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首页> 外文期刊>Journal of Materials Science >Cyclic deformation and damage behaviour of the spring steel wire reinforced aluminium alloy EN AW-6082
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Cyclic deformation and damage behaviour of the spring steel wire reinforced aluminium alloy EN AW-6082

机译:弹簧钢丝增强铝合金的周期性变形和损伤行为EN AW-6082

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摘要

The demand for lightweight materials used for constructions in automotive applications, e.g. space frames, requests for composite materials such as reinforced aluminium extrusions with a high specific stiffness and strength. This contribution shows that a spring steel wire reinforcement content of 11.1 vol% leads to a significant increase in fatigue life of monofilament composite extrusions based on the aluminium alloy, EN AW-6082, in heat treatment state T4 under stress controlled fatigue loading. As groundwork, the cyclic deformation and damage behaviour of the unreinforced matrix material is investigated in detail. Beside the determination of three stages of deformation and damage, the reason for the high fatigue strength in comparison to the quasi-static offset yield strength is also clarified. The main aim of the research focusses on the description of the mechanisms and mechanics of constituent deformation and damage evolution of 11.1 vol% spring steel wire reinforced EN AW-6082, which is presented quantitatively and qualitatively by metallographic means. The three stages represent the deformation and damage of the matrix material, whereas the fourth stage is characterised by the fatigue of the reinforcing element. Based on the knowledge of the quasistatic behaviour of the single components and the fatigue behaviour of the single matrix material, a new lifetime model is deduced from the strain response in order to predict the fatigue life for unidirectionally reinforced material systems.
机译:对汽车应用中建筑用轻质材料的需求空间框架,对复合材料的要求,例如具有较高比刚度和强度的增强铝挤压件。该贡献表明,弹簧钢丝增强含量为11.1 vol%时,在应力控制的疲劳载荷下,热处理状态T4下,基于铝合金EN AW-6082的单丝复合材料挤出件的疲劳寿命显着增加。作为基础,详细研究了未增强基体材料的周期性变形和破坏行为。除了确定变形和损坏的三个阶段外,还阐明了与准静态偏移屈服强度相比,疲劳强度较高的原因。本研究的主要目的是描述用金相学方法定量和定性描述的11.1%(体积)弹簧钢丝EN AW-6082的组成变形和损伤演化的机理和力学。这三个阶段代表了基体材料的变形和损坏,而第四阶段的特征是增强元件的疲劳。基于单组分的准静态行为和单基体材料的疲劳行为的知识,从应变响应推导出新的寿命模型,以便预测单向增强材料系统的疲劳寿命。

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