Long fiber thermoplastic helmet inserts and helmets and methods of making each
US-2015360397-A1 · Dec 17, 2015 · US
US9505151B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9505151-B2 |
| Application number | US-201314072016-A |
| Country | US |
| Kind code | B2 |
| Filing date | Nov 5, 2013 |
| Priority date | Nov 5, 2013 |
| Publication date | Nov 29, 2016 |
| Grant date | Nov 29, 2016 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A carbon composite contains expanded graphite; and at least one of a filler or a reinforcement; wherein the expanded graphite comprises a plurality of randomly oriented basal planes. Methods of making the carbon composite and articles comprising the carbon composite are also disclosed.
Opening claim text (preview).
What is claimed: 1. A carbon composite comprising: expanded graphite; and at least one of a filler or a reinforcement; wherein the expanded graphite comprises a plurality of randomly oriented basal planes. 2. The carbon composite of claim 1 , wherein the filler comprises metal, carbon, ceramic, or a combination comprising at least one of the foregoing. 3. The carbon composite of claim 2 , wherein the metal comprises copper, aluminum, titanium, tungsten, nickel, silicon, chromium, iron, alloys thereof, or a combination comprising at least one of the foregoing. 4. The carbon composite of claim 2 , wherein the carbon comprises amorphous carbon, natural graphite, carbon fiber, or a combination comprising at least one of the foregoing material. 5. The carbon composite of claim 2 , wherein the ceramic comprises SiC, Si 3 N 4 , SiO 2 , BN, and a combination comprising at least one of the foregoing. 6. The carbon composite of claim 1 , wherein the reinforcement comprises a metallic sheet comprising stainless steel, copper alloy, aluminum alloy, titanium alloy, or a combination comprising at least one of the foregoing. 7. The carbon composite of claim 6 , wherein the metallic sheet comprises an aperture. 8. The carbon composite of claim 1 , wherein the expanded graphite is present in an amount of 25 wt. % to 99 wt. %, based on the total weight of the carbon composite. 9. An article comprising the carbon composite of claim 1 . 10. The article of claim 9 , wherein the article is a downhole element. 11. The article of claim 10 , wherein the article comprises packing elements (premier seal), expanding packing elements (ARC seal), O-rings, bonded seals, bullet seals, SSSV dynamic seals, SSSV flapper seals, V rings, back up rings, drill bit seals, mud motor stators, PCP stators, ESP seals, or ESP space out sub. 12. A method for making a carbon composite, the method comprising combining expanded graphite and at least one of a filler or a reinforcement to form a combination; and compressing the combination under an isostatic pressure thereby making the carbon composite; wherein the basal planes of the expanded graphite in the carbon composite are randomly oriented. 13. The method of claim 12 , wherein the combining comprises combining expanded graphite and a metallic filler. 14. The method of claim 12 , wherein the combining comprises combining expanded graphite, a metallic filler, and a reinforcement comprising a metallic sheet. 15. A method for making a carbon composite, the method comprising compressing a composition comprising expanded graphite to form a pre-form comprising an expanded graphite matrix and a plurality of connecting open pores disposed in the matrix; and combining the pre-form with a filler thereby making the carbon composite; wherein the expanded graphite matrix in the carbon composite comprises a plurality of randomly oriented basal planes. 16. The method of claim 15 , further comprising compressing the combination of the pre-form and the filler thereby making the composite. 17. The method of claim 15 , wherein the composition further comprises wax. 18. The method of claim 17 , wherein the compressing is conducted at a temperature greater than the melting temperature of the wax. 19. The method of claim 15 , wherein the combining comprises pouring a molten metallic filler to the pre-form. 20. The method of claim 15 , further comprising forming the composite by compressing expanded graphite to form compressed expanded graphite; and milling the compressed expanded graphite to form graphite particles. 21. The method of claim 20 further comprising combining the graphite particle with a reinforcement. 22. The method of claim 15 , wherein the pre-form further comprises a reinforcement. 23. A method of forming a carbon composite, the method comprises: firstly compressing expanded graphite to form compressed expanded graphite; milling the compressed expanded graphite to form expanded graphite particles; combining the expanded graphite particles with at least a filler or a reinforcement to form a combination; and secondly compressing the combination thereby making the carbon composite; wherein the expanded graphite in the carbon composite comprises a plurality of randomly orientated basal planes.
starting from a melt · CPC title
characterised by the choice of material · CPC title
Iron · CPC title
Producing sealings (B29D99/0085 takes precedence) · CPC title
Use of metals, their alloys or their compounds, as reinforcement · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.