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Residual stress assessment for shot peened nickel based superalloy by eddy current technique

机译:利用涡流技术评估喷丸镍基高温合金的残余应力

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摘要

Surface enhancement treatment by shot peening has been widely used in industrial applications, especially for aircraft engine components. Typical peening processes use small shots of a few hundred micrometer in diameter blasted on component surfaces, resulting in residual stress near the surface in the depth range of a few hundred micrometers nominally. Compressive surface residual stress is useful for improving crack initiation resistance that prolongs service life of the part. To implement this highly desirable maintenance strategy, an in-service nondestructive method is needed to monitor the residual stress state of parts periodically, so that appropriate maintenance actions can be taken when residual-stress protection is lost, by either replacing or re-treating the part. X-ray and neutron diffraction methods are the only two standard methods considered the most reliable. However, conventional XRD methods can achieve relatively low penetration depth (\u3c10 mum for most metals), and hence destructive layer removals are needed for measuring residual stress profiles which typically range from 200 mum to 2000 mum in depth for shot-peened materials of practical interest. Neutron diffraction method has also a practical limitation in terms of its cost and resulting radioactivity. In this dissertation, we developed a swept high frequency eddy current (SHFEC) measurement methodology for conductivity characterization of shot peened nickel based alloys. A model-based, eddy current inversion method is presented and applied to the SHFEC data obtained from a series of shot peened nickel based alloys to determine the depth profiles of actual conductivity up to 400 mum below the samples\u27 surfaces. By developing a modified piezo-resistivity theory that includes the effect of texture on stress-induced conductivity changes, the residual stress profile of a shot peened IN718 sample is obtained from eddy current data. The obtained residual stress depth profile agrees with that measured by the standard layer removal XRD method. Texture profile of the shot peened IN718 sample is demonstrated by an XRD partial pole figure and orientation image microscopy (OIM). A new procedure of analyzing conventional theta--2theta XRD data is also developed in this dissertation for determining residual stresses in shot peened surfaces assuming an isotropic plane stress state. Collectively, this work lays foundation to the eddy current technique to assess residual stress in shot peened nickel based alloys that have extensive applications in aircraft engines.
机译:通过喷丸处理进行的表面增强处理已广泛用于工业应用中,尤其是飞机发动机部件。典型的喷丸处理使用直径为几百微米的小喷丸喷丸在部件表面上,从而导致表面附近的残余应力名义上在几百微米的深度范围内。压缩表面残余应力可用于改善抗裂纹萌生性,从而延长零件的使用寿命。为了实施这一非常理想的维护策略,需要一种在役的非破坏性方法来定期监视零件的残余应力状态,以便当残余应力保护丢失时,可以通过更换或重新处理零件来采取适当的维护措施。部分。 X射线和中子衍射法是唯一被认为最可靠的两种标准方法。但是,传统的XRD方法可以实现相对较低的穿透深度(对于大多数金属而言),因此需要去除破坏性的层来测量残余应力曲线,对于实际应用中的喷丸处理材料,其残余深度通常在200μm至2000μm之间。利益。中子衍射法在成本和产生的放射性方面也有实际限制。在本文中,我们开发了一种扫频高频涡流(SHFEC)测量方法,用于表征喷丸处理的镍基合金的电导率。提出了一种基于模型的涡流反演方法,并将其应用于从一系列喷丸处理的镍基合金获得的SHFEC数据中,以确定样品表面以下至400 mum的实际电导率的深度曲线。通过开发一种改进的压阻理论,该理论包括纹理对应力引起的电导率变化的影响,可以从涡流数据中获得喷丸的IN718样品的残余应力分布。所获得的残余应力深度轮廓与通过标准层去除XRD方法测得的残余应力深度轮廓一致。用XRD偏极图和取向图像显微镜(OIM)证明了喷丸的IN718样品的纹理轮廓。本论文还开发了一种分析常规θ-2θXRD数据的新方法,用于确定在各向同性平面应力状态下喷丸处理表面的残余应力。总的来说,这项工作奠定了涡流技术的基础,该技术用于评估喷丸处理的镍基合金中的残余应力,这些合金在飞机发动机中得到了广泛的应用。

著录项

  • 作者

    Shen, Yuping;

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  • 年度 2007
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  • 原文格式 PDF
  • 正文语种 en
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