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Materials Design for Joinable, High Performance Aluminum Alloys.

机译:可连接的高性能铝合金的材料设计。

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摘要

An aluminum alloy compatible with friction stir welding is designed for automotive and aerospace structural applications. Current weldable automotive aluminum alloys do not possess the necessary strength to meet safety standards and therefore are not able to replace steel in the automotive body. Significant weight savings could be achieved if steel components are replaced with aluminum. Current aerospace alloys are not weldable, requiring machining of large pieces that are then riveted together. If an aerospace alloy could be friction stir welded, smaller pieces could be welded, reducing material waste.;Using a systems approach for materials design, property goals are set from performance objectives. From previous research and computational predictions, a structure is designed for a prototype alloy containing dynamic precipitates to readily dissolve and re-precipitate and high stability precipitates to resist dissolution and coarsening in the weld region. It is found that a Ag modified Al-3.9Mg-0.04Cu (at. %) alloy enhanced the rate and magnitude of hardening during ageing, both beneficial effects for dynamic precipitation. In the same alloy, ageing at 350°C results in hardening from Al 3(Sc,Zr) precipitates. Efforts to effectively precipitate both populations simultaneously are unsuccessful. The Al3(Sc,Zr) precipitation hardened prototype is friction stir processed and no weak zones are found in the weld hardness profile. An aerospace alloy design is proposed, utilizing the dual precipitate structure shown in the prototype.;The automotive alloy is designed using a basic strength model with parameters determined from the initial prototype alloy analysis. After ageing to different conditions, the alloy is put through a simulated heat affected zone thermal cycle with a computer controlled induction heater. The aged samples lose hardness from the weld cycle but recover hardness from a post weld heat treatment. Atom probe tomography and transmission electron microscopy are used to characterize the composition, size, and phase fraction evolution for the automotive alloy strengthening precipitates. It is determined that the dominant precipitate at peak hardness is a metastable T' phase.;The automotive alloy is friction stir processed and found to lose hardness in the heat affected zones surrounding the nugget. A post weld heat treatment nearly recovers the heat affected zones to base hardness. The post weld heat treatment is compatible with the current automotive paint bake step, showing design for processability. Tensile tests confirm the base alloy strength meets the automotive strength goal.
机译:与摩擦搅拌焊接兼容的铝合金设计用于汽车和航空航天结构应用。当前的可焊接汽车铝合金不具有满足安全标准所需的强度,因此不能替代汽车车身中的钢。如果将钢部件替换为铝,则可以大大减轻重量。当前的航空航天合金不可焊接,需要加工大块然后铆接在一起。如果可以将航天合金进行摩擦搅拌焊接,则可以焊接较小的零件,从而减少材料浪费。使用材料设计的系统方法,可以根据性能目标确定性能目标。根据先前的研究和计算预测,为原型合金设计了一种结构,该合金包含易于熔解和再沉淀的动态析出物,以及高稳定性的析出物以抵抗焊接区域的溶解和粗化。发现Ag改性的Al-3.9Mg-0.04Cu(原子%)合金提高了时效过程中硬化的速率和强度,这对动态沉淀都是有益的。在同一合金中,在350°C时效会导致Al 3(Sc,Zr)沉淀物硬化。同时有效地使两个种群沉淀的努力均未成功。 Al3(Sc,Zr)沉淀硬化的原型经过摩擦搅拌处理,在焊接硬度分布图中未发现薄弱区域。提出了一种利用原型中所示的双析出物结构的航空航天合金设计。汽车合金是使用基本强度模型设计的,其参数是从初始原型合金分析中确定的。老化至不同条件后,用计算机控制的感应加热器将合金置于模拟的热影响区热循环中。老化的样品在焊接循环中会失去硬度,但在焊接后热处理后会恢复硬度。原子探针层析成像和透射电子显微镜用于表征汽车合金强化沉淀物的组成,尺寸和相分数演变。确定了在峰值硬度处的主要沉淀是亚稳态的T'相。汽车合金经过摩擦搅拌处理,发现在熔核周围的热影响区中失去硬度。焊后热处理几乎将受热影响的区域恢复到基本硬度。焊后热处理与当前的汽车烤漆步骤兼容,显示出可加工性设计。拉伸测试证实基础合金强度符合汽车强度目标。

著录项

  • 作者

    Glamm, Ryan James.;

  • 作者单位

    Northwestern University.;

  • 授予单位 Northwestern University.;
  • 学科 Nanotechnology.;Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2011
  • 页码 176 p.
  • 总页数 176
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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