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Study on Propagation mechanism of Stress Corrosion Crack with Laser Holographic Interferometry

机译:激光全息干涉法研究应力腐蚀裂纹扩展机理

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Aiming at high strength steel material in aerial accessory, the crack propagation mechanism of material stress corrosion is studied. The theory of laser holographic interferometry and crack extension mechanism of the material stress corrosion are chiefly discussed. The testing method is presented, which includes monitoring with laser holographic interferometry, fringe-image sampling with CCD camera and image processing. The stress corrosion monitoring system of laser holographic interference is set up accordingly. Using this system, a group of real-tune holographic interference patterns are obtained. In these fringe images, it can be seen that dim-spot position of crack tip moves down and the rule of fringe-space change is gotten. According to the test data, the changing velocity of the surface-separating displacement under a certain hour can be obtained by image processing, which is from 0.038 microns to 0.047microns per minute. At last, the measuring range of the recording medium is discussed, which provides a valid means for damage tolerance design and safe life evaluation.
机译:针对航空配件中的高强度钢材,研究了材料应力腐蚀的裂纹扩展机理。主要讨论了激光全息干涉理论和材料应力腐蚀的裂纹扩展机理。提出了一种测试方法,包括用激光全息干涉法进行监控,用CCD照相机进行条纹图像采样以及图像处理。相应地建立了激光全息干涉的应力腐蚀监测系统。使用该系统,获得了一组真实调谐的全息干涉图样。在这些条纹图像中,可以看到裂纹尖端的暗点位置向下移动,并且获得了条纹空间变化的规则。根据测试数据,可以通过图像处理获得在一定小时内表面分离位移的变化速度,该速度为每分钟0.038微米至0.047微米。最后讨论了记录介质的测量范围,为损伤容限设计和安全寿命评估提供了有效的手段。

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