首页> 外文会议>Nondestructive characterization for composite materials, aerospace engineering, civil infrastructure and homeland security 2009 >Monitoring the fracture behavior of SiCp/Al alloy composites using infrared lock-in thermography
【24h】

Monitoring the fracture behavior of SiCp/Al alloy composites using infrared lock-in thermography

机译:使用红外锁定热成像法监测SiCp /铝合金复合材料的断裂行为

获取原文
获取原文并翻译 | 示例

摘要

This work deals with the study of fracture behavior of silicon carbide particle-reinforced (SiC_p) A359 aluminum alloy matrix composites using an innovative nondestructive method based on lock-in thermography. The heat wave, generated by the thermo-mechanical coupling and the intrinsic energy dissipated during mechanical cyclic loading of the sample, was detected by an infrared camera. The coefficient of thermo-elasticity allows for the transformation of the temperature profiles into stresses. A new procedure was developed to determine the crack growth rate using thermographic mapping of the material undergoing fatigue: (a) The distribution of temperature and stresses at the surface of the specimen was monitored during the test. To this end, thermal images were obtained as a function of time and saved in the form of a movie, (b) The stresses were evaluated in a post-processing mode, along a series of equally spaced reference lines of the same length, set in front of the crack-starting notch. The idea was that the stress monitored at the location of a line versus time (or fatigue cycles) would exhibit an increase while the crack approaches the line, then attain a maximum when the crack tip was on the line. Due to the fact that the crack growth path could not be predicted and was not expected to follow a straight line in front of the notch, the stresses were monitored along a series of lines of a certain length, instead of a series of equally spaced points in front of the notch. The exact path of the crack could be easily determined by looking at the stress maxima along each of these reference lines. The thermographic results on the crack growth rate of the metal matrix composite (MMC) samples with three different heat treatments were correlated with measurements obtained by the conventional compliance method, and found to be in agreement.
机译:这项工作使用基于锁定热成像的创新无损方法研究了碳化硅颗粒增强(SiC_p)A359铝合金基复合材料的断裂行为。由热机械耦合产生的热波和在样品的机械循环加载过程中耗散的本征能量由红外摄像机检测。热弹性系数允许将温度曲线转换为应力。开发了一种新的程序,该程序可以通过对经受疲劳的材料进行热像图绘制来确定裂纹的扩展速率:(a)在测试过程中监测样品表面的温度和应力分布。为此,获得的热图像是时间的函数,并以电影的形式保存。(b)在后处理模式下,沿着一系列等长,等长且等间距的参考线,评估应力在裂纹起点之前。想法是,当裂纹接近线时,在管线位置处监视的应力随时间(或疲劳周期)的变化会有所增加,然后当裂纹尖端在线上时达到最大值。由于无法预测裂纹的生长路径,并且预期裂纹的延伸路径不会沿着凹口的前面的直线,因此应力是沿着一定长度的一系列直线而不是一系列等距的点进行监测的在缺口的前面。通过查看沿这些参考线中每条参考线的应力最大值,可以轻松确定裂纹的确切路径。通过三种不同热处理对金属基复合材料(MMC)样品的裂纹扩展速率的热成像结果与常规顺应性方法获得的测量结果相关,并且发现是一致的。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号