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    王艺淋, 潘清林, 韦莉莉, 李波, 李晨. 高强7050-T7451铝合金厚板的疲劳断口特征[J]. 机械工程材料, 2013, 37(6): 26-30.
    引用本文: 王艺淋, 潘清林, 韦莉莉, 李波, 李晨. 高强7050-T7451铝合金厚板的疲劳断口特征[J]. 机械工程材料, 2013, 37(6): 26-30.
    WANG Yi-lin, PAN Qing-lin, WEI Li-li, LI Bo, LI Chen. Fatigue Fracture Characteristic of 7050-T7451 High-Strength Aluminum Alloy Thick Plate[J]. Materials and Mechanical Engineering, 2013, 37(6): 26-30.
    Citation: WANG Yi-lin, PAN Qing-lin, WEI Li-li, LI Bo, LI Chen. Fatigue Fracture Characteristic of 7050-T7451 High-Strength Aluminum Alloy Thick Plate[J]. Materials and Mechanical Engineering, 2013, 37(6): 26-30.

    高强7050-T7451铝合金厚板的疲劳断口特征

    Fatigue Fracture Characteristic of 7050-T7451 High-Strength Aluminum Alloy Thick Plate

    • 摘要: 对7050-T7451铝合金厚板进行了疲劳试验, 并采用光学显微镜、扫描电镜等观察了不同应力幅值下疲劳试样断口, 重点分析厚板试样疲劳裂纹萌生区与扩展区的微观特征。结果表明: 其疲劳裂纹主要在材料中富铁脆性化合物夹杂处萌生, 其位置一般为材料表面或者近表面区, 在240 MPa应力幅值下, 裂纹源距表面距离约为158.64 μm, 而在340 MPa应力幅值下的距离约为120.10 μm; 裂纹扩展区域出现了二次裂纹、峭壁等微观特征, 且疲劳辉纹的间距随应力幅值的增大而增大。

       

      Abstract: The fatigue test for 7050-T7451 high-strength aluminum alloy thick plate was carried out, and the fatigue fractures at different stress amplitudes were observed by optical microscopy and scanning electron microscopy. The microscopic characteristics of crack initiation region and crack propagation region of the alloy were analyzed with an emphasis. The results showed that the fatigue cracks initiated from or near the surface of the specimen where the brittle Fe-rich compound inclusion particles were. The distance from crack initiation to the surface was 158.64 μm under stress amplitude of 240 MPa, while it was 120.10 μm under the stress amplitude of 340 MPa. The micro characteristics of second crack and cliffs exhibited on crack propagation region. And the larger the stress was, the wider the fatigue striations were.

       

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