Coating formulation and application of organic passivation layer onto iron-based rare earth powders
View Patent ↗The present disclosure relates to coating formulations for neodymium-iron-boron type magnetic powders manufactured from rapid solidification processes for the purpose, inter alia, of corrosion and oxidation resistance when exposed to aggressive environments. The coating formulation preferably contains an epoxy binder, curing agent, an accelerating agent, and a lubricant. By incorporating coupling agents and optionally, other specialty additives with the magnetic powder and the organic epoxy components, additional oxidation and corrosion prevention, enhanced adhesion and dispersion between the filler and matrix phases can be achieved. This disclosure relates to all such rare earth-transition metal-boron (RE-TM-B) powders produced by rapid solidification and encompasses both the bonded magnet products that include combinations of the materials mentioned and the application processes.
1. A rapidly solidified rare earth-transition metal-boron magnet material, comprising a coated rare earth-transition metal-boron magnet powder comprising the magnet powder and a coating formulation, wherein the coating formulation comprises a combination, in an amount by weight of the magnet powder, of about 0.1 weight percent to about 1 weight percent of an organotitanate or organozirconate coupling agent, about 0.18 weight percent to about 4.46 weight percent of an epoxy resin, about 0.01 weight percent to about 0.27 weight percent of an amine-based hardener, about 0.004 weight percent to about 0.09 weight percent of an accelerator, and about 0.003 weight percent to about 0.27 weight percent of a lubricant;
wherein the general form of the coupling agent is
(RO—) n (Ti or Zr)(—OR′Y) 4-n
where R is a neopentyl(diallyl), dioctyl, or (2,2-diallyloxymethyl)butyl group, Ti or Zr has a coordination number of 4, R′ is a phosphito, pyrophosphato or cyclic pyrophosphato segment, and Y is a dioctyl or ditridecyl end group with 1≦n≦4.
2. The rapidly solidified rare earth-transition metal-boron magnet material of claim 1 , wherein said coating formulation comprises about 0.1 weight percent to about 1 weight percent of the organotitanate or organozirconate coupling agent, about 0.43 weight percent to about 3 weight percent of the epoxy resin, about 0.025 weight percent to about 0.18 weight percent of the amine-based hardener, about 0.009 weight percent to about 0.06 weight percent of the accelerator, and about 0.009 weight percent to about 0.19 weight percent of the lubricant.
3. A rapidly solidified rare earth-transition metal-boron magnet material comprising a coated rare earth-transition metal-boron magnet powder comprising the magnet powder and a coating formulation, wherein the coating formulation comprises a combination, in an amount by weight of the magnet powder, of about 0.225 weight percent to about 4.25 weight percent of epichlorohydrin/cresol novolac epoxy resin, about 0.01 weight percent to about 0.26 weight percent of dicyandiamide hardener, about 0.005 weight percent to about 0.085 weight percent of an aromatic, tertiary amine accelerator, about 0.004 weight percent to about 0.27 weight percent of zinc stearate lubricant, and about 0.35 weight percent to about 0.75 weight percent of an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group.
4. The rapidly solidified rare earth-transition metal-boron magnet material of claim 3 , wherein said coating formulation comprises about 0.68 weight percent to about 2.76 weight percent of epichlorohydrin/cresol novolac epoxy resin, about 0.04 weight percent to about 0.17 weight percent of dicyandiamide hardener, about 0.01 weight percent to about 0.055 weight percent of the aromatic, tertiary amine accelerator, about 0.01 weight percent to about 0.175 weight percent of the zinc stearate lubricant.
5. A rapidly solidified rare earth-transition metal-boron magnet material, comprising a coated rare earth-transition metal-boron magnet powder comprising the magnet powder and a coating formulation, wherein the coating formulation comprises a combination, in an amount by weight of the magnet powder, of about 0.65 weight percent to about 2.5 weight percent of an epoxy resin, about 0.035 weight percent to about 0.15 weight percent of an amine-based hardener, about 0.01 weight percent to about 0.05 weight percent of an accelerator, about 0.04 weight percent to about 0.16 weight percent of a lubricant, about 0.001 weight percent to about 0.3 weight percent of an organoclay, and about 0.35 weight percent to about 0.75 weight percent of an organotitanate or organozirconate coupling agent of the general form
(RO—) n (Ti or Zr)(—OR′Y) 4-n
where R is a neopentyl(diallyl), dioctyl, or (2,2-diallyoxymethyl)butyl group, Ti or Zr has a coordination number of 4, R′ is a phosphito, pyrophosphato or cyclic pyrophosphato segment, and Y is a dioctyl or ditridecyl end group with 1≦n≦4.
6. The rapidly solidified rare earth-transition metal-boron magnet material of claim 5 , wherein the coupling agent is an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group.
7. The rapidly solidified rare earth-transition metal-boron material of claim 5 , wherein:
the epoxy resin is epichlorohydrin/cresol novolac epoxy resin,
the amine-based hardener is dicyandiamide hardener,
the accelerator is an aromatic, tertiary amine accelerator,
the lubricant is zinc stearate; and
the organoclay comprises bis (hydroxyethyl) methyl tallow alkyl ammonium salts with bentonite.
8. The rapidly solidified rare earth-transition metal-boron magnet material of claim 5 , wherein said coating formulation comprises about 0.001 weight percent to about 0.3 weight percent of an organoclay comprising bis (hydroxyethyl) methyl tallow alkyl ammonium salts with bentonite; and about 0.35 weight percent to about 0.75 weight percent of an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group.
9. A rapidly solidified rare earth-transition metal-boron magnet material comprising a coated rare earth-transition metal-boron magnet powder, comprising a pre-coated magnet powder and a coating formulation,
wherein the pre-coated magnet powder comprises a combination of the magnet powder with a pre-coating of a POSS additive present in an amount by weight of the magnet powder of about 0.1 weight percent to about 5 weight percent; and
wherein the coating formulation comprises a combination, in an amount by total weight of the coating formulation, of about 0.54 weight percent to about 2.75 weight percent of an epoxy resin, about 0.03 weight percent to about 0.17 weight percent of an amine-based hardener, about 0.01 weight percent to about 0.06 weight percent of an accelerator, about 0.035 to about 0.175 weight percent of a lubricant, about 0.35 weight percent to about 0.75 weight percent of an organotitanate or organozirconate coupling agent of the general form
(RO—) n (Ti or Zr)(—OR′Y) 4-n
where R is a neopentyl(diallyl), dioctyl, or (2,2-diallyloxymethyl)butyl group, Ti or Zr has a coordination number of 4 or 5, R′ is a phosphito, pyrophosphato or cyclic pyrophosphato segment, and Y is a dioctyl or ditridecyl end group, with 1≦n≦4, about 0.003 weight percent to about 0.055 weight percent of an organoclay, and about 0.003 weight percent to about 0.015 weight percent of an antioxidant agent.
10. The rapidly solidified rare earth-transition metal-boron magnet material of claim 9 , wherein the coupling agent is an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group.
11. The rapidly solidified rare earth-transition metal-boron magnet material of claim 9 , wherein the POSS additive is trisilanolphenyl or epoxycyclohexyl POSS.
12. The rapidly solidified rare earth-transition metal-boron magnet material of claim 9 , wherein the antioxidant agent is a butylated reaction product of p-cresol and dicyclopentadiene antioxidant.
13. The rapidly solidified rare earth-transition metal-boron magnet material of claim 9 , wherein:
the epoxy resin is epichlorohydrin/cresol novolac epoxy resin,
the amine-based hardener is dicyandiamide hardener,
the accelerator is an aromatic, tertiary amine accelerator,
the lubricant is zinc stearate lubricant; and
the organo clay additive is bis (hydroxyethyl) methyl tallow alkyl ammonium salts with bentonite.
14. The rapidly solidified rare earth-transition metal-boron magnet material of claim 9 , wherein:
said pre-coating is a trisilanolphenyl or epoxycyclohexyl POSS in an amount of about 0.1 weight percent to about 1 weight percent, by weight of the magnet powder; and said coating formulation comprises, by total weight of the mixture, of about 0.54 weight percent to about 2.75 weight percent of epichlorohydrin/cresol novolac epoxy resin, about 0.03 weight percent to about 0.17 weight percent of dicyandiamide hardener, about 0.01 weight percent to about 0.06 weight percent of an aromatic, tertiary amine accelerator, about 0.035 weight percent to about 0.175 weight percent of zinc stearate lubricant,
about 0.35 weight percent to about 0.75 weight percent of an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group,
about 0.003 weight percent to about 0.07 weight percent of an organoclay comprising bis (hydroxyethyl) methyl tallow alkyl ammonium salts with bentonite, and
about 0.003 weight percent to about 0.015 weight percent of a butylated reaction product of p-cresol and dicyclopentadiene antioxidant.
15. A rapidly solidified rare earth-transition metal-boron magnet material, comprising a coated rare earth-transition metal-boron magnet powder comprising the magnet powder and a coating formulation, wherein the coating formulation comprises a combination consisting essentially of, in an amount by weight of the magnet powder, of about 0.1 weight percent to about 1 weight percent of an organotitanate or organozirconate coupling agent, about 0.18 weight percent to about 4.46 weight percent of an epoxy resin, about 0.01 weight percent to about 0.27 weight percent of an amine-based hardener, about 0.004 weight percent to about 0.09 weight percent of an accelerator, and about 0.003 weight percent to about 0.27 weight percent of a lubricant;
wherein the general form of the coupling agent is
(RO—) n (Ti or Zr)(—OR′Y) 4-n
where R is a neopentyl(diallyl), dioctyl, or (2,2-diallyloxymethyl)butyl group, Ti or Zr has a coordination number of 4, R′ is a phosphito, pyrophosphato or cyclic pyrophosphato segment, and Y is a dioctyl or ditridecyl end group, with 1≦n≦4.
16. The rapidly solidified rare earth-transition metal-boron magnet material of claim 15 , wherein said coating formulation consists essentially of about 0.1 weight percent to about 1 weight percent of the organotitanate or organozirconate coupling agent, about 0.43 weight percent to about 3 weight percent of the epoxy resin, about 0.025 weight percent to about 0.18 weight percent of the amine-based hardener, about 0.009 weight percent to about 0.06 weight percent of the accelerator, and about 0.009 weight percent to about 0.19 weight percent of the lubricant.
17. A rapidly solidified rare earth-transition metal-boron magnet material, comprising a coated rare earth-transition metal-boron magnet powder comprising the magnet powder and a coating formulation, wherein the coating formulation comprises a combination consisting essentially of, in an amount by weight of the magnet powder, of about 0.225 weight percent to about 4.25 weight percent of epichlorohydrin/cresol novolac epoxy resin, about 0.01 weight percent to about 0.26 weight percent of dicyandiamide hardener, about 0.005 weight percent to about 0.085 weight percent of an aromatic, tertiary amine accelerator, about 0.004 weight percent to about 0.27 weight percent of zinc stearate lubricant, and about 0.35 weight percent to about 0.75 weight percent of an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group.
18. The rapidly solidified rare earth-transition metal-boron magnet material of claim 17 , wherein said coating formulation consists essentially of about 0.68 weight percent to about 2.76 weight percent of epichlorohydrin/cresol novolac epoxy resin, about 0.04 weight percent to about 0.17 weight percent of dicyandiamide hardener, about 0.01 weight percent to about 0.055 weight percent of the aromatic, tertiary amine accelerator, about 0.01 weight percent to about 0.175 weight percent of the zinc stearate lubricant.
19. A rapidly solidified rare earth-transition metal-boron magnet material, comprising a coated rare earth-transition metal-boron magnet powder comprising the magnet powder and a coating formulation, wherein the coating formulation comprises a combination consisting essentially of, in an amount by weight of the magnet powder, of about 0.65 weight percent to about 2.5 weight percent of an epoxy resin, about 0.035 weight percent to about 0.15 weight percent of an amine-based hardener, about 0.01 weight percent to about 0.05 weight percent of an accelerator, about 0.04 weight percent to about 0.16 weight percent of a lubricant, about 0.001 weight percent to about 0.3 weight percent of an organoclay, and about 0.35 weight percent to about 0.75 weight percent of an organotitanate or organozirconate coupling agent of the general form
(RO—) n (Ti or Zr)(—OR′Y) 4-n
where R is a neopentyl(diallyl), dioctyl, or (2,2-diallyoxymethyl)butyl group, Ti or Zr has a coordination number of 4, R′ is a phosphito, pyrophosphato or cyclic pyrophosphato segment, and Y is a dioctyl or ditridecyl end group, with 1≦n≦4.
20. The rapidly solidified rare earth-transition metal-boron magnet material of claim 19 , wherein the coupling agent is an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group.
21. The rapidly solidified rare earth-transition metal-boron material of claim 19 , wherein:
the epoxy resin is epichlorohydrin/cresol novolac epoxy resin,
the amine-based hardener is dicyandiamide hardener,
the accelerator is an aromatic, tertiary amine accelerator,
the lubricant is zinc stearate; and
the organoclay comprises bis (hydroxyethyl) methyl tallow alkyl ammonium salts with bentonite.
22. The rapidly solidified rare earth-transition metal-boron magnet material of claim 19 , wherein said coating formulation consists essentially of about 0.001 weight percent to about 0.3 weight percent of an organoclay comprising bis (hydroxyethyl) methyl tallow alkyl ammonium salts with bentonite; and about 0.35 weight percent to about 0.75 weight percent of an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group.
23. A rapidly solidified rare earth-transition metal-boron magnet material comprising a coated rare earth-transition metal-boron magnet powder, comprising a pre-coated magnet powder and a coating formulation,
wherein the pre-coated magnet powder comprises a combination of the magnet powder with a pre-coating of a POSS additive present in an amount by weight of the magnet powder of about 0.1 weight percent to about 5 weight percent; and
wherein the coating formulation consists essentially of, in an amount my total weight of the coating formulation, of about 0.54 weight percent to about 2.75 weight percent of an epoxy resin, about 0.03 weight percent to about 0.17 weight percent of an amine-based hardener, about 0.01 weight percent to about 0.06 weight percent of an accelerator, about 0.035 to about 0.175 weight percent of a lubricant, about 0.35 weight percent to about 0.75 weight percent of an organotitanate or organozirconate coupling agent of the general form
(RO—) n (Ti or Zr)(—OR′Y) 4-n
where R is a neopentyl(diallyl), dioctyl, or (2,2-diallyloxymethyl)butyl group, Ti or Zr has a coordination number of 4 or 5, R′ is a phosphito, pyrophosphato or cyclic pyrophosphato segment, and Y is a dioctyl or ditridecyl end group with 1≦n≦4, about 0.003 weight percent to about 0.055 weight percent of an organoclay, and about 0.003 weight percent to about 0.015 weight percent of an antioxidant agent.
24. The rapidly solidified rare earth-transition metal-boron magnet material of claim 23 , wherein the coupling agent is an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group.
25. The rapidly solidified rare earth-transition metal-boron magnet material of claim 23 , wherein the POSS additive is trisilanolphenyl or epoxycyclohexyl POSS.
26. The rapidly solidified rare earth-transition metal-boron magnet material of claim 23 , wherein the antioxidant agent is a butylated reaction product of p-cresol and dicyclopentadiene antioxidant.
27. The rapidly solidified rare earth-transition metal-boron magnet material of claim 23 , wherein:
the epoxy resin is epichlorohydrin/cresol novolac epoxy resin,
the amine-based hardener is dicyandiamide hardener,
the accelerator is an aromatic, tertiary amine accelerator,
the lubricant is zinc stearate lubricant; and
the organo clay additive is bis (hydroxyethyl) methyl tallow alkyl ammonium salts with bentonite.
28. The rapidly solidified rare earth-transition metal-boron magnet material of claim 23 , wherein:
said pre-coating is a trisilanolphenyl or epoxycyclohexyl POSS in an amount of about 0.1 weight percent to about 1 weight percent, by weight of the magnet powder; and said coating formulation consists essentially of, by total weight of the mixture, of about 0.54 weight percent to about 2.75 weight percent of epichlorohydrin/cresol novolac epoxy resin, about 0.03 weight percent to about 0.17 weight percent of dicyandiamide hardener, about 0.01 weight percent to about 0.06 weight percent of an aromatic, tertiary amine accelerator, about 0.035 weight percent to about 0.175 weight percent of zinc stearate lubricant,
about 0.35 weight percent to about 0.75 weight percent of an organotitanate coupling agent of the form
(RO—)Ti(—OR′Y) 3
where R is a neopentyl(diallyl), Ti has a coordination number of 4, R′ is a pyrophosphato segment, and Y is a dioctyl end group,
about 0.003 weight percent to about 0.07 weight percent of an organoclay comprising bis (hydroxyethyl) methyl tallow alkyl ammonium salts with bentonite, and
about 0.003 weight percent to about 0.015 weight percent of a butylated reaction product of p-cresol and dicyclopentadiene antioxidant.