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Noncontact laser ultrasonic inspection of Ceramic Matrix Composites (CMCs)

机译:陶瓷基复合材料(CMC)的非接触激光超声检查

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摘要

Ceramic matrix composites (CMCs) are poised to revolutionize jet engine technology by enabling operation temperatures well beyond those possible with current superalloys, while reducing active cooling requirements and engine weight. Manufacturing of parts formed by silicon-carbide (SiC) fibers in a SiC matrix is now well advanced, with the first non-structural static components entering service in 2017 with the CFM Leap* engine that uses SiC/SiC turbine shrouds. In order to expand the scope of application of CMCs to rotating parts, such as turbine blades, much work is being conducted to understand and characterize the modes of failure of these materials at temperatures beyond ~1100°C. In this context, the ability of nondestructively monitoring the formation and progression of damage in CMCs specimens during high-temperature mechanical testing is critical. However, the elevated temperature precludes the possibility of using sensors placed in direct contact with the specimen and therefore severely restricts the range of available NDE techniques. This paper provides the first experimental assessment of the feasibility of noncontact laser ultrasonic inspection of SiC/SiC flat coupons. An Nd: Yag laser is used to excite ultrasonic waves on one side of the specimen while a Michelson interferometer detects the signals emerging on the other side at the epicenter position. The lasers are mounted on synchronized linear stages to form C-scans as in conventional immersion ultrasonics while ablation damage to the surface of the specimen is prevented by operating the lasers at low power density. Despite the complex microstructure of the SiC/SiC material it is found that the measured waveforms are remarkably similar to those observed when conducting the same tests in aluminum specimens. Moreover, it is shown that it is possible to image interlaminar defects caused by impacts, and monitor crack opening under tensile load. Finally, very good signal stability is observed when temperature is increased from 25 to 1250 °C which confirms the feasibility of laser monitoring at high temperature and is consistent with the good thermal stability of ceramic materials.
机译:陶瓷基复合材料(CMC)有望通过使工作温度大大超过当前超级合金可能的工作温度,同时降低主动冷却要求和发动机重量,彻底改变喷气发动机技术。碳化硅(SiC)纤维在SiC基质中形成的零件的制造现在已经取得了很好的进展,第一批非结构性静态组件于2017年开始投入使用,该发动机使用SiC / SiC涡轮机罩的CFM Leap *发动机。为了扩大CMC在旋转零件(例如涡轮机叶片)中的应用范围,正在开展大量工作来理解和表征这些材料在超过1100°C的温度下的失效模式。在这种情况下,至关重要的是,在高温机械测试过程中,无损监控CMC样品损伤形成和发展的能力至关重要。但是,高温排除了使用直接与样品接触的传感器的可能性,因此严重限制了可用NDE技术的范围。本文提供了对SiC / SiC平板试样非接触激光超声检查的可行性的首次实验评估。使用Nd:Yag激光激发标本一侧的超声波,而迈克尔逊干涉仪则检测位于震中位置另一侧的信号。像传统的浸入式超声一样,将激光器安装在同步的线性平台上以形成C扫描,同时通过在低功率密度下操作激光器来防止对样品表面的烧蚀损坏。尽管SiC / SiC材料具有复杂的微观结构,但是发现测量的波形与在铝样品中进行相同测试时观察到的波形非常相似。而且,显示出可以对由冲击引起的层间缺陷进行成像,并且可以监测在拉伸载荷下的裂缝开度。最后,当温度从25升高到1250°C时,观察到非常好的信号稳定性,这证实了在高温下进行激光监测的可行性,并且与陶瓷材料的良好热稳定性相符。

著录项

  • 来源
    《NDT & E international》 |2017年第6期|8-16|共9页
  • 作者单位

    Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati, OH 45221, USA;

    Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati, OH 45221, USA;

    Next Generation Manufacturing, GE Aviation, OH 45215, USA;

    Next Generation Manufacturing, GE Aviation, OH 45215, USA;

    Composite Materials Behavior, GE Aviation, OH 45215, USA;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Laser ultrasound; Ablation; Thermoelastic; Ceramic-matrix; Composite materials; Delamination;

    机译:激光超声;消融;热弹性陶瓷基体复合材料;分层;

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