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基于叠片换能器的固体火箭推进剂超声检测技术研究
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中北大学极限环境光电动态测试与技术全国重点实验室

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国家自然科学基金(62401525)


Ultrasonic Detection Technology for Solid Rocket Propellant with Laminated Transducers
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State Key Laboratory of Extreme Environment Optoelectronic Dynamic Measurement Technology and Instrument, North University of China

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    摘要:

    为了解决超声波在固体推进剂中传播时存在衰减大、散射强,现有超声换能器无法检测出其内部全部缺陷的问题,提出了一种超声叠片换能器的无损检测研究方法。本研究方法,在国内外学者研究的基础上,提出利用叠片换能器具有较高的发射能量的特性来解决超声波在固体火箭推进剂中传播时存在的衰减和散射问题,设计了一种1 MHz四叠片的超声换能器,该换能器通过晶片堆叠将平面声场转化为柱面声场,以获取更丰富的回波信息,提高缺陷的分辨力;并在超声叠片换能器声场仿真的基础上,研制了1 MHz四叠片超声换能器,通过实验与同规格国内外换能器对比,增益提高了20 dB。最后搭建了固体火箭推进剂超声自动检测系统,实现了固体火箭推进剂的在线检测。结果表明,所研制的检测设备能够准确检测出Φ1.2 mm×5 mm(深)的最小人工盲孔及自然夹杂缺陷,完成了对固体火箭推进剂内、外部缺陷的定性定量无损检测。

    Abstract:

    To address the issue of significant attenuation and strong scattering of ultrasonic waves in solid propellants, which prevents existing ultrasonic transducers from detecting all internal defects, a nondestructive testing research method using ultrasonic laminated transducers is proposed. Based on the research of domestic and international scholars, this study first proposes leveraging the high transmission energy characteristic of laminated transducers to mitigate attenuation and scattering problems during ultrasonic propagation in solid rocket propellants. A 1 MHz four-layer ultrasonic transducer is designed. This transducer converts a planar acoustic field into a cylindrical acoustic field through crystal stacking, thereby enriching echo information and improving defect resolution. Based on acoustic field simulations of the ultrasonic laminated transducer, a 1 MHz four-layer ultrasonic transducer is developed. Experimental comparisons with domestic and international transducers of similar specifications show a 20 dB improvement in gain. Finally, an ultrasonic automated inspection system for solid rocket propellants is established, enabling online inspection of solid rocket propellants. The results indicate that the developed inspection equipment can accurately detect the smallest artificial blind holes measuring Φ1.2 mm × 5 mm (depth) as well as natural inclusion defects, achieving qualitative and quantitative nondestructive testing of all internal defects in solid rocket propellants.

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引用本文

杨顺民. 基于叠片换能器的固体火箭推进剂超声检测技术研究[J]. 含能材料,DOI:10.11943/CJEM2025257.

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  • 收稿日期: 2025-12-04
  • 最后修改日期: 2026-03-25
  • 录用日期: 2026-04-07
  • 在线发布日期: 2026-04-08
  • 出版日期: