CN1386878A - Magnetically controlled Co-Ni-monocrystal marmen - Google Patents
Magnetically controlled Co-Ni-monocrystal marmen Download PDFInfo
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- CN1386878A CN1386878A CN 02111297 CN02111297A CN1386878A CN 1386878 A CN1386878 A CN 1386878A CN 02111297 CN02111297 CN 02111297 CN 02111297 A CN02111297 A CN 02111297A CN 1386878 A CN1386878 A CN 1386878A
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- marmen
- monocrystalline
- monocrystal
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Abstract
A magnetically controlled marmen contains Ni (10-35 wt.%) and Co (65-90 wt.%), and is prepared from direction (001) seed crystal through pull method or floating zone method to obtain monocrystal, heating at 700-950 deg.c, quenching and heat treating in magnetic field. Its advantages are high magnetic strain capacity, high response speed and high plasticity.
Description
Technical field:
The present invention relates to a kind of magnetically controlled Co-Ni-monocrystal marmen, can be used for occasions such as automatic control, energy transformation and make actuator material, belong to the new function material technical field.
Background technology:
The general shape memorial alloy is to be out of shape under the stress field effect, and unloading back shape is replied (super-elasticity) or a kind of functional materials of the back recovery of shape (shape memory effect) of heating fully.It has obtained to use widely in fields such as control automatically, machinery, communication, medical devices.Its advantage is that the output skew amount is big.Yet response frequency is low.And piezoelectric ceramics and magnetostriction materials, strain also can take place in them under the effect in stress or magnetic field, and its response frequency is very high, but the output strain is very little.Piezoelectric ceramics PZT for example, the output strain only is 0.1% order of magnitude; (Fe2), the field causes strain and is about 0.24% because the output displacement is little at present best commercial magnetostriction materials Terfenol-D, has restricted output energy density and propagation distance for Tb0.27, Dy0.73.As seen develop a kind of new function material, make it both have piezoelectric ceramics and the such fast response frequency of magnetostriction materials, can as shape memory alloy, export big strain again, all have major application to be worth civilian and military.For example develop high-power sonar, can find target in farther distance.
Middle 1990s, a kind of mangneto shape-memory material arises at the historic moment.At first at nickel manganese gallium (Ni
2MnGa) find in the monocrystalline, when along [001] direction when temperature 265K applies 8kOe magnetic field, can bring out 0.2% strain (Ullakko K, Huang J.K, Kantner C, O ' Handley and Kokorin S.J, Appl.Phys.Lett.1996,69:1966～1968.).Afterwards to nonstoichiometry NiMnGa (Ni
49.8Mn
28.5Ga
21.7) monocrystalline, under room temperature, 4kOe magnetic field, bring out shearing strain can reach 6.0% (MurrayS.J, Marioni M, Allen S.M, O ' Handley R.C and Lograsso T.A, Appl.Phys.Lett.2000,77:886).Because NiMnGa is a kind of intermetallic compound, matter is crisp easily to be split, and during single crystal growing, Mn is volatile, makes the Composition Control difficulty, has restricted its actual use and large-scale production.
Summary of the invention:
The objective of the invention is at the deficiencies in the prior art, a kind of solid solution alloy-magnetically controlled Co-Ni-monocrystal marmen is provided, make its magneto-strain amount far above existing commercial magnetostriction materials, response frequency is fast simultaneously, plasticity is good, can carry out cold and hot working, has more using value.
For realizing such purpose, technical scheme of the present invention is as follows:
1, She Ji alloying constituent weight percent is: nickel 10%～35%, cobalt Co 65%～90%.In this composition range, material is a sosoloid, and has the martensitic transformation from face-centered cubic (fcc) to close-packed hexagonal (hcp).If Ni content surpasses 35% (weight), martensite point M
sWill be below 100K, magnetic correspondingly can take place, and to bring out the strained temperature also very low, no industrial application value.Reduce with Ni content, martensite point raises gradually.If but Ni content is lower than 10% (weight), martensite is named a person for a particular job and is higher than 673K, almost all is martensitic stucture at room temperature, and magnetic brings out strain can only be by the reorientation of martensite variants, and can not produce by bringing out new martensite, magnetic brings out dependent variable can be reduced.
2, producing axially is the monocrystalline of [001].Adopt the seed crystal of [001] direction to prepare with crystal pulling method preparation or employing floating zone melting method, the speed of growth is controlled to be 1～10mm/ hour.
3, with the monocrystalline of preparation through quenching heat treatment after 700-950 ℃ of heat, in intensity be then+2T～-magnetic field of 2T under, make material be cooled to martensitic transformation end temp M from parent phase
fBelow, or under the action of a magnetic field at M
fBelow and reverse transformation end temp A
fMore than between cooling heating repeatedly, carry out thermomagnetic treatment.
The alloy that the present invention obtains produces the mechanism of huge magneto-strain, the easy magnetization axis that is this alloy system is [111], when along [001] when direction applies magnetic field, the trend that the crystal face of easy magnetization axis rotates oriented outer magnetic field direction in the crystal, thereby 1/6＜211〉partial dislocation on [111] face of driving is moved, the process that causes similar stress-induced six side's martensites to produce, also can make six side's martensite variants of the favourable orientation that has existed, by 1/6＜211〉partial dislocation to move forward into a step-length big, increase, form the monotropic body of favourable orientation, bring out strain thereby produce considerable magnetic field.
New magnetic provided by the invention brings out the strain alloy monocrystalline, its magneto-strain amount can reach 1～5%, surpass best commercial magnetostriction materials Terfenol-D several times to tens times, and frequency response reaches tens of kilohertzs, composition is easy to control, plasticity is good, can carry out cold and hot working, can stand repeatedly alternating magnetic field and bring out strain.
Description of drawings and embodiment:
Below by accompanying drawing and specific embodiment technical scheme of the present invention is further described.
Alloy magnetic field one strain figure that Fig. 1 prepares for the embodiment of the invention 1.
Be Co-31.5% (weight) monocrystalline shown in the figure, at room temperature, apply 1.2T magnetic field, can produce 4.2% strain, after the removal foreign field, 0.2% residual deformation is only arranged along [001] crystal orientation.
Embodiment 1:
With purity is that 99.95% electrolysis Ni and electrolysis Co are mixed with Co-31.5% (weight) Ni alloy, clean through careful, remove surface and oil contaminant and oxide compound, in vacuum non-consumable arc furnace, be smelted into the button-type ingot, melt back 3 times, even to guarantee composition, instil into Φ 10mm * 110mm polycrystalline garden rod again, use for the preparation monocrystalline.Adopt optical levitation zone melting stove, the speed of growth is controlled to be 5mm/ hour, and making axially is the monocrystalline of [001].Through 800 ℃ of quenchings, be as cold as room temperature soon, its M
sPoint is 261.5K, A
s=445K is cooled to 77K (M under 1kOe magnetic field
fFollowing temperature).At room temperature the saturation magnetization along parent phase [001] crystal orientation can reach 120Am
2Kg
-1More than, and only need the foreign field of 3kOe, can reach saturated.
Present embodiment gained alloy applies foreign field along [001] direction, can bring out nearly 3.5% strain to 8kOe, and strain is replied fully after the removal foreign field.Unload magnetic field tens of times through adding repeatedly, strain produces same numerical value repeatedly.When applying the 1.2T foreign field, can detect 4.2% strain, after the removal foreign field, 0.2% residual deformation is only arranged, as shown in Figure 1.
Embodiment 2:
In Co 67% and Ni 33% (weight) ratio alloyage, place crucible with high pure raw material, heat fused under vacuum remains on the fusing point of a little higher than alloy its temperature.To have [001] axial seed crystal and just drop to and contact with liquid level, and make its local melting, and then slowly reduce crucible temperature, and lift while seed crystal is rotated upwards, control growing speed is 5mm/ hour, makes monocrystalline.This alloy martensite transformation temperature M
s=174.8K, reverse transformation temperature A
s=382.8K after thermal treatment and magnetic field treatment, applies foreign field along [001] direction, below 180K, can bring out 1～3% reversible strain.
Embodiment 3:
Make Co-15.1%Ni (weight) monocrystalline, martensitic transformation temperature Ms=569.4K, reverse transformation temperature As=649.5K with embodiment 1 with quadrat method, after heating is cooled off repeatedly under magnetic field, apply foreign field along [001] direction,, can bring out 1～3% strain in room temperature.
Claims (3)
1, a kind of magnetically controlled Co-Ni-monocrystal marmen is characterized in that the composition weight percent is: nickel 10%～35%, cobalt Co 65%～90%, monocrystalline axially are [001].
2, a kind of preparation method of magnetically controlled Co-Ni-monocrystal marmen, it is characterized in that getting the alloying constituent weight percent is: nickel 10%～35%, cobalt Co 65%～90%, produce axially for behind the monocrystalline of [001], with quenching heat treatment after 700-950 ℃ of heat of monocrystalline process, in intensity be then+magnetic field of 2T～2T under, make material be cooled to martensitic transformation end temp M from parent phase
fBelow, or under the action of a magnetic field at M
fBelow and reverse transformation end temp A
fMore than between cooling heating repeatedly, carry out thermomagnetic treatment.
3, as the preparation method of the said magnetically controlled Co-Ni-monocrystal marmen of claim 2, when it is characterized in that producing monocrystalline, adopt the seed crystal of [001] direction to prepare with crystal pulling method preparation or employing floating zone melting method, the speed of growth is controlled to be 1～10mm/ hour.
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| Application Number | Priority Date | Filing Date | Title |
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| CNB021112975A CN1169983C (en) | 2002-04-09 | 2002-04-09 | Magnetically controlled Co-Ni-monocrystal marmen |
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| CNB021112975A CN1169983C (en) | 2002-04-09 | 2002-04-09 | Magnetically controlled Co-Ni-monocrystal marmen |
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| CN1386878A true CN1386878A (en) | 2002-12-25 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101305109B (en) * | 2005-11-09 | 2011-09-28 | 独立行政法人科学技术振兴机构 | Iron-based alloy having shape-memory property and superelasticity and method for manufacture thereof |
| CN102918673A (en) * | 2010-05-28 | 2013-02-06 | Eto电磁有限责任公司 | Method for producing a monocrystalline body from a magnetic shape memory alloy |
| CN105353610A (en) * | 2015-10-10 | 2016-02-24 | 吉林大学 | Magnetic-control shape memory alloy actuator modeling method based on KP model |
-
2002
- 2002-04-09 CN CNB021112975A patent/CN1169983C/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101305109B (en) * | 2005-11-09 | 2011-09-28 | 独立行政法人科学技术振兴机构 | Iron-based alloy having shape-memory property and superelasticity and method for manufacture thereof |
| CN102918673A (en) * | 2010-05-28 | 2013-02-06 | Eto电磁有限责任公司 | Method for producing a monocrystalline body from a magnetic shape memory alloy |
| CN102918673B (en) * | 2010-05-28 | 2015-04-29 | Eto电磁有限责任公司 | Method for producing a monocrystalline body from a magnetic shape memory alloy |
| CN105353610A (en) * | 2015-10-10 | 2016-02-24 | 吉林大学 | Magnetic-control shape memory alloy actuator modeling method based on KP model |
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| CN1169983C (en) | 2004-10-06 |
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