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首页> 外文期刊>International Journal of Fatigue >Effect of microstructure on fretting fatigue and sliding wear of highly workable titanium alloy, Ti-4.5Al-3V-2Mo-2Fe
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Effect of microstructure on fretting fatigue and sliding wear of highly workable titanium alloy, Ti-4.5Al-3V-2Mo-2Fe

机译:显微组织对高加工钛合金Ti-4.5Al-3V-2Mo-2Fe微动疲劳和滑动磨损的影响

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摘要

The effects of frictional wear characteristics and microstructural factors such as volume fraction and diameter of primary a phase on fretting fatigue strength of Ti-4.5Al-3V-2Mo-2Fe annealed at various temperatures were investigated in this study. The fretting fatigue life of Ti-4.5Al-3V-2Mo-2Fe is hardly affected by the volume fraction and diameter of the primary a phase in the low cycle fretting fatigue life region. The fretting fatigue limit of Ti-4.5Al-3V-2Mo-2Fe tends to increase with decrease in the volume fraction and average diameter of primary a phase. However, when volume fraction and average diameter of primary a phase are below certain values, the fretting fatigue limit is lowered by coarsening of the acicular a phase, which precipitates in the beta phase region. The weight of wear debris that is swept out from the specimen surface in frictional wear test of Ti-4.5Al-3V-2Mo-2Fe tends to increase with decrease in hardness. The fretting fatigue life of Ti-4.5Al-3V-2Mo-2Fe tends to decrease with increase in the weight of wear debris that is swept out from the specimen surface in fretting fatigue test and increase in the depth of the crack growth zone caused by contact pressure.
机译:研究了在不同温度下退火的Ti-4.5Al-3V-2Mo-2Fe的摩擦磨损特性和初生a相的体积分数和直径等微观结构因素对微动疲劳强度的影响。 Ti-4.5Al-3V-2Mo-2Fe的微动疲劳寿命几乎不受低循环微动疲劳寿命区域中初生a相的体积分数和直径的影响。 Ti-4.5Al-3V-2Mo-2Fe的微动疲劳极限随着初级a相的体积分数和平均直径的减小而趋于增加。但是,当初级a相的体积分数和平均直径低于某些值时,微细疲劳极限会由于针状a相的粗化而降低,而针状a相则沉淀在β相区域。 Ti-4.5Al-3V-2Mo-2Fe的摩擦磨损试验中,从试样表面扫出的磨屑的重量会随着硬度的降低而增加。 Ti-4.5Al-3V-2Mo-2Fe的微动疲劳寿命会随着微动疲劳试验中从试样表面扫出的磨损碎片的重量增加以及由裂纹引起的裂纹扩展区深度的增加而趋于降低接触压力。

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