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.

Highlights

  • 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’

  • Smaller defects could be detected without the need to increase the total feeding current, keeping the total energy consumption of the system to low levels

  • This paper presented an overview of active infrared thermography techniques recently used for the analysis

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Summary

Infrared Thermography for Aerospace Applications

Infrared thermography (IRT) is a rapid and accurate non-destructive evaluation (NDE) technique that is widely used for the inspection of large aerospace components such as aircraft and helicopters’. In Active IRT, temperature gradients responses at the medium mechanical ultrasonic waves and material enabled features in composites in order to generate heat in surface are recorded and analysed by an IR camera to provide information about the integrity of the the component under inspection [15,16]. As thermal waves flow inside the sample by diffusion, the heat diffusion rate over used to detect and quantify material damage 17 For this reason, active IRT has very competitive costs a material defect will differ from theNDE surrounding area and resulting thermal response cansystem be used compared to more sophisticated equipment such as the ultrasonic phased array and X-ray to (CT-Scan).

Optically
Method variations
Pulsed Thermography
Lock-In Thermography
Illustration of the wing its schematic analysed with
Step Heating and Long Pulse Thermography
Frequency Modulated
Step Heating and Long Pulse
Laser-Spot Thermography and Laser-Line Thermography
Ultrasonic Stimulated Thermography
14. Modelling
Ultrasonic Stimulated Thermography Using the Local Damage Resonance Effect
Nonlinear Ultrasonic Stimulated Thermography
Eddy Current
19. Comparison
Material-Based Thermography
Direct Material-Based Thermography
Indirect Material-Based Thermography
Metal-Based Thermography
Carbon Nanotubes-Based Thermography
Shape Memory Alloys-Based Rapid Thermography
Conclusions
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