The present invention includes composition and methods for the fabrication of very-high-aspect-ratio structures from metallic glasses. The present invention provides a method for nondestructive demolding of templates after thermoplastic molding of metallic glass features.

The present invention includes composition and methods for the fabrication of very-high-aspect-ratio structures from metallic glasses. The present invention provides a method for nondestructive demolding of templates after thermoplastic molding of metallic glass features.

A magnetic powder is represented by general formula Fe.sub.a(Si.sub.bB.sub.cP.sub.d).sub.100-a, and is produced with a gas atomization method. When the value of a and the value of b in the general formula is represented (a, b), (a, b) is within a predetermined region V1. Similarly, (a, c) and (a, d) are within a predetermined region, respectively. Whereby, it is possible to obtain an alloy magnetic powder which has high saturation magnetic flux density, low magnetic loss, and is spherical and easy to handle; and a magnetic core, a variety of coil components, and a motor can be realized by using the magnetic material.

A magnetic powder is represented by general formula Fe.sub.aSi.sub.bB.sub.cP.sub.dCu.sub.e. 71.0≦a≦81.0, 0.14≦b/c≦5, 0≦d≦14, 0<e≦1.4, d≦0.8a−50, e<−0.1(a+d)+10, and a+b+c+d+e=100. A crystallinity is not more than 30% in the case of containing an amorphous phase and a compound phase, and is not more than 60% in the case of not containing a compound phase. The magnetic powder is produced with a gas atomization method. Whereby, it is possible to obtain an alloy magnetic material which has high saturation magnetic flux density and low magnetic loss; and a magnetic core, coil components, and a motor can be realized.

A soft magnetic alloy having high saturation magnetic flux density Bs and low coercivity Hc, and a composition having formula (Fe(1−(α+β))X1αX2β)(1−(a+b+c))MaCbX3c; X1 represents one selected from the group of Co and Ni; X2 represents one selected from the group of Al, Mn, Ag, Zn, Sn, As, Sb, Cu, Cr, Bi, N, O, S, and rare earth elements; M represents one selected from the group of Ta, V, Zr, Hf, Ti, Nb, Mo, and W; X3 represents one selected from the group of P, B, Si, and Ge; and 0≤a≤0.140, 0.005≤b≤0.200, 0<c≤0.180, 0≤d≤0.020, 0.300≤b/(b+c)<1.000, 0≤α(1−(a+b+c))≤0.400, β≥0,0≤α+β≤0.50 are satisfied.

An amorphous lamination core for motor is configured by laminating amorphous alloy pieces, a pressurization member is pressed to a plurality of positions of the amorphous alloy piece, the number of pressurization portions with a crack is N, the total number of pressurization portions to which the pressurization member is pressed is N0 (N0≥100), and a degree of embrittlement is N/N0×100(%), the pressurization member is made of beryllium copper, and has a body portion of φ1.4 mm and a conical portion, the conical portion has a bottom surface of φ4 mm and a vertex angle θ of 120°, and when the degree of embrittlement is evaluated with the conical portion being pressed against the amorphous alloy piece and pressurization force of the pressurization member being set to 14 N, a degree of embrittlement of the amorphous alloy piece is equal to or less than 3.0%.

A soft magnetic powder has a composition represented by Fe.sub.100-a-b-c-d-e-f-g-hCu.sub.aSi.sub.bB.sub.cM.sub.dM′.sub.eX.sub.fAl.sub.gTi.sub.h (at %) (wherein M is at least one element selected from the group consisting of Nb and the like, M′ is at least one element selected from the group consisting of V and the like, X is at least one element selected from the group consisting of C and the like, and a, b, c, d, e, f, g, and h satisfy the following formulae: 0.1≤a≤3, 0<b≤30, 0<c≤25, 5≤b+c≤30, 0.1≤d≤30, 0≤e≤10, 0≤f≤10, 0.002≤g≤0.032, and 0≤h≤0.038), wherein a crystalline structure having a particle diameter of 1 to 30 nm is contained in an amount of 40 vol % or more.

A soft magnetic powder has a composition represented by Fe.sub.100-a-b-c-d-e-f-g-hCu.sub.aSi.sub.bB.sub.cM.sub.dM′.sub.eX.sub.fAl.sub.gTi.sub.h (at %) (wherein M is at least one element selected from the group consisting of Nb and the like, M′ is at least one element selected from the group consisting of V and the like, X is at least one element selected from the group consisting of C and the like, and a, b, c, d, e, f, g, and h satisfy the following formulae: 0.1≤a≤3, 0<b≤30, 0<c≤25, 5≤b+c≤30, 0.1≤d≤30, 0≤e≤10, 0≤f≤10, 0.002≤g≤0.032, and 0≤h≤0.038), wherein a crystalline structure having a particle diameter of 1 to 30 nm is contained in an amount of 40 vol % or more.

Methods and alloy systems for non-Be BMG matrix composite materials that can be used to additively manufacturing parts with superior mechanical properties, especially high toughness and strength, are provided. Alloys are directed to BMGMC materials comprising a high strength BMG matrix reinforced with properly scaled, soft, crystalline metal dendrite inclusions dispersed throughout the matrix in a sufficient concentration to resist fracture.

Methods and alloy systems for non-Be BMG matrix composite materials that can be used to additively manufacturing parts with superior mechanical properties, especially high toughness and strength, are provided. Alloys are directed to BMGMC materials comprising a high strength BMG matrix reinforced with properly scaled, soft, crystalline metal dendrite inclusions dispersed throughout the matrix in a sufficient concentration to resist fracture.