Ceramic fibers for shielding in vacuum chamber systems and methods for using same
US-2024304424-A1 · Sep 12, 2024 · US
US9611937B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9611937-B2 |
| Application number | US-201414527716-A |
| Country | US |
| Kind code | B2 |
| Filing date | Oct 29, 2014 |
| Priority date | Oct 29, 2014 |
| Publication date | Apr 4, 2017 |
| Grant date | Apr 4, 2017 |
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A superelastic metal seal for use in a downhole tool, wherein the superelastic metal seal may be formed from a superelastic Ni—Ti alloy. The superelastic Ni—Ti alloy may be prestrained with a permanent strain. Superelasticity may be imparted to the superelastic Ni—Ti alloy through a thermal treatment process or through prestraining the superelastic Ni—Ti alloy. The superelastic Ni—Ti alloy may exhibit superelastic behavior. The superelastic Ni—Ti alloy may not exhibit shape memory behavior.
Opening claim text (preview).
What is claimed is: 1. A superelastic metal seal, comprising a superelastic Ni—Ti alloy, the superelastic Ni—Ti alloy including, by weight percent, about 65% to about 58% nickel (Ni) and about 35% to about 42% titanium (Ti), and wherein the superelastic Ni—Ti alloy is not capable of shape memory behavior. 2. The superelastic metal seal of claim 1 , wherein the superelastic Ni—Ti alloy is prestrained with at least approximately a 2% permanent strain. 3. The superelastic metal seal of claim 1 , wherein the superelastic Ni—Ti alloy comprises, by weight percent, about 60% nickel (Ni) and about 40% titanium (Ti). 4. The superelastic metal seal of claim 1 , wherein the superelastic Ni—Ti alloy exhibits superelastic behavior at least up to a compressive strain of about 10%. 5. The superelastic metal seal of claim 4 , wherein the superelastic Ni—Ti alloy exhibits superelastic behavior at least up to a compressive strain of about 15%. 6. The superelastic metal seal of claim 1 , wherein the superelastic Ni—Ti alloy exhibits superelastic behavior within a temperature range of from about 120° C. to about 205° C. 7. The superelastic metal seal of claim 6 , wherein the superelastic Ni—Ti alloy exhibits superelastic behavior in a temperature range of from about 20° C. to about 400° C. 8. The superelastic metal seal of claim 1 , wherein the superelastic metal seal is configured for use in a downhole hole tool assembly and is selected from the group consisting of O-rings, C-rings, D-seals, T-seals, V-seals, X-seals, flat seals, lip seals, cup seals, backup rings, bonded seals, and packing elements. 9. A downhole tool, comprising: a component; and a superelastic metal seal disposed adjacent the component, the superelastic metal seal comprising a superelastic Ni—Ti alloy including, by weight percent, about 65% to about 58% nickel (Ni) and about 35% to about 42% titanium (Ti), and wherein the superelastic Ni—Ti alloy exhibits superelastic behavior within a temperature range of from about 120° C. to about 205° C. and is not capable of shape memory behavior. 10. The downhole tool of claim 9 , wherein the superelastic Ni—Ti alloy exhibits superelastic behavior within a temperature range of from about 20° C. to about 400° C. 11. The downhole tool of claim 9 , wherein the superelastic Ni—Ti alloy comprises, by weight percent, about 60% nickel (Ni) and about 40% titanium (Ti). 12. The downhole tool of claim 9 , wherein the superelastic Ni—Ti alloy is plastically prestrained. 13. The downhole tool of claim 10 , wherein the superelastic Ni—Ti alloy is plastically prestrained with at least approximately a 2% permanent strain. 14. The downhole tool of claim 9 , wherein the superelastic Ni—Ti alloy exhibits superelastic behavior at least up to a compressive strain of about 10%.
based on nickel · CPC title
characterised by their structure; Selection of materials · CPC title
characterised by structure or material · CPC title
characterised by material or surface treatment · CPC title
of nickel or cobalt or alloys based thereon · CPC title
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