Welded joint and automobile member
US-2024093708-A1 · Mar 21, 2024 · US
US2016258043A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2016258043-A1 |
| Application number | US-201414552988-A |
| Country | US |
| Kind code | A1 |
| Filing date | Nov 25, 2014 |
| Priority date | Nov 27, 2013 |
| Publication date | Sep 8, 2016 |
| Grant date | — |
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Disclosed herein is a shape memory alloy comprising 48 to 50 atomic percent nickel, 15 to 30 atomic percent hathium, 1 to 5 atomic percent aluminum; with the remainder being titanium. Disclosed herein too is a method of manufacturing a shape memory alloy comprising mixing together to form an alloy nickel, hafnium, aluminum and titanium in amounts of 48 to 50 atomic percent nickel, 15 to 30 atomic percent hafnium, 1 to 5 atomic percent aluminum; with the remainder being titanium; solution treating the alloy at a temperature of 700 to 1300° C. for 50 to 200 hours; and aging the alloy at a temperature of 400 to 800° C. for a time period of 50 to 200 hours to form a shape memory alloy.
Opening claim text (preview).
What is claimed is: 1 . A shape memory alloy comprising: 48 to 50 atomic percent nickel, 15 to 30 atomic percent hathium, 1 to 5 atomic percent aluminum; with the remainder being titanium. 2 . The shape memory alloy of claim 1 , where the shape memory alloy has the formula Ni 50 Ti (30−x) Hf 20 Al x , where x can have a value of 1 to 5. 3 . The shape memory alloy of claim 2 , where x has values of 1, 2, 3, 4, or 5. 4 . The shape memory alloy of claim 1 , where the titanium is present in an amount of 25 to 30 atomic percent. 5 . The shape memory alloy of claim 1 , where the alloy displays a compressive strength of 900 to 1200 MPa at a compressive strain of 1.5 to 5%. 6 . The shape memory alloy of claim 1 , where a composition having 3 to 5 wt % aluminum based on the total weight of the alloy, has precipitates of 1 to 10 nanometers. 7 . A method of manufacturing a shape memory alloy comprising: mixing together to form an alloy nickel, hafnium, aluminum and titanium in amounts of 48 to 50 atomic percent nickel, 15 to 30 atomic percent hafnium, 1 to 5 atomic percent aluminum; with the remainder being titanium; solution treating the alloy at a temperature of 700 to 1300° C. for 50 to 200 hours; and aging the alloy at a temperature of 400 to 800° C. for a time period of 50 to 200 hours to form a shape memory alloy. 8 . The method of claim 5 , where the solution treating is conducted at 950° C. for 100 hours. 9 . The method of claim 5 , where the aging the alloy is conducted at 600° C. for 100 hours.
Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00 · CPC title
Making non-ferrous alloys (by electrothermic methods C22B4/00; by electrolysis C25C1/24, C25C3/36) · CPC title
Alloys containing less than 50% by weight of each constituent · CPC title
Resulting in heat recoverable alloys with a memory effect · CPC title
High-melting or refractory metals or alloys based thereon · CPC title
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