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A comparison of methods used to predict the vibrational energy required for a reliable thermosonic inspection

机译:比较用于预测可靠热超声检查所需振动能量的方法

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摘要

Thermosonics is capable of detecting cracks in several types of components. The component is excited with high-power ultrasonic vibrations, causing cracks to generate heat, which can be detected by an infrared (IR) camera. However, the excitation in a typical thermosonic test is non-reproducible and can lead to cracks being undetected if sufficient vibrational energy is not applied at the crack location. The vibrational energy dissipated as heat at the defect is directly related to the frequency and amplitude of the vibration, and this energy can be represented by a single parameter (Heating Index) computed from the vibration waveform. The Heating Index parameter is useful as it can be used to predict the vibration level required for a reliable thermosonic inspection. The aim of this work is to compare different vibration measuring devices that may be used to capture the vibration waveform required to compute the Heating Index. In this study, an aero engine turbine blade is inspected using a practical thermosonic setup, after which the vibration waveforms acquired from a laser vibrometer, microphone and strain gauge are processed. Results from this work will highlight the relative merits and limitations of these different vibration measuring devices for computing the Heating Index.
机译:Thermosonics能够检测多种类型的组件中的裂纹。高功率超声波振动会激发该组件,导致裂纹产生热量,可以通过红外(IR)摄像机检测到。但是,在典型的热超声测试中,激励是不可重现的,如果在裂纹位置未施加足够的振动能量,则可能导致无法检测到裂纹。在缺陷处作为热量散发的振动能量与振动的频率和幅度直接相关,并且该能量可以由根据振动波形计算出的单个参数(加热指数)来表示。加热指数参数很有用,因为它可用于预测可靠的热超声检查所需的振动水平。这项工作的目的是比较可用于捕获计算加热指数所需的振动波形的不同振动测量设备。在这项研究中,使用实际的热超声设置检查了航空发动机涡轮叶片,然后处理了从激光振动计,麦克风和应变仪获取的振动波形。这项工作的结果将突出显示这些用于计算热指数的不同振动测量设备的相对优缺点。

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