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基于Monte-Carlo模拟的小样本下齿轮疲劳极限计算方法及软件开发 被引量:4
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作者 李扬 刘怀举 +2 位作者 魏沛堂 毛天雨 陈地发 《中国机械工程》 EI CAS CSCD 北大核心 2023年第2期185-192,共8页
齿轮疲劳极限评估Dixon-Mood(D-M)法的试验样本需求量较大,标准差估计值存在较大偏差,因此基于Monte-Carlo模拟提出小样本的齿轮疲劳极限分析方法(CQUboot),并结合大量弯曲疲劳极限试验对D-M法和CQUboot法进行了对比分析。与GB/T 14230... 齿轮疲劳极限评估Dixon-Mood(D-M)法的试验样本需求量较大,标准差估计值存在较大偏差,因此基于Monte-Carlo模拟提出小样本的齿轮疲劳极限分析方法(CQUboot),并结合大量弯曲疲劳极限试验对D-M法和CQUboot法进行了对比分析。与GB/T 14230—2021《齿轮弯曲疲劳强度试验方法》推荐的20~22个样本计算结果相比,样本量降至12时,D-M法的最大误差为15.76%~24.99%,CQUboot法为8.02%~12.98%;以12.66%为疲劳极限预估允许的最大误差时,D-M法至少需要10~18个样本点,CQUboot法只需8个样本点。 展开更多
关键词 齿轮疲劳极限 Dixon-Mood法 MONTE-CARLO模拟 试验验证 软件开发
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Corrosion fatigue behavior of epoxy-coated Mg-3Al-1Zn alloy in gear oil 被引量:1
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作者 贺秀丽 卫英慧 +3 位作者 侯利锋 闫志峰 郭春丽 韩鹏举 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2014年第11期3429-3440,共12页
The corrosion fatigue behavior of epoxy-coated Mg-3Al-1Zn alloy in gear oil was investigated. The corrosion and the fracture surfaces after fatigue test were analyzed by scanning electron microscopy(SEM) and the corro... The corrosion fatigue behavior of epoxy-coated Mg-3Al-1Zn alloy in gear oil was investigated. The corrosion and the fracture surfaces after fatigue test were analyzed by scanning electron microscopy(SEM) and the corrosion compositions were measured by energy-dispersive spectrometry(EDS). The fatigue properties and the crack initiation mechanisms of the specimens before and after epoxy coating treatment were discussed. The results indicate that the fatigue limit after epoxy coating treatment in gear oil is higher than that of the uncoated specimens. The epoxy coating is an excellent way to prevent direct contact between the Mg-3Al-1Zn alloy and surrounding environments. The mechanical properties of the epoxy coating layer are lower than that of magnesium alloy, which is the main reason for the fatigue crack initiation on the epoxy coating layer. In addition, the gear oil lubrication could lead to the flaking off of the epoxy-coated layer. 展开更多
关键词 magnesium alloy gear oil epoxy coating corrosion fatigue fatigue limit fatigue crack initiation
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