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Experimental study of turbine disk residual stress measurement using Lcr wave

机译:Lcr波法测量涡轮盘残余应力的实验研究

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Turbine disk usually cracks near the arc junction between the rim and the plate (called the root of turbine disk). This paper presents the application of an ultrasonic method to measure stresses on the root of turbine disk. The ultrasonic residual stresses measurement is based on the acoustoelastic effect that refers to the change in velocity of the elastic wave when propagating in a stressed media. We employ critically refracted longitudinal waves(Lcr wave) and relate its time variation with applied stress. This paper studies the propagation law of Lcr wave in inclined surface of different angles and verifies that Lcr wave can propagate on rectangular components. The specific probe head is designed to detect residual stress on the root of the turbine disk. The experimental result shows that it is feasible to use Lcr wave to detect residual stress on the roots of the turbine disk.
机译:涡轮盘通常在轮辋和板之间的弧形接合处附近破裂(称为涡轮盘的根部)。本文介绍了超声方法在测量涡轮盘根部应力的应用。超声残余应力的测量基于声弹性效应,该声弹性效应是指在应力介质中传播时弹性波速度的变化。我们使用临界折射纵波(Lcr波),并将其时间变化与施加应力相关联。研究了Lcr波在不同角度的斜面上的传播规律,验证了Lcr波可以在矩形组件上传播。专用探头设计用于检测涡轮盘根部上的残余应力。实验结果表明,用Lcr波检测涡轮盘根部残余应力是可行的。

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