增材制造Rene的过程机械加工

Will James, S. Ganguly, G. Pardal
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引用次数: 0

摘要

在开发用于国防应用的抗蠕变合金的线+电弧增材制造(WAAM)工艺中,结构由镍基高温合金Rene 41 (RE41)构建。对添加剂制造合金的性能进行了分析,包括在高速飞行环境中使用的组件,其中外部结构可以达到高达1000 K的使用温度。作为一个单一使用的系统,飞行时间相对较短,小于1小时,组件将受到高度压力,以尽量减少结构质量。在本文中,采用等离子体转移电弧工艺沉积了三个壁结构,在沉积后,每一层都是通过机器锤击直接机械加工的。在恒定的冲击频率下,对每个壁结构采用三种不同的强化刀行程速度。为了了解最有效的冷加工参数,对样品进行了时效处理后的力学性能和显微组织特征测试和分析。样品在室温下进行测试,并与未经加工的热处理AM材料的结果和从文献综述中获得的变形数据进行比较。热处理后的材料呈现出典型的枝晶组织和大柱状晶粒,而喷丸后的材料呈现出明显不同的晶粒组织。两种条件下形成的相没有明显的差异。力学测试结果表明,与非加工强度相比,该材料的强度有了显著提高。中间和缓慢的喷丸速度非常有效,达到的UTS和YS结果接近锻压合金,与非加工材料相比,弹性模量的增加相似。然而,更快的喷丸速度在使材料恢复变形强度方面效果较差。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
In-Process Mechanical Working of Additive Manufactured Rene 41
In developing the wire + arc additive manufacturing (WAAM) process for creep resistant alloys for defence applications, structures were built from nickel-based superalloy Rene 41 (RE41). The performance of the additive manufactured alloy was analysed for applications including components used in high-speed flight environments, where external structures could reach service temperatures of up to 1000 K. As a single use system with relatively short flight times of < 1 hour, components will be highly stressed to minimise structural mass. In this paper, three wall structures were deposited using a plasma transferred arc process, in a layer-by-layer manner where each layer was mechanically worked by machine hammer peening directly after deposition. With a constant impact frequency, three different travel speeds for the peening tool were used for each wall structure. To understand the most effective cold working parameters, samples were tested and analysed for their mechanical properties and microstructural characteristics after aging treatment. Samples were tested at room temperature and compared with results of both non-worked heat-treated AM material and wrought data obtained from literature review. Heat-treated only material showed a typical dendritic structure with large columnar grains, and peened material showed a significantly different grain structure. No noticeable difference was observed in the formed phases between the two conditions. Mechanical testing showed promising results with a significant improvement over the non-worked strength. Intermediate and slow peening speeds were very effective, achieving UTS and YS results close to that of the wrought alloy, with a similar increase in the elastic modulus compared to non-worked material. However, faster peening speeds were less effective at returning the material to wrought strength.
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