Method for the manufacture of a nanocrystalline magnetic core
US-2016369364-A1 · Dec 22, 2016 · US
US10283265B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10283265-B2 |
| Application number | US-201515513990-A |
| Country | US |
| Kind code | B2 |
| Filing date | Sep 24, 2015 |
| Priority date | Sep 26, 2014 |
| Publication date | May 7, 2019 |
| Grant date | May 7, 2019 |
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A method of manufacturing an amorphous alloy magnetic core, which includes preparing a layered body by layering amorphous alloy thin strips one on another, and has one end face and another end face in a width direction of the thin strips and an inner peripheral surface and an outer peripheral surface orthogonal to a layering direction of the thin strips; forming a hole passing through from the one end face of the layered body as a starting point; subjecting the layered body to which the hole has been formed to a heat treatment while measuring an internal temperature of the hole; and forming a resin layer which blocks the hole and covers at least a part of the one end face by coating and curing a two-liquid mixed type epoxy resin composition having a viscosity of from 38 Pa·s to 51 Pa·s and a T. I. value of from 1.6 to 2.7 on at least a part of at least the one end face of the layered body after being subjected to the heat treatment.
Opening claim text (preview).
The invention claimed is: 1. A method of manufacturing an amorphous alloy magnetic core, the method comprising: a layered body preparing step of preparing a layered body by layering amorphous alloy thin strips one on another, the layered body having one end face and another end face in a width direction of the amorphous alloy thin strips and an inner peripheral surface and an outer peripheral surface orthogonal to a layering direction of the amorphous alloy thin strips; a hole forming step of forming a hole passing through from the one end face of the layered body as a starting point, the width direction corresponding to a depth direction of the hole; a heat treatment step of subjecting the layered body, after being subjected to the hole forming step, to a heat treatment while measuring an internal temperature of the hole; and a resin layer forming step of forming a resin layer which blocks the hole and covers at least a part of the one end face by coating and curing a two-liquid mixed type epoxy resin composition having a viscosity (25° C.) after mixing of two liquids measured under a condition of a rotation speed of 50 rpm of from 38 Pa·s to 51 Pa·s and a thixotropy index value (25° C.) after mixing of the two liquids determined by the following Formula (1) of from 1.6 to 2.7 on a region which is at least a part of at least the one end face of the layered body after being subjected to the heat treatment step and includes the hole: Thixotropy index value (25° C.) after mixing of two liquids=viscosity at 5 rpm/viscosity at 50 rpm Formula (1) wherein, in Formula (1), the term “viscosity at 50 rpm” refers to the viscosity (25° C.) after mixing of the two liquids of the two-liquid mixed type epoxy resin composition measured under the condition of a rotation speed of 50 rpm and the term “viscosity at 5 rpm” refers to the viscosity (25° C.) after mixing of the two liquids of the two-liquid mixed type epoxy resin composition measured under the condition of a rotation speed of 5 rpm. 2. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the heat treatment is conducted on the layered body, which is disposed in a magnetic field in the heat treatment step. 3. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the layered body after being subjected to the hole forming step but before being subjected to the resin layer forming step is configured such that a shortest distance between a center of the hole and a center line in a thickness direction of the layered body is 10% or less with respect to a thickness of the layered body, when viewed from a side of the one end face in the layered body. 4. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the layered body after being subjected to the hole forming step but before being subjected to the resin layer forming step is configured such that the entire hole is included in a range from one end to another end in a longitudinal direction of the inner peripheral surface on the one end face, when viewed from a side of the one end face in the layered body. 5. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the layered body after being subjected to the hole forming step but before being subjected to the resin layer forming step is configured such that a shortest distance between a center of the hole and a center line in a longitudinal direction of the layered body is 20% or less with respect to a length in the longitudinal direction of the layered body, when viewed from a side of the one end face in the layered body. 6. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the layered body after being subjected to the hole forming step but before being subjected to the resin layer forming step is configured such that a depth of the hole is from 30% to 70% with respect to a distance between the one end face and the another end face in the layered body. 7. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the layered body after being subjected to the hole forming step but before being subjected to the resin layer forming step is configured such that a width of the hole is 1.5 mm or more in the layered body. 8. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the layered body after being subjected to the hole forming step but before being subjected to the resin layer forming step is configured such that a width of the hole is narrower than a value to be calculated by a mathematical formula T×(100−LF)/100, wherein a thickness (mm) of the layered body is denoted as T and a space factor (%) of the amorphous alloy magnetic core is denoted as LF in the layered body. 9. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the layered body after being subjected to the hole forming step but before being subjected to the resin layer forming step is configured such that a width of the hole is 3.5 mm or less in the layered body. 10. The method of manufacturing an amorphous alloy magnetic core according to claim 1 , wherein the layered body after being subjected to the hole forming step but before being subjected to the resin layer forming step is configured such that a length of the hole is from 1.5 mm to 35 mm in the layered body.
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