CN102864341A - Super-elastic alloy material and preparation method thereof - Google Patents
Super-elastic alloy material and preparation method thereof Download PDFInfo
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- CN102864341A CN102864341A CN2012103273285A CN201210327328A CN102864341A CN 102864341 A CN102864341 A CN 102864341A CN 2012103273285 A CN2012103273285 A CN 2012103273285A CN 201210327328 A CN201210327328 A CN 201210327328A CN 102864341 A CN102864341 A CN 102864341A
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Abstract
The invention relates to a super-elastic alloy material. The alloy material comprises the following components according to the percentage composition of atoms: 45-55at% of nickel, 0-10at% of ferrum, 25-35at% of titanium and 5-15at% of cobalt. The alloy material provided by the technical scheme not only has narrow hysteresis superelasticity, but also can keep a shape memory effect.
Description
Technical field
The invention belongs to functional technical field of alloy material, refer to especially a kind of superelastic alloy and preparation method thereof.
Background technology
Superelastic alloy is widely used in the fields such as aviation, machinery, precision instrument and medical treatment because it has higher recovered elastic deformation.The most normal superelastic alloy that uses is Ti-Ni alloy at present, there is thermo-elastic martensite in the Ti-Ni alloy, its transformation temperature changes within the specific limits with the alloy ingredient difference, because the nickel titante series alloy not only has peculiar shape memory effect, also has preferably super-elasticity behavior, but its super-elasticity behavior belongs to the super-elasticity behavior of wide transformation hysteresis, so in-fighting is high.
Adopt cobalt Substitute For Partial nickel among China patent publication No. CN102337424 and form a kind of nickel ferro-cobalt gallium alloy material, think to obtain preferably super-elasticity behavior by the martensitic transformation temperature that can change and control alloy material.Analyze by the alloy to this technical scheme, the elastic performance of this alloy is better than common Ti-Ni alloy really, martensite also corresponding minimizing is a lot, but this alloy also has certain defective, has super-elasticity although Here it is, but the shape memory effect for former Ti-Ni alloy greatly reduces, even shape memory effect is zero in some component.Therefore need to develop a kind of alloy material that narrow hysteresis elastic performance can keep again shape memory effect that namely has.
Summary of the invention
The objective of the invention is by a kind of technical scheme is provided, the alloy material of this technical scheme not only has the alloy material that narrow hysteresis elastic performance can keep again shape memory effect.
The present invention is achieved by the following technical solutions:
A kind of superelastic alloy, it is nickel 45-55at% that each of described alloy material forms by atomic percentage conc, iron 0-10at%, titanium 25-35at%, cobalt 10-15at%.
As further improvement, it is nickel 50at% that each of described alloy material forms by atomic percentage conc, iron 5at%, titanium 35at%, cobalt 10at%.
Described a kind of superelastic alloy material preparation method specifically may further comprise the steps:
1), choose the nickel of purity 〉=99.9%, purity 〉=99.99% cobalt, the iron of purity 〉=99.9%, the titanium of purity 〉=99.9% is prepared burden above-mentioned materials according to atomic percentage conc, then put into smelting furnace and be evacuated to 2.0 * 10
-4Pa is filled with argon gas again, inhales casting with mold cools down after the melt back and obtains alloy blank;
2), with 1) in the alloy blank sealing that obtains, be evacuated to 5.0 * 10
-5Pa 1000 ℃ of lower insulations 72 hours, then is cooled to room temperature and obtains the superelastic alloy material.
What described smelting furnace adopted is the non-consumable vacuum arc melting furnace.
Described cooling to be at the uniform velocity being cooled to the master, rate of cooling remain on 2.5-5 ℃ per 15 minutes, this rate of cooling will remain to the blank drop in temperature to 450-500 ℃.
The invention has the beneficial effects as follows:
1, the alloy material of the technical program not only has the alloy material that narrow hysteresis elastic performance can keep again shape memory effect.
2, the production technique of the technical program is simple, is easy to suitability for industrialized production.
Embodiment
Below by embodiment technical scheme of the present invention is elaborated.
A kind of superelastic alloy material, it is nickel 45-55at% that each of described alloy material forms by atomic percentage conc, iron 0-10at%, titanium 25-35at%, cobalt 10-15at%.
As further improvement, it is nickel 50at% that each of described alloy material forms by atomic percentage conc, iron 5at%, titanium 35at%, cobalt 10at%.
Described a kind of superelastic alloy material preparation method specifically may further comprise the steps:
1), choose the nickel of purity 〉=99.9%, purity 〉=99.99% cobalt, the iron of purity 〉=99.9%, the titanium of purity 〉=99.9% is prepared burden above-mentioned materials according to atomic percentage conc, then put into the non-consumable vacuum arc melting furnace and be evacuated to 2.0 * 10
-4Pa is filled with argon gas again, inhales casting with mold cools down after the melt back and obtains alloy blank;
2), with 1) in the alloy blank sealing that obtains, be evacuated to 5.0 * 10
-5Pa 1000 ℃ of lower insulations 72 hours, then is cooled to room temperature and obtains the superelastic alloy material.
Described cooling to be at the uniform velocity being cooled to the master, rate of cooling remain on 2.5-5 ℃ per 15 minutes, this rate of cooling will remain to the blank drop in temperature to 450-500 ℃.The result who does like this is can keep the interior crystalline structure of alloy even, and each particle that forms in unit volume is roughly the same, reduces the in-fighting of energy.
Embodiment 1
Each composition of choosing described alloy material is nickel 50at% by atomic percentage conc, iron 5at%, titanium 35at%, cobalt 10at%.
1), choose the nickel of purity 〉=99.9%, purity 〉=99.99% cobalt, the iron of purity 〉=99.9%, the titanium of purity 〉=99.9% is prepared burden above-mentioned materials according to atomic percentage conc, then put into the non-consumable vacuum arc melting furnace and be evacuated to 2.0 * 10
-4Pa is filled with argon gas again, inhales casting with mold cools down after the melt back and obtains alloy blank;
2), with 1) in the alloy blank sealing that obtains, be evacuated to 5.0 * 10
-5Pa 1000 ℃ of lower insulations 72 hours, then is cooled to room temperature and obtains the superelastic alloy material.
Described cooling to be at the uniform velocity being cooled to the master, rate of cooling remain on 3.5 ℃ per 15 minutes, this rate of cooling will remain to blank drop in temperature to 450 ℃.
The vicissitudinous final temp that the atomic percentage conc of each composition material and rate of cooling is in process of production arranged and keep rate of cooling in following embodiment, it is identical therefore only to form the variation other side by material in embodiment 1-3; In embodiment 4-6 except each material form change, rate of cooling and keep the final temp of rate of cooling to change with embodiment 1-3 but the final temp of rate of cooling in embodiment 4-6 and maintenance rate of cooling is identical.
Embodiment 2
Each composition of choosing described alloy material is nickel 55at% by atomic percentage conc, iron 5at%, titanium 30at%, cobalt 10at%.
Embodiment 3
Each composition of choosing described alloy material is nickel 45at% by atomic percentage conc, iron 10at%, titanium 30at%, cobalt 15at%.
Embodiment 4
Each composition of choosing described alloy material is nickel 48at% by atomic percentage conc, iron 10at%, titanium 30at%, cobalt 12at%.Rate of cooling remain on 5 ℃ per 15 minutes, this rate of cooling will remain to blank drop in temperature to 500 ℃.
Embodiment 5
Each composition of choosing described alloy material is nickel 55at% by atomic percentage conc, iron 10at%, titanium 25at%, cobalt 10at%.Rate of cooling remain on 5 ℃ per 15 minutes, this rate of cooling will remain to blank drop in temperature to 500 ℃.
Embodiment 6
Each composition of choosing described alloy material is nickel 50at% by atomic percentage conc, iron 10at%, titanium 25at%, cobalt 15at%.Rate of cooling remain on 5 ℃ per 15 minutes, this rate of cooling will remain to blank drop in temperature to 500 ℃.
The performance of each component alloy of embodiment 1-6 sees Table 1
Table 1
| Embodiment | Recoverable strain a | Maximum strain hysteresis b | b/a |
| Embodiment 1 | 7.62 | 3.25 | 0.427 |
| Embodiment 2 | 6.84 | 2.97 | 0.434 |
| Embodiment 3 | 6.78 | 3.06 | 0.451 |
| Embodiment 4 | 5.32 | 4.03 | 0.758 |
| Embodiment 5 | 4.13 | 2.14 | 0.518 |
| Embodiment 6 | 5.16 | 2.23 | 0.432 |
The present invention includes but be not limited to present embodiment, every being equal to of carrying out under rule of the present invention, replace or local improvement all should be considered as protection scope of the present invention.
Claims (5)
1. superelastic alloy material is characterized in that: it is nickel 45-55at% that each of described alloy material forms by atomic percentage conc, iron 0-10at%, titanium 25-35at%, cobalt 5-15at%.
2. described superelastic alloy material according to claim 1, it is characterized in that: it is nickel 50at% that each of described alloy material forms by atomic percentage conc, iron 5at%, titanium 35at%, cobalt 10at%.
3. described superelastic alloy material preparation method according to claim 1 is characterized in that: specifically may further comprise the steps:
1), choose the nickel of purity 〉=99.9%, purity 〉=99.99% cobalt, the iron of purity 〉=99.9%, the titanium of purity 〉=99.9% is prepared burden above-mentioned materials according to atomic percentage conc, then put into smelting furnace and be evacuated to 2.0 * 10
-4Pa is filled with argon gas again, inhales casting with mold cools down after the melt back and obtains alloy blank;
2), with 1) in the alloy blank sealing that obtains, be evacuated to 5.0 * 10
-5Pa 1000 ℃ of lower insulations 72 hours, then is cooled to room temperature and obtains the superelastic alloy material.
4. described superelastic alloy material preparation method according to claim 3, it is characterized in that: what described smelting furnace adopted is the non-consumable vacuum arc melting furnace.
5. described superelastic alloy material preparation method according to claim 3 is characterized in that: described cooling to be at the uniform velocity being cooled to the master, rate of cooling remain on 2.5-5 ℃ per 15 minutes, this rate of cooling will remain to the blank drop in temperature to 450-500 ℃.
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102851562A (en) * | 2012-09-14 | 2013-01-02 | 虞海香 | Superelastic memory alloy and preparation method thereof |
| CN102851543A (en) * | 2012-09-14 | 2013-01-02 | 虞海香 | Hyperelastic memory alloy |
| CN102864360A (en) * | 2012-09-14 | 2013-01-09 | 虞海盈 | Super elastic alloy material and preparation method thereof |
| CN102864359A (en) * | 2012-09-14 | 2013-01-09 | 虞海盈 | Super elastic alloy material |
| CN104342568A (en) * | 2014-10-14 | 2015-02-11 | 杨雯雯 | Preparation method of elastic alloy |
| CN104357689A (en) * | 2014-10-14 | 2015-02-18 | 熊荣鑫 | Preparation method of elastic alloy material |
Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110277568A1 (en) * | 2009-11-02 | 2011-11-17 | Saes Smart Materials | Ni-Ti SEMI-FINISHED PRODUCTS AND RELATED METHODS |
| CN102337424A (en) * | 2011-09-16 | 2012-02-01 | 北京理工大学 | Nickel-cobalt-iron-gallium hyperelastic alloy material and preparation method thereof |
-
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- 2012-09-05 CN CN2012103273285A patent/CN102864341A/en active Pending
Patent Citations (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20110277568A1 (en) * | 2009-11-02 | 2011-11-17 | Saes Smart Materials | Ni-Ti SEMI-FINISHED PRODUCTS AND RELATED METHODS |
| CN102337424A (en) * | 2011-09-16 | 2012-02-01 | 北京理工大学 | Nickel-cobalt-iron-gallium hyperelastic alloy material and preparation method thereof |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102851562A (en) * | 2012-09-14 | 2013-01-02 | 虞海香 | Superelastic memory alloy and preparation method thereof |
| CN102851543A (en) * | 2012-09-14 | 2013-01-02 | 虞海香 | Hyperelastic memory alloy |
| CN102864360A (en) * | 2012-09-14 | 2013-01-09 | 虞海盈 | Super elastic alloy material and preparation method thereof |
| CN102864359A (en) * | 2012-09-14 | 2013-01-09 | 虞海盈 | Super elastic alloy material |
| CN104342568A (en) * | 2014-10-14 | 2015-02-11 | 杨雯雯 | Preparation method of elastic alloy |
| CN104357689A (en) * | 2014-10-14 | 2015-02-18 | 熊荣鑫 | Preparation method of elastic alloy material |
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Application publication date: 20130109 |