基于应力平均法的钛合金薄板结构疲劳评估方法

Fatigue evaluation method of titanium alloy sheet structure based on stress average method

  • 摘要:
    目的 通过设计TA23钛合金薄板母材和3种焊接接头(对接、T形、十字形)的测试试样,开展系列试验,旨在获取名义应力S-N曲线,得到各焊接接头疲劳强度。
    方法 通过试验数据和Neuber应力平均法确定了TA23钛合金焊接接头的微观结构长度,可以用于有效应力和虚拟缺口半径计算,该虚拟半径可作为TA23钛合金焊接接头的参考半径。考虑虚拟半径的影响,建立有限元模型,获取各类典型焊接接头缺口处应力梯度。
    结果 采用Neuber应力平均法,基于试验数据和应力梯度计算得到缺口有效应力,定义分散带指数,获取S-N曲线分散带指数随微观结构长度变化的曲线,结果表明,微观结构长度取0.08 mm时,分散带指数最小。
    结论 基于该微观结构长度所得到的虚拟缺口半径,可以为钛合金薄板焊接结构的缺口应力评估提供参考。

     

    Abstract: Objective A series of experiments are carried out by designing the test specimen of TA23 titanium alloy sheet base metal and three kinds of welded joints (butt, T-type and cross-type), the aim is to obtain the nominal stress S-N curve and obtain the fatigue strength of each welded joints. Methods The microstructure length of TA23 titanium alloy welded joints is determined by the experiment data and the Neuber stress average method, which can be used for the calculation of effective stress and virtual notch radius.The virtual notch radius can be used as the reference radius of TA23 titanium alloy welded joints. Considering the influence of virtual radius, a finite element model is established to obtain the stress gradient at the notch of various typical welded joints. Results The notch effective stress is calculated based on the experimental data and stress gradient by using the Neuber stress average method, the dispersion band index is defined, and the curve of the dispersion band index of the S-N curve changes with the length of the microstructure is obtained. The results show that the dispersion band index is the smallest when the length of the microstructure is 0.08 mm. Conclusion The virtual notch radius based on the microstructure length can provide a reference for the notch stress evaluation of titanium alloy sheet welding structures.

     

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