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Article

A Flexible Ultra-Thin Ultrasonic Transducer for Ice Detection on Curved Surfaces

1
College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
2
State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
3
Liaoning Provincial Key Laboratory of Aircraft Ice Protection, AVIC Aerodynamics Research Institute, Shenyang 110034, China
*
Author to whom correspondence should be addressed.
Aerospace 2025, 12(11), 997; https://doi.org/10.3390/aerospace12110997
Submission received: 25 September 2025 / Revised: 28 October 2025 / Accepted: 6 November 2025 / Published: 7 November 2025
(This article belongs to the Special Issue Deicing and Anti-Icing of Aircraft (Volume IV))

Abstract

Icing phenomena occur on aircraft and unmanned aerial vehicles (UAVs) under extreme weather conditions. Ultrasonic detection technology is an effective method for measuring ice formation while maintaining the shape of the structure. However, current ultrasonic sensors, which are large and inflexible, are unsuitable for irregular UAV bodies, limiting their applications in real scenarios. For the detection of icing on curved structure, this study proposes a novel flexible ultra-thin ultrasonic transducer (FUTUT). The transducer exhibits excellent flexibility, making it suitable for use on high-curvature wings. Firstly, the FUTUT was designed based on the material properties of the airframe and the sensitivity requirements for ice detection, following the design guidelines for 1-3 type piezocomposites. The fabrication process for the FUTUT was then investigated, and its flexibility and low-temperature resistance were tested. Finally, icing detection experiments were conducted in an icing wind tunnel (IWT), where the FUTUT of 9.82 MHz demonstrated an ice-thickness-detection sensitivity of 0.29 mm. Experimental results indicate that the FUTUT possesses superior flexibility and exhibits excellent stability in low-temperature environments. These results underscore the FUTUT’s promise for applications in ice detection on curved structures.
Keywords: ice detection; flexible sensor; 1-3 piezocomposite; curved structure; ultrasonic detection ice detection; flexible sensor; 1-3 piezocomposite; curved structure; ultrasonic detection

Share and Cite

MDPI and ACS Style

Wang, Y.; Wang, Y.; Lu, Q.; Zhu, C.; Wu, D.; Zhu, C.; Wu, Y. A Flexible Ultra-Thin Ultrasonic Transducer for Ice Detection on Curved Surfaces. Aerospace 2025, 12, 997. https://doi.org/10.3390/aerospace12110997

AMA Style

Wang Y, Wang Y, Lu Q, Zhu C, Wu D, Zhu C, Wu Y. A Flexible Ultra-Thin Ultrasonic Transducer for Ice Detection on Curved Surfaces. Aerospace. 2025; 12(11):997. https://doi.org/10.3390/aerospace12110997

Chicago/Turabian Style

Wang, Yan, Yuan Wang, Qingwen Lu, Chengxiang Zhu, Dawei Wu, Chunling Zhu, and Yuan Wu. 2025. "A Flexible Ultra-Thin Ultrasonic Transducer for Ice Detection on Curved Surfaces" Aerospace 12, no. 11: 997. https://doi.org/10.3390/aerospace12110997

APA Style

Wang, Y., Wang, Y., Lu, Q., Zhu, C., Wu, D., Zhu, C., & Wu, Y. (2025). A Flexible Ultra-Thin Ultrasonic Transducer for Ice Detection on Curved Surfaces. Aerospace, 12(11), 997. https://doi.org/10.3390/aerospace12110997

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