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High temperature deformation of dispersion strengthened Al-Al4C3 composite

机译:分散体的高温变形强化Al-Al4C3复合材料

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The mutual relationship between mechanical properties and microstructure changes in Al-A_(1_4)C_3 composite system is characterised by tensile test in wide range of testing temperatures. The dominant mechanism of plastic deformation at the deformation temperatures up to 300 deg regardless of used strain rate was dislocation glide. In temperature region from 300 to 450 deg and for lower strain rates the grain boundary glide participates in deformation process. The phenomenon of superplasticlike behaviour was observed at deformation temperature of 450 deg and the strain rate #epsilon#=10~(-1)s~(-1). The dispersion strengthened system has been tested at 400 deg by creep and fatigue superimposed on creep stress as well. The different loading schedules were defined by the stress ratio R. The criteria used to analyse the resistance to creep, or creep-fatigue, were the life to fracture and the strain to fracture.
机译:Al-A_(1_4)C_3复合系统的机械性能与微观结构变化的相互关系,其特征在于各种测试温度的拉伸试验。无论使用常用的应变率,变形温度在变形温度下的塑性变形的主导机制是位错滑动。在温度区域,从300至450°和较低的应变速率,晶界滑动参与变形过程。在450℃的变形温度和应变率#epsilon#= 10〜(-1)S〜(-1)时观察到超塑性般的行为的现象。通过蠕变和疲劳叠加在蠕变应力上的蠕变和疲劳已经在400℃下测试了分散体系。不同的装载时间表由应力比R定义。用于分析蠕变或蠕变 - 疲劳的抗性的标准是骨折的寿命和裂缝的菌株。

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