2011Proceedings of SPIE, the International Society for Optical Engineering/Proceedings of SPIERequires access

Study on detecting CFRP composites using pulsed infrared thermography

Yan Huo, Huijuan Li, Yuejin Zhao, Cunlin Zhang

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Abstract

Composite sandwich structure has been widely used in aerospace due to its lightweight, high stiffness and strength. The quality of the structure is crucial to durability and structural integrity of the rehabilitated the structure, Delaminations, debonding and water ingressing to honeycomb are typical defects in the structure. Defects in the structure will influence the quality of product. Pulse thermography has been an effective NDE method in recent ten years. The technique uses pulse to excite the specimen, because the presence of subsurface defects reduce the diffusion rate, then temperature difference between defect area and sound area will be measured by an infrared camera. Subsurface defects become visible with time delays, it is a non-contact, quickly inspection method. Pulsed infrared thermography has been widely used in aerospace and mechanical manufacture industry because it can offer non-contact, quickly and visual examinations of defects. It is a meaningful research topic to study on quantitative testing with the structure rapidly and non-destructively. Sandwich composites with aluminum facesheet and aluminum honeycomb cores are chosen as study objectives. Some back-drilled holes with different sizes and depths in the specimen are used to simulate delaminations between plies in the strcuture .The paper presents a method for defining the boundaries, quantitatively estimating the sizes of the flaws in the CFRP using pulsed infrared thermography. Processing captured data using splinefitting, measuring the size of the defects by calculating the pixels numbers that exceed the detection threshold and computing areas of defects by binary image. Compared with the designed sizes and areas having defects, the results show that the method offers more than 90% accuracies with reference to the sizes of artificial flaws embedded in the CFRP sheet. The experimental results demonstrate the feasibility of using detection threshold to inspect the CFRP sheet. The curve of the detection threshold and depth obtained could be applied for practical inspection.

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What this paper is about

Composite sandwich structure has been widely used in aerospace due to its lightweight, high stiffness and strength. The quality of the structure is crucial to durability and structural integrity of the rehabilitated the structure, Delaminations, debonding and water ingressing to honeycomb are typical defects in the structure. Defects in the structure will influence the quality of product. Pulse thermography has been an effective NDE method in recent ten years. The technique uses pulse to excite the specimen, because the presence of subsurface defects reduce the diffusion rate, then temperature difference between defect area and sound area will be measured by an infrared camera. Subsurface defects become visible with time delays, it is a non-contact, quickly inspection method. Pulsed infrared thermography has been widely used in aerospace and mechanical manufacture industry because it can offer non-contact, quickly and visual examinations of defects. It is a meaningful research topic to study on quantitative testing with the structure rapidly and non-destructively. Sandwich composites with aluminum facesheet and aluminum honeycomb cores are chosen as study objectives. Some back-drilled holes with different sizes and depths in the specimen are used to simulate delaminations between plies in the strcuture .The paper presents a method for defining the boundaries, quantitatively estimating the sizes of the flaws in the CFRP using pulsed infrared thermography. Processing captured data using splinefitting, measuring the size of the defects by calculating the pixels numbers that exceed the detection threshold and computing areas of defects by binary image. Compared with the designed sizes and areas having defects, the results show that the method offers more than 90% accuracies with reference to the sizes of artificial flaws embedded in the CFRP sheet. The experimental results demonstrate the feasibility of using detection threshold to inspect the CFRP sheet. The curve of the detection threshold and depth obtained could be applied for practical inspection.

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Available abstract

Composite sandwich structure has been widely used in aerospace due to its lightweight, high stiffness and strength. The quality of the structure is crucial to durability and structural integrity of the rehabilitated the structure, Delaminations, debonding and water ingressing to honeycomb are typical defects in the structure. Defects in the structure will influence the quality of product. Pulse thermography has been an effective NDE method in recent ten years. The technique uses pulse to excite the specimen, because the presence of subsurface defects reduce the diffusion rate, then temperature difference between defect area and sound area will be measured by an infrared camera. Subsurface defects become visible with time delays, it is a non-contact, quickly inspection method. Pulsed infrared thermography has been widely used in aerospace and mechanical manufacture industry because it can offer non-contact, quickly and visual examinations of defects. It is a meaningful research topic to study on quantitative testing with the structure rapidly and non-destructively. Sandwich composites with aluminum facesheet and aluminum honeycomb cores are chosen as study objectives. Some back-drilled holes with different sizes and depths in the specimen are used to simulate delaminations between plies in the strcuture .The paper presents a method for defining the boundaries, quantitatively estimating the sizes of the flaws in the CFRP using pulsed infrared thermography. Processing captured data using splinefitting, measuring the size of the defects by calculating the pixels numbers that exceed the detection threshold and computing areas of defects by binary image. Compared with the designed sizes and areas having defects, the results show that the method offers more than 90% accuracies with reference to the sizes of artificial flaws embedded in the CFRP sheet. The experimental results demonstrate the feasibility of using detection threshold to inspect the CFRP sheet. The curve of the detection threshold and depth obtained could be applied for practical inspection.

Key concepts: Thermography, Materials science, Delamination (geology), Nondestructive testing, Aerospace, Infrared, Honeycomb structure, Composite material

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