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Full Length Article | Open Access

A multi-parameter model of heat treatment process for soft magnetic materials on performance of HSERs

Jiaxin YOUaHao YUaHuimin LIANGa( )Yong XIEbDing DINGa
Department of Electrical Engineering, Harbin Institute of Technology, Harbin 150000, China
G&A Electronics Co., Ltd, Guilin 541000, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Material properties play an important role in the performance of electromagnetic mechanism. For an aeronautic Hermetically-Sealed Electromagnetic Relay (HSER), more than 50% parts are made of soft magnetic materials. Therefore, the performance of soft magnetic materials directly determines the static and dynamic characteristics of the HSER. Based on the theory of crystal recrystallization, this paper analyzes cold extrusion and heat treatment in the processing of soft magnetic materials, simulates the grain change process of an armature at different heat treatment temperatures, establishes a correlation model of temperature, grain size, and magnetic energy, and verifies results by scanning electron microscopy. Results of heat treatment temperatures from 800 °C to 920 °C are obtained and compared. A sample soft magnetic material after heat treatment at different temperatures has the largest difference in the initial magnetization range, up to 22%. In order to verify the fluctuation of the overall output characteristics of an HSER caused by the difference between soft magnetic materials, a static and dynamic analysis model of a typical HSER is established, and the accuracy of the model is verified by a set of actual test system. The difference of dynamic characteristics under different heat treatment temperatures is nearly 3%.

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Chinese Journal of Aeronautics
Pages 379-388

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Cite this article:
YOU J, YU H, LIANG H, et al. A multi-parameter model of heat treatment process for soft magnetic materials on performance of HSERs. Chinese Journal of Aeronautics, 2022, 35(9): 379-388. https://doi.org/10.1016/j.cja.2022.03.002

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Received: 07 April 2021
Revised: 27 May 2021
Accepted: 07 July 2021
Published: 11 March 2022
© 2022 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).