Laminated core, rotary electric machine, pressurizing jig, and method for manufacturing laminated core

A laminated core with region-specific adhesive strengths addresses the issue of compressive stress-induced magnetic property deterioration by differentially bonding electromagnetic steel sheets, ensuring strong adhesion where magnetic flux is low and weak adhesion where it's high, thus improving machine performance.

WO2025216279A1 Publication Date: 2025-10-16NIPPON STEEL CORPORATION
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Patent Information

Application Number
PCT/JP2025/014310
Authority / Receiving Office
WO · WO
Patent Type
Applications
Current Assignee / Owner
Priority Date
2024-04-10
Filing Date
2025-04-10
Publication Date
2025-10-16

AI Technical Summary

Technical Problem

The challenge of maintaining the laminated structure of electromagnetic steel sheets in rotating electric machines while minimizing the deterioration of magnetic properties due to compressive stress from adhesive shrinkage, particularly as sheets become thinner.

Method used

A laminated core design with varying adhesive strengths in different regions based on magnetic flux distribution, where regions with less magnetic flux have stronger adhesion and regions with more flux have weaker adhesion, using a pressing jig to apply differential pressure during bonding.

Benefits of technology

Ensures necessary fixing force while reducing the adverse impact on magnetic properties, thereby enhancing the performance of rotating electric machines by minimizing iron loss and other magnetic property degradations.

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Abstract

This laminated core (1) comprises a plurality of laminated electromagnetic steel sheets (10), and an adhesion part (41) that is provided between the electromagnetic steel sheets (10) adjacent to each other in the lamination direction and bonds the electromagnetic steel sheets (10) to each other. The adhesion part (41) has a first adhesion section (41A) provided in a first region (11) of the electromagnetic steel sheet (10), and a second adhesion section (41B) provided in a second region (12) different from the first region (11). The compression stress remaining in the first region (11) provided with the first adhesion section (41A) is greater than the compression stress remaining in the second region (12) provided with the second adhesion section (41B).
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