局部短期热处理对轨道成形功能部件成形性的影响

Andreas Hetzel , Marion Merklein , Michael Lechner
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引用次数: 4

摘要

传统的工艺,如剪切处理缺乏效率和成形性,以制造具有高几何多样性的功能部件。实现高效和可持续制造的一种可能性是应用创新的成形操作,如轨道成形。因此,具有适应载荷的厚度轮廓的应变硬化部件可以在单阶段工艺中制造。因此,由于三维应力和应变状态,材料流的控制可以被认为是主要的挑战。为了减轻零件重量,同时保证相同的性能水平,传统的钢被轻质材料取代,如沉淀硬化铝合金。然而,与传统钢相比,铝的成形性降低,从而带来了新的挑战。在最近的研究中,可以显示短期热处理扩大成形性的潜力。所提出的工艺在局部降低了材料强度,从而允许通过软化区域和区域之间的相互作用来控制材料流动,这提供了初始条件。本文研究了局部短期热处理对沉淀硬化铝合金enaw6016轨道成形件成形性能的影响。为了在不同的径向位置上最大限度地增厚,采用了不同几何形状的热处理布局。通过比较传统工艺路线和先前热处理制造的部件的几何和机械性能,评估提高成形性的潜力。对径向截面和硬度分布的分析揭示了热处理的积极影响,但也指出了由于轨道成形中材料流动的特征而产生的影响的几何依赖性。
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Influence of a local short-term heat treatment on the formability of orbital formed functional components

Conventional processes like shearing dispose a lack in efficiency and formability to manufacture functional components with a high geometric variety. A possibility to allow the efficient and sustainable manufacturing is the application of innovative forming operations like orbital forming. Thus, a strain-hardened component with a load-adapted thickness profile can be manufactured in a single-stage process. Thereby, the control of the material flow could be identified as major challenge due to the three-dimensional stress and strain state. In order to reduce the parts weight and simultaneously guarantee the same level of performance, conventional steel is substituted by lightweight materials such as precipitation hardenable aluminum alloys. However, new challenges arise due to the reduced formability of aluminum compared to conventional steel. In recent research, the potential of a short-term heat treatment to enlarge the formability could be shown. The presented process locally reduces the materials strength, thus allowing a control of the material flow by the interaction between softened areas and areas, which offer the initial conditions. In this contribution, the influence on the formability of orbital formed components manufactured out of the precipitation hardenable aluminum alloy EN AW 6016 by a local short-term heat treatment is investigated. Different geometry-based heat treatment layouts are applied in order to maximize the thickening on different radial positions. The potential to enhance the formability is evaluated by comparing geometrical and mechanical properties of the components manufactured in the conventional process route and with a previous heat treatment. The analysis of radial cross-sections and the hardness distribution reveals the positive influence of the heat treatment but also points out the geometrical dependency of the effect due to the characteristic material flow in orbital forming.

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