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Open Access

Ultrasonic signal separation and ice thickness identification methods in dynamic icing process

Yanxin ZHANGHongjian ZHANGXian YI( )Xingshi GUZhanwei HUJianjun XIONG
State Key Laboratory of Aerodynamics, China Aerodynamics Research and Development Center, Mianyang 621000, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

Ultrasonic pulse-echo icing detectors currently lack sensitivity to the early stages of icing, failing to effectively identify the thickness of thin ice layers and issue timely ice formation warnings during flight. The thin ice layers at the initial stage of icing can result in the overlap and mixing of ultrasonic signals, posing a significant challenge for ice thickness identification. This paper initially simulates ultrasonic pulse-echo signals for ice layers of varying thicknesses using the finite element method. Subsequently, the blind source separation algorithm, FastICA, is utilized to separate the ultrasonic mixture signals at the early stages of icing, with a comparison of the signal separation effects of nonlinear functions G1, G2, and G3. The results indicate that the G2 nonlinear function exhibits poor stability in signal separation, leading to signal distortion during the process, thus favoring the use of G1 type and G3 type nonlinear functions. This paper further analyzes the intrinsic causes of the periodic fluctuations in the phase difference/time of flight curve through signal distribution and correlation features, and validates the feasibility of the algorithm through dynamic icing experiments, achieving effective identification of thin ice layer thickness during the initial stages of icing.

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Chinese Journal of Aeronautics

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Cite this article:
ZHANG Y, ZHANG H, YI X, et al. Ultrasonic signal separation and ice thickness identification methods in dynamic icing process. Chinese Journal of Aeronautics, 2026, 39(3). https://doi.org/10.1016/j.cja.2025.103670

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Received: 23 December 2024
Revised: 06 January 2025
Accepted: 19 January 2025
Published: 10 July 2025
© 2025 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/).