Patent Application
20110233455
The present invention relates to a sintered Nd—Fe—B permanent magnet with high coercivity for high temperature applications.
Nd—Fe—B magnets have been recently developed as the leading RE permanent magnets with the highest room temperature magnetic properties beneficial for the wide use. The experimental value of the energy product of sintered Nd—Fe—B reached 59.5MGOe about 93% of the theoretic value and the remanence reached about 96% of the theoretic value in 2006, which was attained through the conventional single-alloy powder metallurgy method. Total weight of the 2007 production of Nd—Fe—B sintered magnets probably reached 58000 metric tones.
However, Nd—Fe—B permanent magnet materials have extremely poorer thermal stability than conventional Sm—Co permanent magnets. The coercivity of the magnet with highest energy product is as low as 8.2 kOe. Thus, they have suffered from the problems that they cannot be assembled in automobiles or precious devices appliances, and that they cannot be used in high temperature environments.
In order to make Nd—Fe—B sintered magnets more useful in a wider variety of applications at high temperature, the higher coercivity is essential. Because of the consequence of this, deficiency is reflected in the temperature coefficient of Br (remnant magnetism) and Hci (intrinsic coercivity), especially in the latter.
To address these problems, numerous researches have been carried out to improve their operating temperature. The elements addition is an effective approach, two types of substituent elements (S1, S2), which replace the rare-earth element (S1=Dy, Tb) or the transition element sites (S2=Co, Ni, Cr) in the hard magnetic phase, and two types of dopant elements (M1, M2) are distinguished. Substituent elements mainly change the intrinsic properties, such as spontaneous magnetic polarization, Curie temperature, and magnetocrystalline anisotropy. Both types of dopant elements influence the microstructure in a different way. M1 (Al, Cu, Zn, Ga, Ge, Sn) form binary M1-Nd or ternary M1-Fe—Nd phases, M2 (Ti, Zr, V, Mo, Nb, W) form binary M2-B or ternary M2-Fe—B phases.
Those efforts can affect the properties by changing the intrinsic behaviour of the matrix phase or improving the microstructure or both. In many instances, some properties of the sintered characteristics of the ternary Nd—Fe—B system are commonly improved but by sacrificing other properties. The reason is that one or several of the intrinsic magnetic properties of the matrix phase are impaired when these elements are dissolved in the matrix phase.
Based on the argumentation, it is necessary to find a method (or alloy) for improving the thermal stability (Tc and Hci;) without impairing the magnetic performance (Br (remnant magnetism)and (BH)max(magnetic energy production)).
The main object of the present invention is to provide an anisotropic sintered Nd—Fe—B permanent magnet having improved intrinsic coercivity suitable for high temperature applications by varying the chemical composition and optimizing the microstructure of magnets.
Another object of the invention is to develop a method of manufacturing a magnet which improves not only the thermal stability (Hci and Tc) of the Nd—Fe—B magnet but also the Br and (BH)max. The magnet is produced by two-alloy method (binary powder blending technique), wherein the powders of intergranular-phase thereof are modified by nano-powders to obtain preferred intergranular morphologies and make the microstructures of magnets as refined as possible, so as to be distinguished from conventional two alloy method.
A remarkable improvement in coercivity is observed in modified magnet showing a peak value at 10 wt % intergranular-phase alloy addition. There is a slight increase in density at small amount of 5˜10 wt % nano-powders modified intergranular-phase alloy (
The intergranular-phase alloy powders used in this invention are modified by very small addition of nano-powders with average particle size of 1˜60 nm which are selected from the group consisting of NiAl, TiC, SiC, AlN, TiN, ZrN and their combination thereof. These nano-powders afford a variety of excellent characteristic performances such as high melting point, low-density, low thermal conductivity and antioxidation properties.
The main processing methods of the present invention include alloy melting, strip casting, mechanically ball milling, hydrogen decrepitation, jet milling. The homogenous mixture of the required powders obtained is subsequently aligned in a magnetic field, then compressed under pressure, followed by sintering and tempering, to obtain final product of the magnets. The magnetic properties of the magnets are measured by AMT-4 magnetic measurement. The microstructures and components of the sintered magnets were analyzed by scanning electron microscope (SEM) equipped with energy dispersive X-ray detector (EDX).
The results showed that the sintered permanent magnet of the present invention has high coercivity Hci of about 30KOe or more, which is illustrated in the figures. There is an evident increase in density of the magnetic after being modified by adding nano-powder additive. Further micro-analysis shows that there is fine and uniform Nd2Fe14B main phase grains which is substantially spherical existing in these magnets modified by nano-powder additive, with an average size of approximately 5˜6 μm which is much smaller than that of the conventional unmodified magnet with an average size of approximately 8˜9 μm. Modified magnet has small, regular shaped grain boundaries, and most grains of its master-phase isolate from each other for they are covered by a layer of even Nd-rich film with a thickness of around 2 nm, wherein the thin layer weakens the exchange couple demagnetization effect between grains. Further analysis shows that the nano-powder additives or high-melting particles become pinning points in the border region of the 2-14-1 phase and hinder the abnormal grain growth. This kind of microstructures could contribute to the improvement of the intrinsic coercivity of the magnet.
Other and further advantages, features and benefits of the magnet of the present invention are illustrated in the following drawings and exemplary embodiments.
1) The master-phase and intergranular-phase alloys were prepared respectively. Strip flakes are prepared by the strip casting technique. The melted master-phase alloy is ejected onto a spinning copper wheel with speed 1.2 m/s, the composition is, by atomic percent, Nd13.12Fe80.69B5.73(Dy0.22Al0.24). The melted intergranular-phase alloy is ejected onto a spinning copper wheel with speed 18 m/s, the composition is, by atomic percent, Nd17.2Fe75.58B6.38Dy0.64Ga0.2.
2) The master-phase and intergranular-phase powders were prepared respectively. The powers were prepared by using jaw-crusher as coarse crushing and followed medium crushing by using medium-crusher. Subsequently, the master-phase alloy was made into powders with average particle diameter 3.0 μm and the intergranular-phase with average particle diameter 1.0 μm by jet milling in nitrogen condition.
3) Mixed the intergranular-phase powders and 0.01 wt % NiAl powders with average particle size of 60 nm well-proportioned with 3 wt % monohexadecyl ether as antioxidant and 2 wt % oleic acid as lubricant in a mixer.
4) The mixture powders were prepared by mixing the master-phase alloy powders with 2˜15 wt % intergranular-phase alloy powders modified by NiAl nano-powder and 1 wt % gasoline in blender mixer. Synchronously, the mixture powers were prepared by mixing the master-phase alloy powers with 5˜10 wt % unmodified intergranular-phase alloy powders and 1 wt % gasoline in blender mixer.
5) The mixture powers were compacted and aligned in a magnetic field of 1.2 T. The green compacts were pressed in a completely sealed glove box to insulate magnetic powers from air.
6) The green compacts were sintered in a high vacuum sintering furnace of 10−4 pa at temperature 1050° C. for 3 h and then annealed at temperature 890° C. for 3 h then 500° C. for 3 h followed by rapidly cooling rate of 200° C./min to room temperature. Finally, the finished sintered magnets were obtained.
Density was measured by Archimedes' method. The magnetic properties of the magnets were measured by AMT-4 measurement as shown in
1) The master-phase and intergranular-phase alloys were prepared respectively. Strip flakes were prepared by the strip casting technique. The melted master-phase alloy was ejected onto a spinning copper wheel with speed 2.0 m/s, the composition was, by atomic percent, Nd14.2Fe77.15B5.82(Tb0.31Al0.24Co2Nb0.28). The melted intergranular-phase alloy was ejected onto a spinning copper wheel with speed 18 m/s, the composition was, by atomic percent, Nd16.7Fe75.27B6.31(Dy1.2Ga0.2Al0.32).
2) The master-phase and intergranular-phase powders were prepared respectively. The powders were prepared by HDDR process during which the alloy was hydrogenised to saturation at room temperature and then dehydrogenated into powers at 500° C. for 8 h. Subsequently, the master-phase alloy was made into powders with average particle diameter 4 μm and the intergranular-phase with average particle diameter 2 μm by jet milling in nitrogen condition.
3) Mixed the intergranular-phase powders and 1 wt % TiC, SiC or AlN powders with average particle size of 1 nm well-proportioned with 4 wt % poly-oxacyclopropane fatty acid ester as antioxidant and 3 wt % polyethylene glycol as lubricant in a mixer.
4) The mixture powders were prepared by mixing the master-phase alloy powers with 2˜15 wt % intergranular-phase alloy powers modified by TiC, SiC or AlN nano-powders and 1.2 wt % gasoline in blender mixer.
5) The mixture powders were compacted and aligned in a magnetic field of 1.4 T. The green compacts were pressed in a completely sealed glove box to insulate magnetic powers from air.
6) The green compacts were sintered in a high vacuum sintering furnace of 10−4 pa at temperature 1065° C. for 3 h and then annealed at temperature 960° C. for 2 h then 530° C. for 2.5 h followed by rapidly cooling rate of 300° C./min to room temperature. Finally, the finished magnets were obtained.
The magnetic properties of the magnets were measured by AMT-4 measurement as shown in
1) The master-phase and intergranular-phase alloys were prepared respectively. Strip flakes were prepared by the strip casting technique. The melted master-phase alloy was ejected onto a spinning copper wheel with speed 2.2 m/s, the composition was, by atomic percent, Nd11.56Fe81.55B5.9Dy0.99. The melted intergranular-phase alloy was ejected onto a spinning copper wheel with speed 18 m/s, the composition was, by atomic percent, Nd27.83Fe56.2B6.68Dy2.47Co6.82.
2) The master-phase and intergranular-phase powders were prepared respectively. The powders were prepared by using jaw-crusher as coarse crushing and followed medium crushing by using medium-crusher. Subsequently, the master-phase alloy was made into powers with average particle diameter 5 μm and the intergranular-phase with average particle diameter 3 μm by jet milling in nitrogen condition.
3) Mixed the intergranular-phase powders and 0.2 wt % TiN or ZrN powders with average particle size of 40 nm well-proportioned with 4 wt % monohexadecyl ether as antioxidant and 4 wt % dehydrate sorbitan as lubricant in a mixer.
4) The mixture powers were prepared by mixing the master-phase alloy powers with 2˜15 wt % intergranular-phase alloy powers modified TiN or ZrN nano-powders and 2 wt % gasoline in blender mixer.
5) The mixture powders were compacted and aligned in a magnetic field of 1.8 T. The green compacts were pressed in a completely sealed glove box to insulate magnetic powers from air.
6) The green compacts were sintered in a high vacuum sintering furnace of 10−4 pa at temperature 1085° C. for 4.5 h and then annealed at temperature 900° C. for 2 h then 560° C. for 4 h followed by rapidly cooling rate of 100° C./min to room temperature. Finally, the finished magnets were obtained.
The magnetic properties of the magnets were measured by AMT-4 measurement as shown in
1) The master-phase and intergranular-phase alloys were prepared respectively. Strip flakes were prepared by the strip casting technique. The melted master-phase alloy was ejected onto a spinning copper wheel with speed 1.5 m/s, the composition was, by atomic percent, Nd12.69Fe80.21B5.7Dy1.4. The melted intergranular-phase alloy was ejected onto a spinning copper wheel with speed 18 m/s, the composition was, by atomic percent, Nd23.74Fe64.78B6.88(Dy0.92Co1.27C0.35Nb0.4Al1.66).
2) The master-phase and intergranular-phase powders were prepared respectively. the powers were prepared by HDDR process during which the alloy was absorbed hydrogen to saturation at room temperature and then dehydrogenated into powers at 500° C. for 8 h. Subsequently, the master-phase alloy was made into powers with average particle diameter 6 μm and the intergranular-phase with average particle diameter 4 μm by jet milling in nitrogen condition.
3) Mixed the intergranular-phase powders and 0.05 wt % TiC or AlN powders with average particle size of 20 nm well-proportioned with 8 wt % poly-oxacyclopropane fatty acid ester as antioxidant and 3 wt % polyethylene glycol as lubricant in a mixer.
4) The mixture powers were prepared by mixing the master-phase alloy powers with 5˜10 wt % intergranular-phase alloy powers modified by TiC or AlN nano-powders and 3.4 wt % gasoline in blender mixer. Synchronously, the mixture powers were prepared by mixing the master-phase alloy powers with 5˜10 wt % unmodified intergranular-phase alloy powers and 3.4 wt % gasoline in blender mixer.
5) The mixture powders were compacted and aligned in a magnetic field of 1.6 T. The green compacts were pressed in a completely sealed glove box to insulate magnetic powers from air.
6) The green compacts were sintered in a high vacuum sintering furnace of 10−4 pa at temperature 1080° C. for 3 h and then annealed at temperature 1000° C. for 2 h then 650° C. for 3 h followed by rapidly cooling rate of 400° C./min to room temperature. Finally, the finished magnets were obtained.
The magnetic properties of the magnets were measured by AMT-4 measurement as shown in
| Filing Document | Filing Date | Country | Kind | 371c Date |
|---|---|---|---|---|
| PCT/CN2008/073270 | 12/1/2008 | WO | 00 | 6/1/2011 |
