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Proceedings of the 2020 International Conference on Quantitative InfraRed Thermography最新文献

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Thermal analysis of impact damage of prepreg composite materials 预浸料复合材料冲击损伤的热分析
P. Bagavac, L. Krstulović-Opara, Ž. Domazet
Composite materials are employed in industry at a high rate, and the demand is increasing. Recently, prepreg carbon and aramid-carbon composite structures, when compared to carbon fiber reinforced polymer composites, have attracted increasing attention due to their better impact damage resistance. In order to characterize the material, impact test according to EN DIN 6038 was carried out including infrared acquisition of impact. Based on the cooled MW InSb detector IR camera, the spread of damage was observed during impact test.
复合材料在工业上的应用速度很快,需求量也在不断增加。近年来,与碳纤维增强聚合物复合材料相比,预浸碳和芳纶-碳复合材料结构由于具有更好的抗冲击损伤性而越来越受到人们的关注。为了对材料进行表征,根据6038进行了冲击试验,包括红外冲击采集。基于冷却的MW InSb探测器红外相机,观察了冲击试验过程中损伤的扩展情况。
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引用次数: 0
Quantitative inspection of thickness of thermally sprayed coatings by flash pulse thermographic method 用闪光脉冲热成像法定量检测热喷涂涂层的厚度
M. Švantner, L. Muzika, A. Moskovchenko, Š. Houdková, Petra Frková
Flash-pulse thermography is a method for a detection of discontinuities or inhomogeneities in materials at their surface. It is based on an excitation of an inspected sample by a short pulse and analysis of its thermal response. An application of flash-pulse thermography for a quantitative inspection of thickness differences of thermally sprayed coatings is introduced in this contribution. Requirements for a synchronization of thermal response recording and data smoothing precision are described. Signal derivative, pulse-phase and time power-transformation (P-function) methods for an evaluation of the thermographic records are presented. Procedure and results of the inspection are demonstrated on HVOF, TWAS and flame sprayed coatings. A comparison of the method showed that the P-function method is the most suitable for a quantification of coating thickness differences. Some characteristic of the method are demonstrated by numerical computation.
闪光脉冲热成像是一种检测材料表面不连续性或不均匀性的方法。它是基于被检测样品的短脉冲激励和热响应分析。本文介绍了闪光脉冲热成像技术在热喷涂涂层厚度差定量检测中的应用。描述了热响应记录同步和数据平滑精度的要求。给出了评价热成像记录的信号导数、脉冲相位和时间功率变换(p函数)方法。介绍了HVOF、TWAS和火焰喷涂涂层的检测过程和结果。结果表明,p函数法最适合于镀层厚度差的定量分析。通过数值计算验证了该方法的一些特点。
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引用次数: 0
A robust multi-scale gapped smoothing algorithm for baseline-free damage mapping from raw thermal images in flash thermography 一种鲁棒的多尺度间隙平滑算法用于闪光热成像中原始热图像的无基线损伤映射
G. Poelman, S. Hedayatrasa, J. Segers, W. Paepegem, M. Kersemans
Flash thermography is a promising non-destructive testing technique for the inspection of composite components. However, non-uniform heating, measurement noise and lateral heat diffusion complicate the interpretation of thermographic measurements. In order to overcome these difficulties, a novel baseline-free processing technique called ‘Multi-Scale Gapped Smoothing Algorithm’ is presented. This algorithm constructs a damage map directly from the measured data, in which an (almost) zero-reference background is obtained, and where measurement noise and excitation non-uniformity are effectively suppressed. The efficiency of the proposed technique is evaluated and confirmed through synthetic data and experimental results of a carbon fiber reinforced polymer with various artificial defects.
闪蒸热成像技术是一种很有前途的复合材料构件无损检测技术。然而,不均匀加热、测量噪声和侧向热扩散使热成像测量的解释复杂化。为了克服这些困难,提出了一种新的无基线处理技术——“多尺度间隙平滑算法”。该算法直接从测量数据中构建损伤图,该损伤图获得了一个(几乎)零参考背景,并且有效地抑制了测量噪声和激励非均匀性。通过合成数据和具有各种人工缺陷的碳纤维增强聚合物的实验结果,对该技术的有效性进行了评价和验证。
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引用次数: 1
Correlation between the reading of a thermal imaging camera and the focus of an electronic component thermogram 热成像仪读数与电子元件热成像焦点之间的关系
K. Dziarski
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引用次数: 0
Diagnostic accuracy in thermographic imaging for granulation of uninfected diabetic ulcers. 未感染糖尿病溃疡肉芽肿的热成像诊断准确性。
R. D, C. J, Benites-Castillo S
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引用次数: 1
Absolute Temperature Field Measurements in Flames based on Infrared ThermoSpectroscopic Imaging 基于红外热光谱成像的火焰绝对温度场测量
A. Aouali, S. Chevalier, A. Sommier, J. Batsale, C. Pradère
Plasma torches are a type of source that generates very high temperatures. They are mainly used in surface treatment applications and ultimate waste treatment. The knowledge of the temperature field in plasma torches is of prime interest for researchers and industry to model and optimize the torch design. First experiments to measure the plasma torch temperature were reported by J.-L. Gardarein et al. [1] using a probe with a thermocouple directly inserted into the plasma. This first measurement led to the knowledge of plasma heat flux, but it was an intrusive method which gives only a single average value. To move forward, researches at I2M are conducted in collaboration with Europlasma to thermally and chemically characterize plasma torches with the end goal of 3D non-contact heat flux and temperature field measurements. To ensure the previous objective, radiometric techniques are developed which provide adequate means to measure contactless temperature [2]. This temperature can be deduced from the luminance measured using an IR camera if the emissivity of the body is known [3]. In flame measurements, the assumption of thermal equilibrium is generally done [4] which makes the cartography of the emissivity, ε, to be equal to the absorptivity, α. Thus, by measuring the transmissivity,τ, of an IR beam through the flame, one can deduce the absorptivity, where α = 1 − τ in semi-transparent medium, and therefore obtain ε. This methodology is validated at the lab scale using a small flame generated by a burner, an IR source and camera. In Figure 1, the experimental setup to measure the flame temperature is depicted. Three simultaneous acquisitions are made using a shutter synchronized with the camera: (1) the IR source beam alone, (2) the IR source beam + the proper emission of the flame, and (3) the proper emission of the flame alone. From this 3-images method, the total hemispheric transmissivity τ is measured. This result is presented is Figure 2(a) where the thermo-dependence of the transmittivity in the flame is observed. The transmittivity ranges from 0.16 to 0.4, which leads to an emissivity range between 1 and 0.84 (Figure 2(b)). As expected, the flame differs from the black body (emissivity of 1) which has justified the need of emissivity measurements to obtain the true flame temperature from an IR camera. This thermodependency of emissivity is expected to be strengthened in plasma torches which reach 5000 K (about 4-5 time hotter than the flame used in this experiments). In the oral presentation, this 3-images methodology will be presented in details and results of flame temperature measurements will be reported. Fig. 1. Set-up used for the 3-images method 10.21611/qirt.2020.085 15 Quantitative InfraRed Thermography Conference, 6 – 10 July 2020, Porto, Portugal 2 Fig. 2. (a). Cartography of Transmissivity, (b). Cartography of Emissivity
等离子体火炬是一种产生非常高温度的光源。它们主要用于表面处理应用和最终废物处理。等离子体火炬的温度场知识是研究人员和行业对火炬设计建模和优化的主要兴趣。j - l首次报道了测量等离子炬温度的实验。Gardarein等人[1]使用带有热电偶的探针直接插入等离子体。这第一次测量导致了对等离子体热流的认识,但它是一种侵入性的方法,只给出了一个平均值。为了进一步推进,I2M与Europlasma合作开展了研究,对等离子体火炬进行热化学表征,最终目标是三维非接触式热通量和温度场测量。为了确保上述目标,开发了辐射测量技术,为测量非接触式温度提供了足够的手段[2]。如果已知物体的发射率[3],则可以从使用红外相机测量的亮度推断出该温度。在火焰测量中,一般采用热平衡假设[4],使发射率ε等于吸收率α。因此,通过测量红外光束通过火焰的透射率τ,可以推导出吸收率,其中α = 1 - τ在半透明介质中,因此得到ε。该方法在实验室规模上通过燃烧器、红外光源和相机产生的小火焰进行了验证。在图1中,描述了测量火焰温度的实验装置。使用与相机同步的快门进行三次同时采集:(1)单独的红外源光束,(2)红外源光束+火焰的适当发射,(3)单独的火焰的适当发射。利用这种三图像方法,测量了总半球透射率τ。该结果如图2(a)所示,其中观察到火焰透射率的热依赖性。透射率范围为0.16 ~ 0.4,发射率范围为1 ~ 0.84(图2(b))。正如预期的那样,火焰不同于黑体(发射率为1),这证明需要发射率测量才能从红外相机获得真实的火焰温度。这种发射率的热依赖性预计将在达到5000 K的等离子体火炬中得到加强(大约比本实验中使用的火焰热4-5倍)。在口头报告中,将详细介绍这种三图像方法,并报告火焰温度测量的结果。图1所示。第15届定量红外热成像会议,2020年7月6日至10日,葡萄牙波尔图,图2。(a)透射率制图,(b)发射率制图
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引用次数: 0
Discontinuous finite element numerical modelling for infrared thermographic crack characterization 红外热成像裂纹表征的非连续有限元数值模拟
J. Rodríguez-Aseguinolaza, J. González, R. Celorrio, A. Mendioroz, A. Salazar
A new numerical model based on discontinuous Galerkin Finite Element Methods for laser spot lock-in thermopgraphy has been developed able to characterize very narrow cracks in materials, difficult to quantify by alternative numerical methods. It has also been validated by means of experimental results from a wide variety of cracks in terms of size, width, depth and crack orientation angle. Overall, the obtained results indicate a very good agreement with experiments maintaining a satisfactory accuracy and improved computational economy.
基于非连续Galerkin有限元方法,建立了一种新的激光光斑锁定热成像数值模型,该模型能够表征材料中非常窄的裂纹,而其他数值方法难以量化。并通过各种裂纹在尺寸、宽度、深度和裂纹取向角等方面的实验结果进行了验证。总体而言,所得结果与实验结果非常吻合,保持了令人满意的精度,提高了计算经济性。
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引用次数: 0
Analysis of paint thickness based on flash pulse thermography 基于闪光脉冲热成像的涂料厚度分析
L. Muzika, M. Švantner
Coating thickness (thermal barrier coatings, anticorrosion paints, etc.) can influence its properties and therefore the thickness is often measured in industrial application. This contribution describes fast areal thickness estimation based on flash pulse thermography. Specimens sprayed by a black paint on AISI 304 substrates were used for a demonstration of the thickness estimation. Two different types of post-processing and thickness estimation were used: functional calibration with FFT (phase) and analytical model. Both procedures were compared and both provided satisfactory results with maximum error of thickness estimation less than 10 %. Advantages and disadvantages of proposed techniques are discussed.
涂层厚度(热障涂层、防腐涂料等)会影响其性能,因此在工业应用中经常测量厚度。这一贡献描述了基于闪光脉冲热成像的快速面厚度估计。用黑色涂料喷涂在aisi304衬底上的样品用于厚度估计的演示。采用两种不同类型的后处理和厚度估计:FFT(相位)功能校准和分析模型。两种方法的比较结果均令人满意,厚度估计的最大误差小于10%。讨论了所提技术的优缺点。
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引用次数: 0
Parametric simulation of Induction Thermography for optimal cracks detection and characterization 感应热成像的参数化模拟,用于最佳的裂纹检测和表征
Ghibaudo Olivier, Foucher Fabrice, Kalai Anouar
In the last few years, induction thermography has been identified as a non-destructive testing method for detecting and characterizing surface cracks in metals. The sample to be inspected is heated with a short induced electrical current pulse, and the infrared camera records the temperature distribution and transient temporal behavior at the surface during and after the heating pulse. In this work, 3D Finite element simulations, performed with the software FLUX©, were carried out to investigate how the thermal contrast depends on parameters such as excitation frequency, pulse duration, material parameters, crack depth and length. 1. Simulation description To compare the simulations with the experimental results, the modeled inductor is a realistic U-ferritic yoke surmounted by a copper winding. The two block samples involve two materials massively used in aeronautics: the first one is paramagnetic (nickel based superalloy INCONEL 718), the second one is ferromagnetic (low carbon steel 16CND13), which implies very different skin depths. The magnetic excitation frequency varies between 10 kHz and 600 kHz, and the step heating duration between 10 to 100 ms. Also, the length of the notch varies between 0.2 mm to 5 mm and the depth between 0.1 to 5 mm. A total of 360 configurations have been simulated. The multiphysical simulations take into account the non-linearity of the sample magnetic permeabilities, which makes it possible to calculate finely the total impedance of the inductor at each magnetic frequency. For a current imposed excitation through the inductor, this allows to normalize the observations with respect to the active and reactive power consumed by the inductor. (a) (b) (c) Fig. 1. (a) : Real inductor from Edevis©. (b) : schematic view of the problem : in green the ferrite of the inductor, in blue the plate sample, in red the defect (notch). (c) cross section of the mesh problem. (a) (b) (c) (d) Fig. 2. (a) : Simulation results : temperature distribution on the surface of Inconel sample at t=100 ms and fmag=100 kHz. (b) : without defect. (c) defect height=0.5 mm and length=2.5 mm. (d) : defect height=2 mm and length=2.5 mm. 10.21611/qirt.2020.076 15 Quantitative InfraRed Thermography Conference, 6 – 10 July 2020, Porto, Portugal 2 2. Signal analysis From the temperature distributions at each time step, the analysis of the differential thermal contrast between a defect situation and a defect-free situation, emphasizes the detectability of the defect as a function of the introduced parametric variations. The thermal-temporal extractions provided are used firstly to find the optimal excitation parameters (frequency of the induced currents, heating duration) which maximizes the thermal contrast, and on the other hand to define a methodology for sizing defects according to their lengths and depths. The optimum contrast calculated on the phase of the Fourier Transform (Pulse Phase Thermography PPT) provides credible but sensitive information
在过去的几年中,感应热成像已被确定为一种无损检测方法,用于检测和表征金属表面裂纹。用短脉冲感应电流加热待测样品,红外摄像机记录加热脉冲期间和之后样品表面的温度分布和瞬态时间行为。在这项工作中,使用FLUX©软件进行了三维有限元模拟,以研究热对比如何依赖于激励频率、脉冲持续时间、材料参数、裂纹深度和长度等参数。1. 为了将模拟结果与实验结果进行比较,模拟的电感器是一个真实的u -铁素体轭,上面有一个铜绕组。这两个块样品涉及航空领域大量使用的两种材料:第一个是顺磁性的(镍基高温合金INCONEL 718),第二个是铁磁性的(低碳钢16CND13),这意味着非常不同的蒙皮深度。磁激励频率在10khz ~ 600khz之间,步进加热时间在10 ~ 100ms之间。此外,缺口的长度在0.2毫米至5毫米之间变化,深度在0.1至5毫米之间变化。总共模拟了360种配置。多物理场模拟考虑了样品磁导率的非线性,从而可以精确地计算出电感器在各个磁频下的总阻抗。对于通过电感施加的励磁电流,这允许对电感消耗的有功和无功功率进行归一化观察。(a) (b) (c)图1(a):来自Edevis的真实电感©。(b):问题示意图:绿色为电感的铁氧体,蓝色为板样,红色为缺陷(缺口)。(c)网格问题的横截面。(a) (b) (c) (d)(a):仿真结果:t=100 ms, fmag=100 kHz时,Inconel试样表面温度分布。(b):无缺陷。(c)缺陷高度=0.5 mm,长度=2.5 mm。(d)缺陷高度= 2mm,长度=2.5 mm。10.21611/qirt.2020.076 15定量红外热成像会议,2020年7月6 - 10日,波尔图,葡萄牙2。信号分析从每个时间步长的温度分布,分析缺陷情况和无缺陷情况之间的热差对比,强调缺陷的可检测性是引入参数变化的函数。所提供的热时间提取首先用于找到最佳的激励参数(感应电流的频率,加热持续时间),使热对比度最大化,另一方面定义了根据其长度和深度确定缺陷尺寸的方法。根据傅里叶变换(脉冲相位热成像PPT)的相位计算的最佳对比度提供了与激励参数和缺陷几何参数相关的可靠而敏感的信息。最后,本文将比较两种分析方法:PPT和小波脉冲相控热成像。图3所示。不同激励和缺陷参数下快速傅里叶变换的时间变化和相位。数据是在缺陷正交轴附近的表面上的一个点上计算的。使差分对比度最大化的FFT fopt的最佳分析频率随阶跃加热时间和缺陷的大小而变化。10.21611 / qirt.2020.076
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Proceedings of the 2020 International Conference on Quantitative InfraRed Thermography
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