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用于航空航天部件无损检测的主动红外热成像技术的最新进展

Recent Advances in Active Infrared Thermography for Non-Destructive Testing of Aerospace Components.

作者信息

Ciampa Francesco, Mahmoodi Pooya, Pinto Fulvio, Meo Michele

机构信息

Materials and Structures Centre (MAST), Department of Mechanical Engineering, University of Bath, Bath BA2 7AY, UK.

出版信息

Sensors (Basel). 2018 Feb 16;18(2):609. doi: 10.3390/s18020609.

Abstract

Active infrared thermography is a fast and accurate non-destructive evaluation technique that is of particular relevance to the aerospace industry for the inspection of aircraft and helicopters' primary and secondary structures, aero-engine parts, spacecraft components and its subsystems. This review provides an exhaustive summary of most recent active thermographic methods used for aerospace applications according to their physical principle and thermal excitation sources. Besides traditional optically stimulated thermography, which uses external optical radiation such as flashes, heaters and laser systems, novel hybrid thermographic techniques are also investigated. These include ultrasonic stimulated thermography, which uses ultrasonic waves and the local damage resonance effect to enhance the reliability and sensitivity to micro-cracks, eddy current stimulated thermography, which uses cost-effective eddy current excitation to generate induction heating, and microwave thermography, which uses electromagnetic radiation at the microwave frequency bands to provide rapid detection of cracks and delamination. All these techniques are here analysed and numerous examples are provided for different damage scenarios and aerospace components in order to identify the strength and limitations of each thermographic technique. Moreover, alternative strategies to current external thermal excitation sources, here named as material-based thermography methods, are examined in this paper. These novel thermographic techniques rely on thermoresistive internal heating and offer a fast, low power, accurate and reliable assessment of damage in aerospace composites.

摘要

主动红外热成像技术是一种快速且准确的无损评估技术,对航空航天工业检查飞机和直升机的主、次结构、航空发动机部件、航天器组件及其子系统尤为重要。本综述根据其物理原理和热激发源,对用于航空航天应用的最新主动热成像方法进行了详尽总结。除了使用诸如闪光灯、加热器和激光系统等外部光辐射的传统光激发热成像外,还研究了新型混合热成像技术。这些技术包括利用超声波和局部损伤共振效应来提高对微裂纹的可靠性和灵敏度的超声激发热成像、利用经济高效的涡流激发产生感应加热的涡流激发热成像,以及利用微波频段电磁辐射快速检测裂纹和分层的微波热成像。本文对所有这些技术进行了分析,并针对不同的损伤情况和航空航天部件提供了大量示例,以确定每种热成像技术的优势和局限性。此外,本文还研究了当前外部热激发源的替代策略,这里称为基于材料的热成像方法。这些新型热成像技术依靠热阻内部加热,能对航空航天复合材料中的损伤进行快速、低功耗、准确且可靠的评估。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/e16a/5856039/d5d5cbff9b8a/sensors-18-00609-g001a.jpg

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