Method of manufacturing amorphous alloy magnetic core

US10283265B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10283265-B2
Application numberUS-201515513990-A
CountryUS
Kind codeB2
Filing dateSep 24, 2015
Priority dateSep 26, 2014
Publication dateMay 7, 2019
Grant dateMay 7, 2019

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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Abstract

Official abstract text for this publication.

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.

First claim

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.

Assignees

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Classifications

  • made from strips or ribbons · CPC title

  • from amorphous ribbons · CPC title

  • made from strips or ribbons (H01F27/26 takes precedence) · CPC title

  • Amorphous metallic alloys, e.g. glassy metals {(making ferrous amorphous alloys C22C33/003)} · CPC title

  • Magnetic cores · CPC title

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What does patent US10283265B2 cover?
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 …
Who is the assignee on this patent?
Hitachi Metals Ltd
What technology area does this patent fall under?
Primary CPC classification H01F41/0226. Mapped technology areas include Electricity.
When was this patent published?
Publication date Tue May 07 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).