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NEAR-SURFACE RESIDUAL STRESS-PROFILING WITH HIGHFREQUENCY EDDY CURRENT CONDUCTIVITY MEASUREMENT

机译:近表面残余应力 - 具有高频率涡流电导率测量的剖析

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The lifetime of aero engine components can be extended by applying an additionalstrain to the material. Typical aero engine-alloys like Nickel-Base superalloys or Titanium alloys canbe surface-treated by use of shot peening to induce the compressive strain near the surface.However, in order to use the additional life for critical aero engine components, a quantitativedetermination of strain gradients near the surface has to be carried out periodically. We propose tomeasure the depth-profile of residual stresses non-destructively by use of high frequency eddycurrent techniques. This paper presents results obtained with an experimental set-up based on a highprecision impedance analyzer. Test samples prepared from IN718 by shot peening of differentintensities can be easily distinguished. By sweeping the frequency from 100 kHz up to 100 MHz adepth profile for the electrical conductivity from 50 pm to 500 gm can be obtained. The measuredconductivity profile is a resultant from residual stresses, cold work, surface roughness and thetexture of the material. In addition, first results for strain profiling obtained with industry applicableNDE instrument will be presented.
机译:可以通过将额外的粒子施加到材料来延伸航空发动机部件的寿命。典型的航空发动机合金,如镍基超合金或钛合金可以通过使用喷丸诱导表面处理,以诱导表面附近的压缩菌株。然而,为了利用临界航空发动机部件的额外寿命,菌株的定量测定。表面附近的梯度必须定期进行。我们提出了通过使用高频射频技术而非破坏性的抗损伤的深度曲线。本文介绍了基于高精度阻抗分析仪的实验设置获得的结果。可以容易地区分由射击喷丸的射击喷丸的测试样品。通过将100kHz的频率从100KHz扫描到100 MHz的频率,可以获得从50pm至500克的导电率的推动。测量的曲线是由物质的残余应力,冷加工,表面粗糙度和材料的缩小。此外,将提出使用工业应用型仪器获得的第一个结果剖面。

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