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Plain fatigue and fretting fatigue strengths of AC4CH aluminum alloy

机译:AC4CH铝合金的平滑疲劳和疲劳强度

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Plain fatigue, fatigue crack growth and frettingfatigue tests were carried out using cast Al-Si aluminum alloy JISAC4CH-T6 as well as the forged aluminum alloy JIS 6061-T6.Plain fatigue strength of the cast aluminum alloy was lower thanthat of the forged alloy. The lower fatigue strength was attributedto casting defects such as pores in the cast aluminum alloy, whichenhanced fatigue crack formation. On the other hand, frettingfatigue strength of the cast aluminum alloy was almost equal tothat of the forged alloy. No difference of both tangential forcecoefficient in fretting fatigue and fatigue crack growth rates wereobserved between the two materials. The prediction of frettingfatigue lives for both materials were made on the basis of thefracture mechanics approach. The predicted lives were in goodagreement with the experimental results.
机译:使用铸铝铝合金JISAC4CH-T6以及锻造铝合金JIS 6061-T6进行疲劳,疲劳裂纹生长和碎屑试验。铸铝合金的疲劳强度是锻造合金的较低Thanthat。 较低的疲劳强度是归因于铸造铝合金等孔的铸造缺陷,这是抗疲劳裂缝形成。 另一方面,铸铝合金的碎屑强度几乎平等地锻造锻造合金。 在两种材料之间没有切向疲劳疲劳和疲劳裂纹生长速率的切向易用的差异。 基于折衷机械方法,制定了对两种材料进行碎屑寿命的预测。 预测的生命与实验结果进行了真实性。

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