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Publishing Language: Chinese | Open Access

Experimental design for the effect of ablation on the opening process of soft insulator in pulse motor

Yunlong BIAN1,2,3Haiyang LI1,3( )Zhibin SHEN1,3Hongbing ZHU2Zhiqiang WANG2
College of Aerospace Science and Engineering, National University of Defense Technology, Changsha 410073, China
The 41st Institute of the Sixth Academy of CASIC, Huhhot 010010, China
Hunan Key Laboratory of Intelligent Planning and Simulation for Aerospace Missions, Changsha 410073, China
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Abstract

Aiming at the problem that the soft insulator of pulse motor can not accurately describe its state and regular in the actual working process, a soft insulator opening test system was designed, which approximately simulated the working process of the soft insulator in the pulse motor. The opening characteristics of the ablative and non ablative soft insulator were compared, and the deformation law of the ablative and non ablative interlayer from the mechanism was explained by the means of scanning electron microscope. The test results show that the ablation rate calculated by the ablation simulation test is approximately equivalent to the insulator of a test pulse motor, and the relative error can be controlled within 5%; the deformation of the non ablated insulator is “valley pile” and the deformation of the ablated insulator is “bulb”. The established soft insulator layer opening test system can provide a feasible technical approach and means for the design and test verification of the soft insulator of pulse motor.

CLC number: V438 Document code: A Article ID: 1001-2486(2024)06-025-08

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Journal of National University of Defense Technology
Pages 25-32

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Cite this article:
BIAN Y, LI H, SHEN Z, et al. Experimental design for the effect of ablation on the opening process of soft insulator in pulse motor. Journal of National University of Defense Technology, 2024, 46(6): 25-32. https://doi.org/10.11887/j.cn.202406003

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Received: 29 June 2022
Published: 28 December 2024
© 2024 Journal of National University of Defense Technology

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