R-T-B-BASED SINTERED MAGNET AND PREPARATION METHOD THEREFOR

1 . An R-T-B-based sintered magnet, wherein the R-T-B-based sintered magnet comprises R, B, Ti, Ga, Al, Cu and T by the following percentage:

29.0-33% of R;

0.86-0.93% of B;

0.05-0.25% of Ti;

0.3-0.5% of Ga, exclusive of 0.5%;

0.6-1% of Al, exclusive of 0.6%;

0.36-0.55% of Cu;

wherein, R is rare earth element comprising at least Nd, B is boron, Ti is titanium, Ga is gallium, Al is aluminum, Cu is copper, T comprises Fe and Co; the percentage is mass percentage.

2 . The R-T-B-based sintered magnet of claim 1 , wherein R is 30.2-33%;

or, RH in R is 0 or not more than 1%, such as 0% or 0.5%;

or, B is 0.915-0.93%, such as 0.915%, 0.92% or 0.93%;

or, Ti is 0.15-0.25%, such as 0.15%, 0.2% or 0.25%;

or, Ga is 0.3-0.455%, such as 0.3%, 0.4% or 0.455%;

or, Al is 0.65-1%, exclusive of 1%, such as 0.65%, 0.7%, 0.8% or 0.9%;

or, Cu is 0.45-0.55%, such as 0.45%, 0.5% or 0.55%;

or, Fe and Co are a balance of 100% mass percentage;

or, C, N and O of the R-T-B-based sintered magnet in total are 1000 ppm-3500 ppm;

the percentage is mass percentage.

3 . The R-T-B-based sintered magnet of claim 1 , wherein the R-T-B-based sintered magnet comprises a main phase and a grain boundary phase; wherein the main phase comprises R 2 T 14 B, the grain boundary phase comprises R x —(Cu a —Ga b —Al c ) y and rare earth oxide phase;

wherein, x/y=1.5-3; a/b=2-5; (a+b)/c=30-70;

the main phase is 94-98%; the R x —(Cu a —Ga b —Al c ) y is 1-3.5%; the rare earth oxide phase is 1-2.5%, the percentage is volume percentage.

4 . The RTB-based sintered magnet of claim 1 , wherein the R-T-B-based sintered magnet comprises 31.5% of Nd, 0.92% of B, 0.5% of Co; 0.9% of Al, 0.45% of Cu, 0.455% of Ga, 0.2% of Ti, and Fe as a balance; the percentage is mass percentage;

or, the R-T-B-based sintered magnet comprises 31.5% of Nd, 0.92% of B, 0.5% of Co; 1.0% of Al, 0.5% of Cu, 0.455% of Ga, 0.2% of Ti, and Fe as a balance; the percentage is mass percentage;

or, the R-T-B-based sintered magnet comprises 31.5% of Nd, 0.5% of Dy; 0.915% of B, 0.5% of Co; 0.7% of Al, 0.55% of Cu, 0.455% of Ga, 0.25% of Ti, and Fe as a balance; the percentage is mass percentage;

or, the R-T-B-based sintered magnet comprises 30.2% of Nd, 0.93% of B, 1.5% of Co; 0.65% of Al, 0.4% of Cu, 0.3% of Ga, 0.15% of Ti, and Fe as a balance; the percentage is mass percentage;

or, the R-T-B-based sintered magnet comprises 33% of Nd, 0.86% of B, 3.0% of Co; 0.8% of Al, 0.36% of Cu, 0.4% of Ga, 0.05% of Ti, and Fe as a balance; the percentage is mass percentage.

5 . An R-T-B-based sintered magnet, wherein the R-T-B-based sintered magnet comprises a main phase and a grain boundary phase; the main phase comprises R 2 T 14 B, the grain boundary phase comprises R x —(Cu a —Ga b —Al c ) y and rare earth oxide phase;

wherein, x/y=1.5-3; a/b=2-5; (a+b)/c=30-70;

the main phase content is 94-98%; the R x —(Cu a —Ga b —Al c ) y is 1-3.5%; the rare earth oxide phase is 1-2.5%, the percentage is volume percentage.

6 . The R-T-B-based sintered magnet of claim 5 , in the grain boundary R x —(Cu a —Ga b —Al c ) y , x/y=1.5-3, a:b:c=(10-40):(6-19): 1 .

7 . A method for preparing the R-T-B-based sintered magnet of claim 1 , wherein the method involves smelting, casting, hydrogen decrepitating, jet milling, forming, sintering and aging a raw material of the R-T-B-based sintered magnet successively.

8 . The method of claim 7 , wherein the smelting is carried out in a high frequency induction vacuum melting furnace;

or, the smelting has a temperature of 1450-1550° C.;

or, the casting is carried out under an Ar gas conditions;

or, the casting is carried out at a gas pressure of 20-70 kPa;

or, the casting has a copper roller wheel speed of 0.4-2 m/s, such as 1 m/s;

or, the casting produces an R-T-B alloy sheet having a thickness of 0.15-0.5 mm;

or, the hydrogen decrepitation has a hydrogen absorption temperature of 20-300° C.;

or, the hydrogen decrepitation has a hydrogen absorption pressure of 0.12-0.19 MPa;

or, the hydrogen decrepitation has a hydrogen desorption time of 0.5-5 h, such as 2 h;

or, the hydrogen decrepitation has a hydrogen desorption temperature of 450-600° C.;

or, the jet milling is to add the R-T-B alloy powder into jet milling machine for successively pulverizing by jet milling to obtain a fine powder;

or, the forming is carried out under a magnetic field strength above 1.8 T, and protection of nitrogen gas atmosphere;

or, the sintering comprises four steps: (1) a heat treatment at a temperature of 150-300° C. for 1-4 h; (2) a heat treatment at a temperature of 400-600° C. for 1-4 h; (3) a heat treatment at a temperature of 800-900° C. for 1-4 h; (4) a heat treatment at a temperature of 1000-1090° C. for more than 3 h;

the aging comprises a primary aging and a secondary aging.

9 . An R-T-B-based sintered magnet, which is prepared by the method of claim 7 .

10 . A use of the R-T-B-based sintered magnet of claim 1 , as a magnetic steel of motor rotor.

11 . The R-T-B-based sintered magnet of claim 2 , wherein Co is 0.5-3%; or Fe is 60-68%.

12 . The R-T-B-based sintered magnet of claim 3 , in the grain boundary, R x —(Cu a —Ga b —Al c ) y , x/y=1.5-3, a:b:c=(10-40):(6-19): 1 .

13 . The method of claim 8 , wherein the melting furnace has a vacuum degree of less than 0.1 Pa;

or, the smelting temperature of 1500-1550° C.;

or, the casting is carried out at a gas pressure of 30-50 kPa;

or, the R-T-B alloy sheet has a thickness of 0.2-0.35 mm;

or, the fine powder has a medium value particle size D 50 of 3-5.5 μm;

or, the jet milling has a pulverization pressure of 0.3-0.5 MPa;

or, the primary aging has a temperature of 850° C.-950° C.;

or, the secondary aging has a temperature of 440° C.-540° C.

14 . The method of claim 13 , wherein the melting furnace has a vacuum degree of less than 0.02 Pa.