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Variable amplitude loading of spray-formed hypereutectic aluminium silicon alloy DISPAL® S232 in the VHCF regime

机译:喷射成型的过共晶铝硅合金DISPAL®S232在VHCF模式下的可变振幅载荷

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摘要

Spray-formed hypereutectic aluminium silicon alloy DISPAL® S232-T6x is cycled with variable amplitude at ultrasonic frequency up to the very high cycle fatigue (VHCF) regime under fully reversed tension-compression loading. The Powder Metallurgy alloy is tested using a Gaussian cumulative frequency distribution of load cycles, and lifetimes are compared with constant amplitude data. Miner calculation delivers mean damage sums between 0.5 and 0.9 for mean lifetimes between 8 × 10~7 and 1.6 × 10~(10) cycles, respectively. Cracks are initiated at voids, at inclusions or at distributed inhomogeneitdes (porous areas or oxides) at the surface or in the interior. In situ analysis of vibration properties indicates that cracks are formed and start growing from the beginning of fatigue cycling, even if failure occurs in the very high cycle fatigue regime. Crack initiation stage is negligible. Lifetime prediction calculation is performed using an adapted Paris-law and considering lifetime as cycles necessary to propagate an initial crack to failure. Measured and predicted mean lifetimes differ by factor 0.4-1.0. Large crack-initiating defects strongly reduce the fatigue lifetimes, which is successfully covered in the crack propagation model.
机译:喷涂成型的过共晶铝硅合金DISPAL®S232-T6x在完全反向的拉伸压缩载荷下,以可变的频率在超声波频率下循环至非常高的循环疲劳(VHCF)状况。使用负载循环的高斯累积频率分布对粉末冶金合金进行测试,并将寿命与恒定振幅数据进行比较。矿工计算得出的平均损害总和分别为8×10〜7和1.6×10〜(10)个周期的平均寿命。裂纹是在表面或内部的空隙,内含物或分布的不均匀性(多孔区域或氧化物)处引发的。振动特性的原位分析表明,即使在非常高的循环疲劳状态下发生故障,也会从疲劳循环的开始就形成裂纹并开始扩展裂纹。裂纹萌生阶段可以忽略不计。使用修改后的巴黎定律并将寿命作为将初始裂纹扩展到破坏所必需的周期,来进行寿命预测计算。测量和预测的平均寿命相差0.4-1.0。较大的裂纹引发缺陷会极大地降低疲劳寿命,这在裂纹扩展模型中已得到成功覆盖。

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