comprising: 30%-45% by weight resin, wherein said resin is at least one of 2-propenoic acid, homopolymer, isophthalic acid, 1,4-Dimethoxybenzene, saturated polyester resin, and maleic anhydride; 10%-20% by weight industrial ceramic inorganic nanomaterials; 30%-45% by weight industrial ceramic inorganic abrasion-resistant powder; and styrene, wherein said styrene is less than 25% by weight of said UV-cured cross-linked liquid resin reinforced with ceramic inorganic nano-particles and ceramic inorganic abrasion-resistant powder.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
[0013] For a more complete understanding of the present invention and the advantages thereof, reference is now made to the following description and the accompanying drawings, in which:
[0014]
[0015]
[0016]
[0017]
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0018] Instead of attempting costly and potentially dangerous conventional methods, the end user needs a one-component thixotropic paste that can be formed into virtually any shape and cured to extreme strength and hardness within minutes. Essentially, a high strength “industrial ceramic parts factory in a tube” is needed. There is an extreme need in virtually all industries for a molding material where an average citizen can make strong custom parts and/or make quality permanent custom repairs in minutes.
[0019] The present invention is a UV cured cross-linked liquid resin reinforced with ceramic inorganic nanoparticles and ceramic inorganic abrasion-resistant powder comprised of the following in percentages by weight: [0020] 30%-45% resin from any of 2-propenoic acid, homopolymer (CAS Nos. 9003-01-4), Isophthalic acid (CAS No. 121-91-5), 1,4-Dimethoxybenzene (CAS No. 150-78-7, dimethyl 5-sodiosulfoisophthalate-ethylene glycol-isophthalic acid-terephthalic acid copolymer (CAS No. 61926-16-7), or Maleic anhydride (CAS No. 108-31-6); [0021] 10%-20% industrial ceramic inorganic nanomaterials including aluminum hydroxide (CAS No. 21654-51-2); [0022] 30%-45% industrial ceramic inorganic abrasion-resistant powder such as silicon dioxide (CAS No. 14808-60-7), amorphous, fumed silica (CAS No. 112945-52-5) and/or silica glass (CAS No. 60676-86-0); and [0023] styrene (less than 25%) (CAS NO. 100-42-5).
[0024] This composition forms a UV cured industrial paste for repair of wear-resistant (or abrasion-resistant) material and casting custom parts. The UV cured resin must achieve at least ⅛″ of fully cured material in less than 5 minutes when exposed to the appropriate UV Light. When the UV activated resin is fully cured and hardened it must attain a hardness of greater than 60 Barcol using the Barcol impresser scale. The resin preferably comprises about 45% of the nanocomposite by weight. The ceramic inorganic materials and abrasion resistant powder together preferably comprise 50%-60%, and preferably about 55%, of the nanocomposite by weight.
[0025] As shown in
[0026] The present invention may be used with other types of applicators and is by no means limited to this particular applicator. For example, the US cured industrial paste of the present invention could be placed within a housing or container having a plunger to push the paste out of a nozzle. Such a container could be made of any of many different materials, including but not limited to plastic. Any of these or many other known means for holding the paste and applying it may be referred to as an “applicator.”
[0027] The UV cured resin of the present invention may have many other applications, such as to encapsulate a bolt as shown in
[0028] The materials and products according to the present invention may be used, for example, for repair of abrasion-resistant, non-decorative tile, brick or plate for bulk materials handling, military applications and aerospace applications including, but not limited to, General Aerospace Repair, Aerospace Composite Repair, Carbon Fiber Repair, Automotive Composite Repair and other Advanced Composite Repair.
[0029] A significant drawback during Aerospace repair and other advanced composite repair are the lengthy cure times coupled with labor intensive multipart resin components. Mandatory cold storage of resins and the specialized heat equipment required for high temperature induced curing methods leads to costly and extremely time-consuming repairs.
[0030] The Aerospace Industry and advanced composite repair industry are in great need of a One-Part UV cured Nano-Composite that can literally achieve full cure of at least ⅛″ in less than 5 minutes. The nanocomposite of the present invention can be stored at room temperature and maintain its stability and viability for 2, 3, or even 5 or more years.
[0031] The one-part nano-composite of the present invention can also reinforce or be reinforced with a multitude of various fillers, fibers and/or composites including, but not limited to: Chopped Carbon Fiber, Continuous Carbon Fiber, Kevlar, Dyneema, Woven Reinforcements, Multiaxial Reinforcements, Honeycomb, Ceramic Fibers, Aluminum Fibers, Quartz Fabric, Man Made Vitreous Fiber, Glass Fiber Mats, Glass Fiber chopped strand mats, Polyamide Fabrics, Fiber Reinforcements (Fibers, whiskers, particles), Rigid Foam, Wood, Metal, Paper Honeycomb, Nomex Honeycomb, Carbon Honeycomb, Fiberglass Honeycomb, Metal Honeycomb, Fiberglass Cloth, Nylon, Cotton, Nylon Thermoplastic Fibers, Polyester Thermoplastic Fibers, E-Glass, E-CR Glass, S-Glass, Alumina-Lime-Borosilicate, Aramid Fibers (Polyaramids), CARBON FIBERS, Graphite Fibers (>99% Carbon Fibers), Spider Silk (Natural), Spider Silk (Man-Made) Aromatic Polyamid, Man-Made Organic Fibers, Aluminum Oxide nano-particles, Aluminum Hydroxide nano-particles, Graphene, Halloysite, Wollastonite, Talc, Mica, Glass Beads, Hollow glass, Roving Mat, Milled Fiber Mat, Chopped Strand Mat, Continuous Fiber May, Thermoform-able Mat, Multi-End Rovings, Single-End Rovings Filament winding applications, Pultrusion applications, Non-Woven Veils, Soluble & Insoluble Fibers, Unidirectional reinforcements, Tapes, Tows, unidirectional tow sheet and roving, Monocrystalline Whiskers, Polymer-Matrix-Composites, Metal-Matrix-Composites, Ceramic-Matrix-Composites, Silicon Carbide, Carbon Nano Tubes, Titanium Dioxide, Titanium Carbide, Unidirectional Tapes, Non-Crimp Fabrics, Dry Carbon Fabrics, Yarns, Petroleum Pitch, Polyacrylonitrile, Rayon, phenolic micro-balloons, plastic micro-balloons, Reactive Carbon Nano-Fibers, Nano-Cellulose, and Cellulose Nano-Crystal.
[0032] The foregoing description of the preferred embodiment of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise form disclosed, and modifications and variations are possible in light of the above teachings or may be acquired from practice of the invention. The embodiment was chosen and described in order to explain the principles of the invention and its practical application to enable one skilled in the art to utilize the invention in various embodiments as are suited to the particular use contemplated. It is intended that the scope of the invention be defined by the claims appended hereto, and their equivalents. The entirety of each of the aforementioned documents is incorporated by reference herein.