CN107142419A - A kind of preparation method of LaFeSiH materials - Google Patents

A kind of preparation method of LaFeSiH materials Download PDF

Info

Publication number
CN107142419A
CN107142419A CN201710255250.3A CN201710255250A CN107142419A CN 107142419 A CN107142419 A CN 107142419A CN 201710255250 A CN201710255250 A CN 201710255250A CN 107142419 A CN107142419 A CN 107142419A
Authority
CN
China
Prior art keywords
alloy
powder
flushed
hydrogen
lafesih
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201710255250.3A
Other languages
Chinese (zh)
Inventor
王占洲
孙永阳
章晓峰
洪群峰
韩相华
郝忠彬
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hengdian Group DMEGC Magnetics Co Ltd
Original Assignee
Hengdian Group DMEGC Magnetics Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hengdian Group DMEGC Magnetics Co Ltd filed Critical Hengdian Group DMEGC Magnetics Co Ltd
Priority to CN201710255250.3A priority Critical patent/CN107142419A/en
Publication of CN107142419A publication Critical patent/CN107142419A/en
Pending legal-status Critical Current

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/005Ferrous alloys, e.g. steel alloys containing rare earths, i.e. Sc, Y, Lanthanides
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C33/00Making ferrous alloys
    • C22C33/02Making ferrous alloys by powder metallurgy
    • C22C33/0257Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
    • C22C33/0278Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/002Ferrous alloys, e.g. steel alloys containing In, Mg, or other elements not provided for in one single group C22C38/001 - C22C38/60
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/02Ferrous alloys, e.g. steel alloys containing silicon
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/04Ferrous alloys, e.g. steel alloys containing manganese
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01FMAGNETS; INDUCTANCES; TRANSFORMERS; SELECTION OF MATERIALS FOR THEIR MAGNETIC PROPERTIES
    • H01F1/00Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties
    • H01F1/01Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials
    • H01F1/012Magnets or magnetic bodies characterised by the magnetic materials therefor; Selection of materials for their magnetic properties of inorganic materials adapted for magnetic entropy change by magnetocaloric effect, e.g. used as magnetic refrigerating material

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Power Engineering (AREA)
  • Hard Magnetic Materials (AREA)
  • Powder Metallurgy (AREA)

Abstract

The invention discloses a kind of preparation method of LaFeSiH materials.It specifically includes following steps:(1) La is chosen1‑xRx(Fe13‑y‑bMy)SibHcAlloy is flushed with hydrogen powder;(2) bonding agent being mixed to get in proportion using epoxy resin and curing agent;(3) with bonding agent and alloy be flushed with hydrogen powder and be put into container, and pour into acetone as solvent, be stirred, being flushed with hydrogen powder after bonding agent and alloy is well mixed and after acetone volatilizees, is granulated, re-compacted shaping;(4) sample after being molded solidifies at low temperature, and wherein low temperature is not higher than 80 DEG C.The beneficial effects of the invention are as follows:While the intensity and performance of alloy is ensured, moreover it is possible to ensure alloy not dehydrogenation, the performance of magnetic refrigerating material is not influenceed, and adiabatic temperature becomes, Curie temperature and magnetic entropy become and can be guaranteed.

Description

A kind of preparation method of LaFeSiH materials
Technical field
The present invention relates to magnetic refrigerating material correlative technology field, a kind of preparation method of LaFeSiH materials is referred in particular to.
Background technology
Room temperature magnetic refrigerating technology has environmental protection, it is energy-efficient, reliable and stable the characteristics of, generation has been caused in the last few years The extensive concern of boundary's scope.Society always consumes energy more than 15% is accounted for because refrigeration industry consumes energy, and is used in vapor compression refrigeration Gas refrigerant can destroy atmospheric ozone layer and cause greenhouse effects, so the advantage that room-temperature magnetic refrigerator possesses so that this Technology is expected to replace traditional vapor compression refrigeration.Several type high temps or even room temperature that the U.S., China, Holland, Japan find in succession Area's materials with the giant magnetocaloric effect has promoted expectation of the people to environmental protection magnetic Refrigeration Technique significantly, for example:Gd-Si-Ge、LaCaMnO3、 The compound such as the based compound of Ni-Mn-Ga, La (Fe, Si) 13, Mn-Fe-P-As, MnAs.These new giant magnetio-caloric effects materials Common feature is that magnetic entropy change is above traditional room temperature magnetic refrigerating material Gd, and phase transition property is one-level, and majority is presented strongly Magnetocrystalline coupling characteristics, magnetic phase transition with significant crystal structure phase transformation generation.These new materials also show different materials Expect characteristic, for example, Gd-Si-Ge is expensive, needed in preparation process to the further purification of raw material, Mn-Fe-P-As, MnAs It is poisonous etc. Deng compound starting material.
The research of room-temperature magnetic refrigerator and application are also constantly improving, the U.S., China, France, Britain, Italy, Denmark, Canada, Japan, Spain etc. have developed various room-temperature magnetic refrigerators in succession.Room-temperature magnetic refrigerator uses electromagnetism at first Iron or superconductor make magnetic field, but superconduction and electromagnet are expensive, and maintenance cost is high, is restricted for commercialization.At present, The magnetic field of room-temperature magnetic refrigerator is provided by permanent magnet, while realizing high-power, high-frequency.
With the development of room-temperature magnetic refrigerator, it is believed that in magnetic refrigerating material, most application prospect is LaFeSi systems Alloy.It is frangible and the first order phase change magnetic refrigerating material that LaFeSi systems alloy is obtained after being flushed with hydrogen can become very crisp.So magnetothermal effect The shaping of material also turns into the problem of needing urgent solve.Magnetic refrigerating material in the regenerator of magnetic refrigerator needs to be processed into Type, is made required shape, this needs is bonded together powdered LaFeSi materials with adhesive, and retentivity as far as possible Can, re-compacted shaping makes moulded products keep high intensity by techniques such as solidifications.And conventionally used bonding agent needs to solidify temperature 80-180 DEG C of degree, heats 0.5h-2h in this temperature range, can lose substantial amounts of hydrogen atom, cause the LaFeSi systems of first order phase change Alloy property is reduced, and influences the performance of magnetic refrigerating material, and adiabatic temperature change, Curie temperature and magnetic entropy become and can all declined.
The content of the invention
The present invention is above-mentioned to ensure alloy not dehydrogenation and property there is provided one kind to overcome the shortcomings of to exist in the prior art The preparation method of constant LaFeSiH materials can be kept.
To achieve these goals, the present invention uses following technical scheme:
A kind of preparation method of LaFeSiH materials, specifically includes following steps:
(1) La is chosen1-xRx(Fe13-y-bMy)SibHcAlloy is flushed with hydrogen powder;
(2) bonding agent being mixed to get in proportion using epoxy resin and curing agent;
(3) bonding agent matched somebody with somebody is flushed with hydrogen powder with alloy and is put into container, and pours into acetone as solvent, is stirred, After bonding agent and alloy be flushed with hydrogen powder be well mixed and after acetone volatilization after, granulated, re-compacted shaping;
(4) sample after being molded solidifies at low temperature, and wherein low temperature is not higher than 80 DEG C.
It can make to lose substantial amounts of hydrogen in alloy using hot setting in the curing process, so the present invention is by using epoxy instead The solidification bonding agent that resin and curing agent proportioning are obtained, its solidification temperature is not more than 80 DEG C, and the intensity and performance of such alloy can To be guaranteed simultaneously, alloy not dehydrogenation is also ensured in addition.
Preferably, in step (1), R is one or several kinds of compositions of following rare earth elements, the rare earth member Element is:Ce、Pr、Nd、Sm、Eu、Gd、Tb、Dy、Ho、Er、Tm、Yb、Lu、Sc、Y;X scope is:0≤x≤0.3;M be Mn, One kind in Ti, V, Cr, Co, Ni, Cu, Zn, Ga;Y scope is:0.003≤y≤0.5;B scope is:1.0≤b≤1.5; C scope is:0≤c≤3.0.
Preferably, in step (1), La1-xRx(Fe13-y-bMy)SibHcThe powder diameter control that alloy is flushed with hydrogen powder exists Less than 300 μm.If powder diameter is too big, mobility is too poor in pressing process, is molded for the more box-shaped pressed compact of seamed edge It is difficult.
Preferably, in step (2), the ratio of epoxy resin and curing agent is 1~2: 1.
Preferably, in step (2), bonding agent accounts for alloy and is flushed with hydrogen the mass fraction of powder for 1.5%-3%.If viscous The mass fraction for connecing agent is too high, then alloy powder viscosity is too big, is unfavorable for granulation.
The beneficial effects of the invention are as follows:While the intensity and performance of alloy is ensured, moreover it is possible to ensure alloy not dehydrogenation, no The performance of magnetic refrigerating material is influenceed, adiabatic temperature becomes, Curie temperature and magnetic entropy become and can be guaranteed.
Brief description of the drawings
Fig. 1 is La0.7Ce0.3Fe11.30Mn0.20Si1.5HxIt is flushed with hydrogen the Entropy Changes and temperature relation figure of powder;
Fig. 2 is La0.7Ce0.3Fe11.30Mn0.20Si1.5HxAlloy is using the Entropy Changes after the solidification of room temperature curing agent bonding sheet and temperature Spend graph of a relation;
Fig. 3 is La0.7Ce0.3Fe11.30Mn0.20Si1.5HxAlloy is using the Entropy Changes after the solidification of high-temperature curing agent bonding sheet and temperature Spend graph of a relation;
Fig. 4 is La0.7Ce0.3Fe11.4Mn0.28i1.4HxWith La0.7Ce0.3Fe11.45Mn0.15Si1.4HxTwo kinds of curie points are flushed with hydrogen Alloy powder and the thermal insulation temperature of each self-corresponding compressing become graph of a relation.
Wherein:Fig. 1, Fig. 2 and Fig. 3 abscissa all represent temperature, and using Kelvin, unit is used as using K;Ordinate Represent Entropy Changes value Δ S, unit Jkg-1K-1.The corresponding abscissa of the peak value of curve represents Curie temperature in figure.Same figure In three curves be respectively the corresponding different temperatures under three kinds of magnetic flux densities (0.5T, 0.8T, 1T) Entropy Changes value.In Fig. 4 Powder 1 (closed square, solid line) represents La respectively with piece 1 (hollow square, dotted line)0.7Ce0.3Fe11.4Mn0.2Si1.4HxMaterial is consolidated Powder and solidification aftershaping piece before changing, powder 2 (filled circles, solid line) are represented respectively with piece 2 (open circles, dotted line) La0.7Ce0.3Fei1.45Mn0.15Si1.4HxPowder and solidification aftershaping piece before material solidification;Abscissa represents temperature and uses Kelvin temperature Degree, using K as unit, ordinate represents adiabatic temperature change Δ T, unit K or DEG C.
Embodiment
The present invention will be further described with reference to the accompanying drawings and detailed description.
LaFeSiH alloy powders to keep its excellent performance, then need when the regenerator of magnetic refrigerator is made Ensure alloy not dehydrogenation, so 80 DEG C of bonding agent should be not higher than using solidification temperature.So, the intensity and performance of alloy can To ensure simultaneously.Choose La1-xCex(Fe13-y-bMny)SibHcAlloy is flushed with hydrogen powder 50g and makees molded test, wherein:X scope It is:0≤x≤0.5, y scope is:0.003≤y≤0.5, b scope is:1.0≤b≤1.5, c scope is:0≤c≤ 3.0.Alloy is flushed with hydrogen the control of the powder diameter of powder below 300 μm, if powder diameter is too big, in pressing process, mobility is too Difference, for the more box-shaped pressed compact difficult forming of seamed edge.Here the alloy chosen is flushed with hydrogen powder La0.7Ce0.3Fe11.30Mn0.20Si1.5Hx
Using E44 epoxy resin and the polyamide of curing agent 650 1: 1 bonding agent being mixed to get in proportion, quality point Number is 2.5%.With bonding agent and alloy powder be put into container, and pour into acetone as solvent, be stirred, wait to be bonded Agent is well mixed with alloy powder and after after acetone volatilization, granulated, re-compacted shaping, the sample after shaping is at 40 DEG C or so Solidification, Entropy Changes is held essentially constant, and data are shown in Table 1, and the Entropy Changes value under 0.8T magnetic field intensities is 8.85Jkg-1K-1, is occupied In temperature be 287K.Curve is as depicted in figs. 1 and 2.
Rear powder 50g is flushed with hydrogen with identical LaFeSiH series alloy powders, using E51 epoxy resin and dicy-curing agent The bonding agent of mixing, both ratios are according to 5: 1, and the mass fraction of bonding agent is 2.5%.Bonding agent is put into container with alloy powder In, and acetone is poured into as solvent, it is stirred, is well mixed and after acetone volatilization, is made with alloy powder after bonding agent Grain, re-compacted shaping, the sample after shaping solidifies at 160 DEG C, and the hydrogen content in sample is decreased obviously, in 0.8T magnetic field intensities 8.93Jkg-1K-1 of the lower Entropy Changes value before solidifying is reduced to 4.93Jkg-1K-1 after solidification.As shown in Figure 3.
Choose La0.7Ce0.3Fe11.30Mn0.20Si1.5HxPowder is flushed with hydrogen, is mixed with E51 epoxy resin with dicy-curing agent Bonding agent, both ratios are according to 5: 1, and the mass fraction of bonding agent is 2.5%.Bonding agent and alloy powder are all put into container In, and acetone is poured into as solvent, it is stirred, treats that bonding agent is well mixed acetone volatilization with alloy powder, granulated, made Alloy powder after grain, tests hydrogen content, and hydrogen mass fraction is 0.3857%;LaFeSiH systems alloy after shaping is made at solidification Reason, treats that sample is fully cured, and the mass fraction for measuring hydrogen content is 0.3392%.It can be seen that metal dust matrix band is solid Hydrogen content change before and after changing, the hydrogen content after solidification in alloy declines, and hot setting causes dehydrogenation in alloy, the performance of alloy It can decline therewith.
In order to obtain optimal solidification effect, do tests below not influenceing metal to be flushed with hydrogen under the premise of the performance of powder. The proportioning of E44 epoxy resin and 650 polyamide curing agent is respectively adopted 1: 1,1.5: 1,2: 1;The mass fraction of bonding agent It is 2.5%, 3%, solidification temperature uses 160 DEG C, 80 DEG C and 40 DEG C;10 minutes, 1 hour, 2 hours hardening time.It is measured Obtain the hydrogen content change of alloy powder, such as table 2.The proportioning of E44 epoxy resin and 650 polyamide curing agent be 1: 1, When 1.5: 1,2: 1, in the case of the mass fraction 2.5% of bonding agent, in bonding agent hydrogen content be respectively 0.194%, 0.158%th, 0.141%;In the case of the mass fraction 3% of bonding agent, in bonding agent hydrogen content be respectively 0.244%, 0.197%th, 0.175%.Through measuring the hydrogen content about 0.21% or so of such a alloy in itself.Hydrogen content includes three aspects, Protium in the protium of alloy in itself, bonding agent, the hydrogen content for also having remaining acetone.The protium of alloy powder after granulation Including this three, after being fully cured, it is believed that acetone volatilizees completely, the above two are only existed.If solidification temperature is too high, close The golden hydrogen of itself can overflow on a small quantity.And have two kinds the reason for reduced with the growth hydrogen content of hardening time, in the case of a high temperature Final hydrogen content, which is reduced, includes in two parts, a small amount of alloy hydrogen and acetone from being not completely evaporated into complete volatilization;At 40 DEG C In the case of left and right, hydrogen content changes over time the volatilization for being primarily due to acetone.Wherein 40 DEG C solidifications, final protium content Keep constant after acetone volatilizees completely, now the mass fraction of protium includes the protium in two parts, alloy in alloy With the protium in bonding agent.
Wherein, after 40 DEG C of temperatures above solidify 2 hours, hydrogen content and bonding agent after alloy solidification are granulated from table 2 Compared with the difference of hydrogen content and alloy powder itself hydrogen content 0.21%, it can be seen that hydrogen content has all declined in alloy, 40 DEG C solidification hydrogen content be held essentially constant.In order to improve intensity, high-temperature curing agent can not be using cryogenic temperature solidification.Therefore to select Selecting the solidification of 80 DEG C of temperature below can keep that hydrogen content is constant in alloy and can also meet the bonding agent of intensity requirement.
Meanwhile, in 160 DEG C of sheet samples solidified compared with the prilling powder before solidification, adiabatic temperature, which becomes Δ T, also to be had substantially Decline, the corresponding Curie temperature Tc of peak point that adiabatic temperature becomes also is decreased obviously.As shown in figure 4, powder 1 and powder 2 into It is respectively La0.7Ce0.3Fe11.4Mn0.2Si1.4HxWith La0.7Ce0.3Fe11.45Mn0.15Si1.4Hx;The powder that is flushed with hydrogen of two kinds of alloys exists It is 2.5K and 2.4K respectively that thermal insulation temperature under 0.8T magnetic field intensities, which becomes,.Two kinds of alloy materials are granulated with identical curing agent, compacting Slabbing sample, 160 DEG C solidify 1 hour after, measured under 0.8T magnetic field intensities thermal insulation temperature become be respectively 1.8K with 1.68K;Adiabatic temperature becomes the corresponding corresponding temperature of peak point also to be reduced respectively by original 283K (10 DEG C) and 293K (20 DEG C) For 272K (- 1 DEG C) and 283K (10 DEG C).The sheet sample for being flushed with hydrogen powder, hot setting of two kinds of materials is in 0.8T magnetic field intensities Under thermal insulation temperature become data be shown in Table 3.
Wherein:When the mass fraction of bonding agent is 3%, alloy powder viscosity is too big, is unfavorable for granulation.E44 epoxy resin It is much better in 1: 1 granulation outcome with 650 polyamide ratios.
The bond samples for being flushed with hydrogen powder, the sheet sample of hot setting and cold curing of the material of table 1 are strong in different magnetic field Entropy Changes under degree
Table it is 2-in-1 gold in hydrogen content with solidification temperature change
Thermal insulation temperature of the sheet sample for being flushed with hydrogen powder, hot setting of the material of table 3 under 0.8T magnetic field intensities becomes

Claims (5)

1. a kind of preparation method of LaFeSiH materials, it is characterized in that, specifically include following steps:
(1) La is chosen1-xRx(Fe13-y-bMy)SibHcAlloy is flushed with hydrogen powder;
(2) bonding agent being mixed to get in proportion using epoxy resin and curing agent;
(3) bonding agent matched somebody with somebody is flushed with hydrogen powder with alloy and is put into container, and pours into acetone as solvent, is stirred, waits to glue Connect agent and alloy and be flushed with hydrogen powder and be well mixed and after after acetone volatilization, granulated, re-compacted shaping;
(4) sample after being molded solidifies at low temperature, and wherein low temperature is not higher than 80 DEG C.
2. a kind of preparation method of LaFeSiH materials according to claim 1, it is characterized in that, in step (1), under R is One or several kinds of compositions of rare earth element are stated, the rare earth element is:Ce、Pr、Nd、Sm、Eu、Gd、Tb、Dy、Ho、 Er、Tm、Yb、Lu、Sc、Y;X scope is:0≤x≤0.5;M is one kind in Mn, Ti, V, Cr, Co, Ni, Cu, Zn, Ga;Y's Scope is:0.003≤y≤0.5;B scope is:1.0≤b≤1.5;C scope is:0≤c≤3.0.
3. a kind of preparation method of LaFeSiH materials according to claim 1 or 2, it is characterized in that, in step (1), La1-xRx(Fe13-y-bMy)SibHcAlloy is flushed with hydrogen the control of the powder diameter of powder below 300 μm.
4. a kind of preparation method of LaFeSiH materials according to claim 1, it is characterized in that, in step (2), epoxy The ratio of resin and curing agent is 1~2: 1.
5. a kind of preparation method of LaFeSiH materials according to claim 1 or 4, it is characterized in that, in step (2), glue Connect agent account for alloy be flushed with hydrogen powder mass fraction be 1.5%-3%.
CN201710255250.3A 2017-04-18 2017-04-18 A kind of preparation method of LaFeSiH materials Pending CN107142419A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201710255250.3A CN107142419A (en) 2017-04-18 2017-04-18 A kind of preparation method of LaFeSiH materials

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201710255250.3A CN107142419A (en) 2017-04-18 2017-04-18 A kind of preparation method of LaFeSiH materials

Publications (1)

Publication Number Publication Date
CN107142419A true CN107142419A (en) 2017-09-08

Family

ID=59774221

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201710255250.3A Pending CN107142419A (en) 2017-04-18 2017-04-18 A kind of preparation method of LaFeSiH materials

Country Status (1)

Country Link
CN (1) CN107142419A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109378148A (en) * 2018-07-25 2019-02-22 中国科学院宁波材料技术与工程研究所 A kind of lanthanum iron silicon substrate magnetic refrigerating material and preparation method thereof
CN112885549A (en) * 2021-01-08 2021-06-01 哈尔滨工业大学 Preparation method of magnetic phase change material of regenerator of magnetic refrigerator and magnetic refrigeration circulating system
CN115368711A (en) * 2022-08-11 2022-11-22 湖北航泰科技有限公司 Strong magnetocaloric effect fast curing epoxy resin

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102964774A (en) * 2012-10-16 2013-03-13 横店集团东磁股份有限公司 Manufacturing method of soft magnetic alloy composite material
CN103137281A (en) * 2011-11-22 2013-06-05 中国科学院物理研究所 Bonding La (Fe, Si) 13 base magnetocaloric effect material and preparation method and use thereof
CN104332301A (en) * 2014-11-25 2015-02-04 湖南航天磁电有限责任公司 Method for preparing bonded NdFeB permanent magnet
CN105957672A (en) * 2016-01-19 2016-09-21 包头稀土研究院 Lanthanum-iron-silicon-based hydride magnetic refrigerant, preparation method of lanthanum-iron-silicon-based hydride magnetic refrigerant and magnetic refrigerator

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103137281A (en) * 2011-11-22 2013-06-05 中国科学院物理研究所 Bonding La (Fe, Si) 13 base magnetocaloric effect material and preparation method and use thereof
CN102964774A (en) * 2012-10-16 2013-03-13 横店集团东磁股份有限公司 Manufacturing method of soft magnetic alloy composite material
CN104332301A (en) * 2014-11-25 2015-02-04 湖南航天磁电有限责任公司 Method for preparing bonded NdFeB permanent magnet
CN105957672A (en) * 2016-01-19 2016-09-21 包头稀土研究院 Lanthanum-iron-silicon-based hydride magnetic refrigerant, preparation method of lanthanum-iron-silicon-based hydride magnetic refrigerant and magnetic refrigerator

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109378148A (en) * 2018-07-25 2019-02-22 中国科学院宁波材料技术与工程研究所 A kind of lanthanum iron silicon substrate magnetic refrigerating material and preparation method thereof
CN109378148B (en) * 2018-07-25 2020-12-15 中国科学院宁波材料技术与工程研究所 Lanthanum-iron-silicon-based magnetic refrigeration material and preparation method thereof
CN112885549A (en) * 2021-01-08 2021-06-01 哈尔滨工业大学 Preparation method of magnetic phase change material of regenerator of magnetic refrigerator and magnetic refrigeration circulating system
CN112885549B (en) * 2021-01-08 2022-09-20 哈尔滨工业大学 Preparation method of magnetic phase change material of regenerator of magnetic refrigerator and magnetic refrigeration circulating system
CN115368711A (en) * 2022-08-11 2022-11-22 湖北航泰科技有限公司 Strong magnetocaloric effect fast curing epoxy resin

Similar Documents

Publication Publication Date Title
CN103137281B (en) Bonding La (Fe, Si)13Base magnetothermal effect material and its production and use
EP3031057B1 (en) Magnetocaloric materials containing b
Shen et al. A novel hard magnetic material for sintering permanent magnets
CN107142419A (en) A kind of preparation method of LaFeSiH materials
JP6480933B2 (en) Magneto-caloric material containing B
EP3031058B1 (en) Magnetocaloric materials containing b
CN107689278A (en) A kind of La Fe Si base magnetic refrigeration composite materials and preparation method thereof
CN111564305B (en) Preparation method of high-performance composite magnet
Zhong et al. Table-like magnetocaloric effect and enhanced refrigerant capacity of HPS La (Fe, Si) 13-based composites by Ce–Co grain boundary diffusion
CN108735411B (en) Lanthanum-iron-silicon/gadolinium composite magnetic refrigeration material and preparation process thereof
JPH02288305A (en) Rare earth magnet and manufacture thereof
CN108242302A (en) A kind of LaFeSi bases magnetic refrigeration composite block material based on grain boundary decision technology and preparation method thereof
CN106967923A (en) A kind of compound magnetic refrigerating material and its production and use
CN110534276A (en) A kind of La-Fe-Si base magnetic refrigeration composite material and preparation method thereof based on hot pressure reaction sintering
CN109454225A (en) A kind of basal cell La-Fe-Si temperature magnetic refrigerating composite material and preparation method
CN101734722A (en) Anti-perovskite solid material with near-zero thermal expansion characteristic
CN111161949B (en) YCe co-doped nanocrystalline rare earth permanent magnet and preparation method thereof
Lijuan et al. Influence of partial substitution of cerium for lanthanum on magnetocaloric properties of La1–xCexFe11. 44Si1. 56 and their hydrides
CN115938771B (en) SmFe (zinc oxide) x M 12-x Preparation method of nanocrystalline permanent magnet material
CN102373354A (en) Room temperature magnetic cooling material
Zhong et al. Superior comprehensive properties of LaFe11. 8Si1. 2/Ce60Co40 magnetocaloric composites
CN114156031A (en) Neodymium-iron-boron magnet and preparation method thereof
CN101994055A (en) Composite magnetostrictive material and preparation method thereof
CN106373691B (en) A kind of bonding La (Fe, Si) that heat conductivility is excellent13Block shaped magnet and preparation method thereof
CN109637768A (en) A kind of rare earth permanent-magnetic material and preparation method thereof containing yttrium

Legal Events

Date Code Title Description
PB01 Publication
PB01 Publication
SE01 Entry into force of request for substantive examination
SE01 Entry into force of request for substantive examination
RJ01 Rejection of invention patent application after publication
RJ01 Rejection of invention patent application after publication

Application publication date: 20170908