Metal-ceramic composite structure and fabrication method thereof
US-2017312817-A1 · Nov 2, 2017 · US
US2016288200A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016288200-A1 |
| Application number | US-201514676864-A |
| Country | US |
| Kind code | A1 |
| Filing date | Apr 2, 2015 |
| Priority date | Apr 2, 2015 |
| Publication date | Oct 6, 2016 |
| Grant date | — |
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A metal composite comprises: a matrix comprising periodic metal springs; and a filler material comprising one or more of the following: a carbon composite; a polymer; a metal; graphite; cotton; asbestos; or glass fiber; wherein the filler material is bounded to the matrix via one or more of the following: a mechanical interlocking; a chemical bond; a solid solution; or an active layer disposed between the periodic metal springs and the filler material.
Opening claim text (preview).
What is claimed is: 1 . A metal composite comprising: a metal matrix comprising periodic metal springs; and a filler material comprising one or more of the following: a carbon composite; a polymer; a metal; graphite; cotton; asbestos; or glass fiber; wherein the filler material is bounded to the metal matrix via one or more of the following: a mechanical interlocking; a chemical bond; a solid solution; or an active layer disposed between the periodic metal springs and the filler material. 2 . The metal composite of claim 1 , wherein the periodic metal springs comprise coil springs having an average spring pitch of about 0.8 to about 7.5 mm and an average spring diameter of about 0.8 to about 7.5 mm. 3 . The metal composite of claim 1 , wherein the periodic metal springs have an average wire diameter of about 0.08 to about 0.5 mm. 4 . The metal composite of claim 1 , wherein the periodic metal springs have a density of about 0.2 to about 4 g/cm 3 . 5 . The metal composite of claim 1 , wherein the periodic metal springs comprise one or more of the following: an iron alloy; a nickel-chromium based alloy; a nickel alloy; copper; or a shape memory alloy. 6 . The metal composite of claim 1 , wherein the carbon composite of the filler material comprises carbon and a binder containing one or more of the following: SiO 2 ; Si; B; B 2 O 3 ; a metal; or an alloy of the metal; and wherein the metal is one or more of the following: aluminum; copper; titanium; nickel; tungsten; chromium; iron; manganese; zirconium; hafnium; vanadium; niobium; molybdenum; tin; bismuth; antimony; lead; cadmium; or selenium. 7 . The metal composite of claim 6 , wherein the carbon in the carbon composite comprises one or more of the following: expanded graphite; expandable graphite; natural graphite; or synthetic graphite. 8 . The metal composite of claim 1 , wherein the metal of the filler material comprises one or more of the following: aluminum; copper; tin; or a eutectic alloy. 9 . The metal composite of claim 1 , wherein the polymer of the filler material comprises one or more of the following: an acrylonitrile butadiene rubber; hydrogenated nitrile butadiene; acrylonitrile butadiene carboxy monomer; ethylene propylene diene monomer; fluorocarbon rubber; perfluorocarbon rubber; tetrafluoro ethylene/propylene rubbers; an aliphatic polyamide; polyethylene; polytetrafluoroethylene; polyphenylene sulfide or crosslinked polyphenylene sulfide; or polycarbonate. 10 . The metal composite of claim 1 , wherein the filler material further comprises a reinforcement agent. 11 . The metal composite of claim 1 , wherein the filler material is disposed in a plurality of pores within the matrix. 12 . The metal composite of claim 1 , wherein the filler material forms a coating at least partially encapsulating the matrix. 13 . The metal composite of claim 1 , wherein the matrix is disposed between two layers formed from the filler material. 14 . The metal composite of claim 1 , wherein the volume ratio of the matrix relative to the filler is about 2.5%:97.5% to about 80%:20%. 15 . A method of manufacturing a metal composite, the method comprising: combining a matrix comprising periodic metal springs with a filler material; and forming the metal composite via one or more of the following: powder infiltration and sintering; compression molding; injection molding; extrusion molding; vacuum infiltration; vapor deposition; electrochemical deposition; hot isostatic pressing; casting; or brazing. 16 . The method of claim 15 , wherein the method further comprises forming the matrix by a process comprising one or more of the following: micromachining; three-dimensional printing; weaving; non-weaving; photolithography; projection microstereolithography; etching; or a micromanufacturing process. 17 . The method of claim 15 , further comprising heating the metal composite at atmospheric pressure to release residual stress. 18 . The method of claim 15 comprising: forming two layers from the filler material; disposing the matrix between the two layers; and forming the composite via one or more of the following: sintering; compression molding; or brazing. 19 . The method of claim 15 comprising: forming an encapsulation layer from the filler material; disposing the encapsulation layer around the matrix; and forming the composite via one or more of the following: sintering; compression molding; or brazing. 20 . An article comprising the metal composite of claim 1 . 21 . The article of claim 19 , wherein the article is a downhole element comprising a seal; a high pressure beaded frac screen plug; a screen base pipe plug; a coating for balls and seats; a compression packing element; an expandable packing element; an O-ring; a bonded seal; a bullet seal; a sub-surface safety valve seal; a sub-surface safety valve flapper seal; a dynamic seal; a V-ring; a back-up ring; a drill bit seal; a liner port plug; an atmospheric disc; an atmospheric chamber disc; a debris barrier; a drill in stim liner plug; an inflow control device plug; a flapper; a seat; a ball seat; a direct connect disk; a drill-in linear disk; a gas lift valve plug; a fluid loss control flapper; an electric submersible pump seal; a shear out plug; a flapper valve; a gaslift valve; or a sleeve.
Direct sintering or melting · CPC title
by thermal means (control of energy beam parameters for post heating B22F10/364) · CPC title
with organic materials as the main non-metallic constituent, e.g. resin · CPC title
carbon or graphite as the main non-metallic constituent · CPC title
Compacting only · CPC title
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