用于飞机结构无损检测的x射线诱发声计算机断层扫描

T. Tran, Pratik Samant, L. Xiang, Yingtao Liu
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引用次数: 3

摘要

几十年来,飞机失事一直是航空公司,尤其是消费者关注的问题。世界各地的科学家一直在不断努力研究、发现和发明新的测试和预防方法,以减少未来的飞机事故。其中一种方法是无损检测,它是一种广泛适用于分析大阵列物体结构完整性的方法。x射线、超声波和计算机断层扫描(CT)是商用飞机维修中常用的无损检测应用。这些飞机结构无损检测方法为我们提供了高质量的结构损伤图像,但在图像的分辨率和对比度机制方面存在一些不足。本研究的目的是通过k波MATLAB工具箱的仿真,演示x射线诱导声计算机断层扫描(XACT)成像方法用于缺陷检测和定位的概念。XACT是一种基于x射线诱导声效应的技术。在XACT中,需要短脉冲的x射线来实现热响应并产生声波。x射线到达物体时,光子被吸收,使物体的温度升高,由于热弹性膨胀而产生声波。这些声波然后被超声波换能器检测到。在飞机的机身内,飞机的加强筋是使用SolidWorks设计的。伴随着两种不同类型的缺陷,通过空隙,由于制造过程的不完善。此外,在MATLAB中创建了由于机械故障导致的模型表面裂纹。我们选择了铝6065和因科乃尔625材料的两种特性进行模拟研究,因为它经常用于机身和/或飞机发动机。XACT图像是在高x射线吸收和超声换能器的结合下产生的,它将能够克服x射线成像技术和超声成像技术在图像分辨率和对比度机制上的缺点。仿真研究结果表明,XACT方法不仅可以获得高分辨率的图像,而且可以获得更高的图像对比度,从而可以检测所创建对象的位置精度。
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X-Ray Induced Acoustic Computed Tomography for Non-Destructive Testing of Aircraft Structure
For decades, aircraft disasters have always been a concern for airline companies and especially for consumers. Scientists all over the world have been constantly trying to study, discover and invent new methods for testing and prevention to reduce future aircraft accidents. One of those methods is non-destructive testing, which is a widely adaptive process for analyzing structural integrity over wide arrays of object. X-rays, ultrasound and computed tomography (CT) are non-destructive testing applications commonly used for the commercial aircraft maintenance. These non-destructive testing methods for aircraft structures give us high-quality images of structural damage but, there are some disadvantages related to resolution and the contrast mechanism of the image. The goal of this study is to demonstrate the concept of X-Ray Induced Acoustic Computed Tomography (XACT) imaging method for defect detection and localization through simulations using k-wave MATLAB toolbox. XACT is a technique based on the X-ray induced acoustic effect. In XACT, a short pulsed of X-rays are required to achieve thermal response and generate acoustic waves. X-ray travels to an object, the photons are absorbed causing the temperature in the object to raise, which generates acoustic waves due to thermoelastic expansion. These acoustic waves are then detected by ultrasonic transducers. Within the fuselage of the aircraft, the aircraft’s stiffener is designed using SolidWorks. along with two different types of defects through voids due to manufacturing imperfection process. As well as, cracks in the surface of the model due to mechanical failures are created in MATLAB. Two properties of Aluminum 6065 and Inconel 625 materials were selected for our simulation study since it is often used for the fuselage and/or aircraft engines. XACT images are generated under the combination of high X-ray absorption and ultrasonic transducers that will be able to overcome the disadvantages of the X-ray imaging technique and ultrasound imaging technique in image resolution and contrast mechanisms. The results from this simulation study demonstrate that the XACT method not only gives us high-resolution images but moreover, higher contrast of images that also allows us to detect position accuracy of the cons created.
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