Further Developments in Nuclear Pressure Vessel Manufacture Using the Hot Isostatic Pressing Process and Thick-Section Electron Beam Welding

T. Warner, J. Sulley, P. Wallace, D. Stewart, G. Jones, D. Thatcher
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These benefits would include cost savings, lead-time reductions, an increase in the material quality, and improved inspectability of the as-manufactured material. TSEBW offers the opportunity to dramatically reduce vessel section welding time, and, as no filler material is used, the potential to have a weld microstructure very similar to the parent material, thus providing the opportunity to eliminate through-life vessel weld inspections to reduce plant in-service costs. Production cost and timescale reductions are of particular interest with large vessel manufacture being a most significant contributor to the overall cost and manufacturing time of primary nuclear plant; this against a backdrop of the industry striving to drive down the cost of nuclear power generation in order to ensure viability with other forms of power generation.\n Applying the HIP process to LAS materials presents particular challenges due to the propensity for oxygen pick-up during the powder manufacturing stage, or in subsequent filling and processing operations. 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Of note is the production of a Small Vessel Demonstrator, which, to the best of Rolls-Royce’s knowledge, is the first of a kind HIPed, TSEB welded, LAS, high integrity pressure vessel with integral cladding. Achieving integral cladding by the HIP process has the potential to provide significant cost and time savings by deleting time consuming fusion techniques and machining operations. A Large Vessel Demonstrator section has also been manufactured and successfully EB welded.\n The paper concludes that although meeting material property specification requirements, further work is required to improve the Charpy impact toughness of HIPed LAS material to achieve similar values to the forged equivalent. 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Abstract

Hot Isostatic Pressing (HIPing) – Powder Metallurgy has been used by Rolls-Royce to successfully manufacture nuclear pressure boundary components such as valves, piping, and pump casings; the majority of these components being manufactured in stainless steels, typically 316L. Rolls-Royce has pioneered the use of this technology in the nuclear field in order to provide cost and lead-time reductions. Rolls-Royce considers there to be significant potential benefits in applying the HIP process, together with Thick Section Electron Beam Welding (TSEBW), to the manufacture of large Low Alloy Steel (LAS) pressure vessels. These benefits would include cost savings, lead-time reductions, an increase in the material quality, and improved inspectability of the as-manufactured material. TSEBW offers the opportunity to dramatically reduce vessel section welding time, and, as no filler material is used, the potential to have a weld microstructure very similar to the parent material, thus providing the opportunity to eliminate through-life vessel weld inspections to reduce plant in-service costs. Production cost and timescale reductions are of particular interest with large vessel manufacture being a most significant contributor to the overall cost and manufacturing time of primary nuclear plant; this against a backdrop of the industry striving to drive down the cost of nuclear power generation in order to ensure viability with other forms of power generation. Applying the HIP process to LAS materials presents particular challenges due to the propensity for oxygen pick-up during the powder manufacturing stage, or in subsequent filling and processing operations. The potential for oxide formation on powder particles presents a risk to the material properties being adversely affected, particularly a material’s fracture toughness, which is critical to the structural integrity of nuclear pressure vessels. Previously, Rolls-Royce has shown it is possible to achieve enhanced tensile properties compared to wrought equivalent material, and to meet the specified Charpy impact toughness requirements. However, under certain conditions, i.e. relatively high oxygen levels in the HIP powder, the Charpy impact toughness was found to be 66% of typical wrought material at room temperature. This paper presents further material testing work conducted by Rolls-Royce to assess any improvement in material property results when the potential for oxygen ingress in the process is reduced. This paper also presents the latest HIP vessel demonstrator work that Rolls-Royce has conducted to assess the viability of the technology to achieve vessel geometries. Of note is the production of a Small Vessel Demonstrator, which, to the best of Rolls-Royce’s knowledge, is the first of a kind HIPed, TSEB welded, LAS, high integrity pressure vessel with integral cladding. Achieving integral cladding by the HIP process has the potential to provide significant cost and time savings by deleting time consuming fusion techniques and machining operations. A Large Vessel Demonstrator section has also been manufactured and successfully EB welded. The paper concludes that although meeting material property specification requirements, further work is required to improve the Charpy impact toughness of HIPed LAS material to achieve similar values to the forged equivalent. Although some improvement in toughness was observed at sub-zero temperatures by reducing the potential for oxygen pick-up in the powder filling process, improvements might be best achieved by focusing on reducing the initial oxygen content of the powder stock, i.e. striving for oxygen levels far lower than 200ppm. It also concludes, that although achieving large-scale vessel geometry is considered feasible, further development work is required in order to achieve near net/net shape vessel geometry to incorporate integral cladding and/or minimising general planar machining operations. This is in the field of preventing geometric imperfections by ensuring a high powder packing density by focusing on the HIP can powder filling process and the powder morphology and particle size distribution, and also possibly can design/manufacture. EB welding has, in the main, been successful, but further work is required to optimise the EB parameters, particularly with beam retraction to prevent the generation of defects.
热等静压工艺和厚截面电子束焊接在核压力容器制造中的进一步发展
热等静压(HIPing) -粉末冶金已被罗尔斯·罗伊斯公司成功地用于制造核压力边界部件,如阀门、管道和泵壳;这些部件大多是用不锈钢制造的,通常是316L。罗尔斯·罗伊斯公司率先在核领域使用这项技术,以降低成本和交货时间。罗尔斯·罗伊斯公司认为,将HIP工艺与厚截面电子束焊接(TSEBW)一起应用于制造大型低合金钢(LAS)压力容器具有显著的潜在效益。这些好处包括节省成本,缩短交货时间,提高材料质量,提高成品材料的可检验性。TSEBW提供了大幅缩短容器截面焊接时间的机会,并且由于不使用填充材料,焊缝微观结构可能与母材非常相似,因此有机会消除整个容器的焊接检查,从而降低工厂在役成本。生产成本和时间尺度的降低是特别感兴趣的,因为大型容器制造是主要核电站总成本和制造时间的最重要贡献者;在此背景下,业界正努力降低核能发电的成本,以确保与其他形式的发电相适应。由于在粉末制造阶段或随后的填充和加工操作中有吸氧的倾向,将HIP工艺应用于LAS材料提出了特殊的挑战。粉末颗粒上形成氧化物的可能性会对材料性能产生不利影响,特别是材料的断裂韧性,这对核压力容器的结构完整性至关重要。此前,罗尔斯·罗伊斯公司已经证明,与变形等效材料相比,它有可能实现增强的拉伸性能,并满足规定的夏比冲击韧性要求。然而,在某些条件下,即在相对较高的氧含量下,在室温下,发现夏比冲击韧性是典型锻造材料的66%。本文介绍了Rolls-Royce进行的进一步材料测试工作,以评估在降低过程中氧气进入的可能性时材料性能结果的任何改进。本文还介绍了Rolls-Royce公司最新的HIP船舶演示工作,以评估该技术实现船舶几何形状的可行性。值得注意的是小型容器演示器的生产,据罗尔斯·罗伊斯所知,这是第一个具有完整包层的HIPed, TSEB焊接,LAS的高完整性压力容器。通过HIP工艺实现整体包覆,可以省去耗时的融合技术和加工操作,从而节省大量成本和时间。大型船舶演示部分也已制造并成功地进行了电子束焊接。本文认为,虽然满足材料性能规范要求,但仍需进一步提高HIPed LAS材料的夏比冲击韧性,以达到与锻造等效材料相近的值。虽然在零度以下的温度下,通过减少粉末填充过程中氧气吸收的可能性,可以观察到韧性的一些改善,但改善的最佳方法可能是专注于降低粉末原料的初始氧含量,即努力使氧含量远低于200ppm。研究还得出结论,尽管实现大型容器几何形状被认为是可行的,但为了实现接近净/净形状的容器几何形状,以整合整体包层和/或最小化一般平面加工操作,还需要进一步的开发工作。这是在通过关注HIP罐粉末填充过程和粉末形态和粒度分布,确保高粉末包装密度来防止几何缺陷的领域,也可能是设计/制造。总的来说,电子束焊接是成功的,但需要进一步优化电子束参数,特别是电子束缩回,以防止产生缺陷。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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