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Mechanical performance of laser powder bed fused Ti-6Al-4V: The influence of filter condition and part location 激光粉末床熔融 Ti-6Al-4V 的机械性能:过滤条件和零件位置的影响
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-11-08 DOI: 10.1016/j.addlet.2024.100255
Mohammad Salman Yasin , Kevin Stonaker , Shuai Shao , Nima Shamsaei
Deteriorated filter condition in laser powder bed fusion (L-PBF) systems may negatively impact shield gas flow, causing inadequate spatter particle/plume removal, leading to laser beam attenuation and reduction in melt pool depth, and potentially causing more frequent formation of volumetric defects. This work investigated the effects of filter condition and part location on the micro-/defect-structure and mechanical behavior, including tensile and fatigue, of Ti-6Al-4V parts fabricated by L-PBF. Interestingly, within the manufacturer recommended service intervals, no specific effect of filter condition could be observed on the micro-/defect-structure or the mechanical behavior of the fabricated parts. However, the parts’ defect-structures were affected by their location, with ones located near the center of the build plate having less porosity than the ones located away. Although these defects did not affect the tensile properties, they frequently observed to initiate fatigue cracks (the critical defects sizes were often in the range of a few tens of micrometers). Therefore, their sensitivity to location resulted in the location dependence of the fatigue behavior.
激光粉末床熔融(L-PBF)系统中的过滤器条件恶化可能会对保护气流产生负面影响,导致飞溅颗粒/飞溅物去除不充分,从而导致激光束衰减和熔池深度降低,并可能导致更频繁地形成体积缺陷。这项工作研究了过滤器条件和零件位置对 L-PBF 制造的 Ti-6Al-4V 零件的微观/缺陷结构和机械性能(包括拉伸和疲劳)的影响。有趣的是,在制造商推荐的维护周期内,无法观察到过滤器条件对制造零件的微观/缺陷结构或机械性能的具体影响。不过,部件的缺陷结构会受到其位置的影响,靠近制造板中心的缺陷比远离制造板中心的缺陷孔隙率要低。虽然这些缺陷不会影响拉伸性能,但它们经常会引发疲劳裂纹(临界缺陷尺寸通常在几十微米范围内)。因此,它们对位置的敏感性导致了疲劳行为的位置依赖性。
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引用次数: 0
Area-based composition predictions of materials fabricated using simultaneous wire-powder-directed energy deposition 利用同步线-粉末定向能沉积法制造材料的基于面积的成分预测
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-11-04 DOI: 10.1016/j.addlet.2024.100254
Scott C. Bozeman, O. Burkan Isgor, Julie D. Tucker
Functionally graded materials are an emergent method for designing components with programmable site-specific material properties. These materials are typically fabricated using metal additive manufacturing tools by simultaneously feeding multiple wire and/or powder feedstocks at various rates to achieve spatial composition change. The wire-powder-directed energy deposition (WP-DED) technique is of particular interest for many functionally graded material applications by balancing the low raw materials cost of wire with the high resolution of powder. However, feeding wire and powder are inherently different processes since all extruded wire enters the melt pool, while much of the blown powder is scattered, which makes determining the composition of the build challenging. In this study, we devise a simple area-based measurement method for estimating the composition of WP-DED structures. WP-DED single beads are printed using 309L stainless steel wire and commercially pure Fe powder at five wire feed rates (0.5, 0.75, 1.00, 1.25, 1.50 mm/mm) and five powder feed rates (2, 4, 6, 8, 10 rpm). Characteristic defects including interface gaps and macrosegregation (lack of mixing) tendencies are examined. High powder feed rates (8, 10 rpm) result in interface gaps at all wire feed rates, but smooth deposition and complete mixing is achieved at low powder feed rates, particularly with lower wire feed rates as well. The area-based composition measurement method is within ±20% of energy dispersive x-ray spectroscopy measurements for all samples, showing its effectiveness as a rapid composition estimate for WP-DED materials development.
功能分级材料是设计具有可编程特定部位材料特性的组件的一种新兴方法。这些材料通常使用金属增材制造工具制造,方法是以不同的速率同时馈入多种金属丝和/或粉末原料,以实现空间成分变化。线材-粉末定向能量沉积(WP-DED)技术兼顾了线材的低原材料成本和粉末的高分辨率,因此在许多功能分级材料应用中特别受关注。然而,线材和粉末的喂料过程本质上是不同的,因为所有挤出的线材都进入熔池,而大部分吹出的粉末都是散落的,这就给确定构建材料的成分带来了挑战。在本研究中,我们设计了一种简单的基于面积的测量方法,用于估算 WP-DED 结构的成分。使用 309L 不锈钢丝和市售纯铁粉,以五种金属丝进给速率(0.5、0.75、1.00、1.25、1.50 mm/mm)和五种粉末进给速率(2、4、6、8、10 rpm)打印 WP-DED 单珠。对包括界面间隙和大偏析(缺乏混合)倾向在内的特征性缺陷进行了研究。高粉末进给率(8、10 rpm)会导致所有线材进给率下的界面间隙,但在低粉末进给率下,尤其是在较低线材进给率下,可实现平稳沉积和完全混合。对所有样品而言,基于面积的成分测量方法与能量色散 X 射线光谱测量结果的误差均在±20%以内,这表明该方法可有效地快速评估 WP-DED 材料的成分。
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引用次数: 0
Modelling process monitoring data in laser powder bed fusion: A pragmatic route to additive manufacturing quality assurance 激光粉末床熔融过程监控数据建模:快速成型制造质量保证的实用途径
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-10-29 DOI: 10.1016/j.addlet.2024.100252
Luke N. Carter , Victor M. Villapún , James Andrews , Thomas R.B. Grandjean , John Dardis , Sophie C. Cox
Quality assurance remains a significant challenge for laser powder bed fusion and metal additive manufacturing. Despite system manufacturers offering process monitoring as a possible solution, datasets are large and cumbersome with practical use limited without direct comparative data. Model datasets would enable individual build validation, highlight deviations, and facilitate intelligent build planning whereby challenging features or build strategies could be pre-emptively assessed.
Herein a pragmatic approach has been developed to model process monitoring data from a commercial system using a relatively simple algorithm. Using a heuristic method, the algorithm response has been fitted to an experimental dataset to derive governing constants and their relationship to key process parameters. Predictability of constants and model fit has been shown to improve with increasing line energy up to a maximum R2=0.8. Algorithm variable trends, supported by corresponding sensitivity analysis, identified two different behavioural regimes. Under low linear energy density (<0.2J/mm) the cumulative spacetime proximity time-weight variable shows a low sensitivity index, characterised by a flat model response reflected in the experimental data. At higher energies (≥0.2J/mm) algorithm variables become more predictable, reflected in stabilising sensitivity indices, as measurements adopt a form characteristic of the cumulative spacetime proximity function.
Effectiveness has been demonstrated through presentation of experimental and model data. Refining the methodology to accommodate noise, geometry, and systematic behaviours are identified as key steps to future development. This feasibility study has laid the groundwork for a generalised predictive tool, capable of realising the quality assurance ambitions promised by laser powder-bed fusion process monitoring.
质量保证仍然是激光粉末床熔融和金属增材制造面临的重大挑战。尽管系统制造商提供了过程监控作为可能的解决方案,但数据集庞大而繁琐,在没有直接比较数据的情况下,实际用途有限。模型数据集可对单个构建进行验证,突出偏差,并促进智能构建规划,从而对具有挑战性的特征或构建策略进行预先评估。在此,我们开发了一种实用方法,使用相对简单的算法对商用系统的过程监控数据进行建模。采用启发式方法,将算法响应与实验数据集进行拟合,从而得出控制常数及其与关键工艺参数的关系。结果表明,常数和模型拟合的可预测性随着线能量的增加而提高,最大 R2=0.8。在相应的敏感性分析支持下,算法变量趋势确定了两种不同的行为模式。在低线性能量密度(<0.2J/mm)条件下,累积时空临近时间权重变量显示出较低的灵敏度指数,其特点是实验数据中反映的模型响应平缓。在能量较高(≥0.2J/mm)时,算法变量变得更可预测,反映在稳定的灵敏度指数上,因为测量采用了累积时空接近函数的特征形式。改进方法以适应噪声、几何和系统行为被确定为未来发展的关键步骤。这项可行性研究为通用预测工具奠定了基础,它能够实现激光粉末床熔融过程监控所承诺的质量保证目标。
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引用次数: 0
Drop-on-demand 3D printing of programable magnetic composites for soft robotics 用于软机器人的可编程磁性复合材料的按需滴落三维打印技术
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-10-28 DOI: 10.1016/j.addlet.2024.100250
Anil Bastola , Luke Parry , Robyn Worsley , Nisar Ahmed , Edward Lester , Richard Hague , Christopher Tuck
Soft robotics have become increasingly popular as a versatile alternative to traditional robotics. Magnetic composite materials, which respond to external magnetic fields, have attracted significant interest in this field due to their programmable two-way actuation and shape-morphing capabilities. Additive manufacturing (AM)/3D printing allows for the incorporation of different functional composite materials to create active components for soft robotics. However, current AM methods have limitations, especially when it comes to printing smart composite materials with high functional material content. This is a key requirement for enhancing responsiveness to external stimuli. Commonly used AM methods for smart magnetic composites, such as direct ink writing (DIW), confront challenges in achieving discontinuous printing, and enabling multi-material control at the voxel level, while some AM techniques are not suitable for producing composite materials. To address these limitations, we employed high-viscosity drop-on-demand (DoD) jetting and developed programmable magnetic composites filled with micron-sized hard magnetic particles. This method bridges the gap between conventional ink-jetting and DIW, which require printing inks with viscosities at opposite ends of the spectrum. This high-viscosity DoD jetting enables continuous, discontinuous, and non-contact printing, making it a versatile and effective method for 3D printing functional magnetic composites even with micron-sized fillers. Furthermore, we demonstrated stable magnetic domain programming and two-way shape-morphing actuations of printed structures for soft robotics. In summary, our work highlights high-viscosity DoD jetting as a promising method for printing functional magnetic composites and other similar materials for a wide range of applications.
作为传统机器人技术的多功能替代品,软机器人技术越来越受欢迎。磁性复合材料可对外部磁场做出反应,由于其可编程的双向驱动和形状变形能力,在这一领域引起了极大的兴趣。增材制造(AM)/三维打印技术可以将不同的功能复合材料结合在一起,为软体机器人制造有源元件。然而,目前的增材制造方法存在局限性,尤其是在打印高功能材料含量的智能复合材料时。这是提高对外部刺激响应能力的关键要求。用于智能磁性复合材料的常用 AM 方法(如直接墨水写入(DIW))在实现不连续打印和在体素级实现多材料控制方面面临挑战,而一些 AM 技术则不适合生产复合材料。为了解决这些限制,我们采用了高粘度按需滴墨(DoD)喷射技术,并开发出了填充微米级硬磁性颗粒的可编程磁性复合材料。这种方法弥补了传统喷墨和按需滴墨之间的差距,因为传统喷墨和按需滴墨需要打印粘度处于光谱两端的墨水。这种高粘度 DoD 喷射可实现连续、不连续和非接触式打印,使其成为一种通用而有效的 3D 打印功能性磁性复合材料的方法,即使使用微米级填料也不例外。此外,我们还展示了用于软机器人的稳定磁域编程和打印结构的双向形状变形执行。总之,我们的工作凸显了高粘度 DoD 喷射是打印功能性磁性复合材料和其他类似材料的一种前景广阔的方法。
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引用次数: 0
In-situ heating TEM observation of solidification cell evolutions in an Al-Fe alloy built by laser-powder bed fusion 原位加热 TEM 观察激光粉末床熔融法制造的 Al-Fe 合金中凝固单元的演变过程
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-10-28 DOI: 10.1016/j.addlet.2024.100251
Ji-Yun Wang , Verner Soh , Pei Wang , Tzu-Ching Tsao , Ming-Wen Chu , Ming-Hao Lee , Zhongji Sun , Shao-Pu Tsai
Cellular structures (i.e., solidification cells) are a unique feature within alloys fabricated through rapid solidification, such as laser-powder bed fusion (L-PBF). Ever since the report of these structures’ beneficial effects on the material's mechanical properties, numerous studies have been devoted to the understanding of their formation mechanisms. Yet, the integrity and stability of the cellular structures are often less investigated, despite their significance on property interpretation and evolution. In this work, a stepwise in-situ heating transmission electron microscopy (TEM) experiment was performed on the exemplary LPBF-fabricated AlFeSiMoZr alloy. A critical threshold of 325 °C was identified, beyond which the cellular structures start to decompose in conjunction with precipitate coarsening. Preferred precipitate nucleation sites and their subsequent coarsening kinetics were determined and presented. Nanometer-sized crystalline embryos (3.81 ± 0.66 nm) were discovered within the cellular structure boundaries in their as-built condition, offering new insights on the precipitate formation and evolution at elevated temperatures.
晶胞结构(即凝固晶胞)是通过激光粉末床熔融(L-PBF)等快速凝固技术制造合金的一个独特特征。自从这些结构对材料的机械性能产生有利影响的报道发表以来,许多研究都致力于了解它们的形成机制。然而,细胞结构的完整性和稳定性往往研究较少,尽管它们对性能解释和演变具有重要意义。在这项工作中,对 LPBF 制成的 AlFeSiMoZr 合金进行了分步原位加热透射电子显微镜(TEM)实验。实验确定了一个临界点,即 325 °C,当温度超过这个临界点时,蜂窝结构开始分解,同时析出物也变得粗大。确定并展示了首选沉淀成核点及其随后的粗化动力学。在细胞结构边界内发现了纳米大小的结晶胚(3.81 ± 0.66 nm),为高温下沉淀物的形成和演变提供了新的见解。
{"title":"In-situ heating TEM observation of solidification cell evolutions in an Al-Fe alloy built by laser-powder bed fusion","authors":"Ji-Yun Wang ,&nbsp;Verner Soh ,&nbsp;Pei Wang ,&nbsp;Tzu-Ching Tsao ,&nbsp;Ming-Wen Chu ,&nbsp;Ming-Hao Lee ,&nbsp;Zhongji Sun ,&nbsp;Shao-Pu Tsai","doi":"10.1016/j.addlet.2024.100251","DOIUrl":"10.1016/j.addlet.2024.100251","url":null,"abstract":"<div><div>Cellular structures (i.e., solidification cells) are a unique feature within alloys fabricated through rapid solidification, such as laser-powder bed fusion (L-PBF). Ever since the report of these structures’ beneficial effects on the material's mechanical properties, numerous studies have been devoted to the understanding of their formation mechanisms. Yet, the integrity and stability of the cellular structures are often less investigated, despite their significance on property interpretation and evolution. In this work, a stepwise <em>in-situ</em> heating transmission electron microscopy (TEM) experiment was performed on the exemplary LPBF-fabricated AlFeSiMoZr alloy. A critical threshold of 325 °C was identified, beyond which the cellular structures start to decompose in conjunction with precipitate coarsening. Preferred precipitate nucleation sites and their subsequent coarsening kinetics were determined and presented. Nanometer-sized crystalline embryos (3.81 ± 0.66 nm) were discovered within the cellular structure boundaries in their as-built condition, offering new insights on the precipitate formation and evolution at elevated temperatures.</div></div>","PeriodicalId":72068,"journal":{"name":"Additive manufacturing letters","volume":"11 ","pages":"Article 100251"},"PeriodicalIF":4.2,"publicationDate":"2024-10-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"142578222","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
A non-melting additive approach to structural repair of aluminum aircraft fastener holes 铝制飞机紧固件孔结构修复的非熔化添加剂方法
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-10-23 DOI: 10.1016/j.addlet.2024.100249
R. Joey Griffiths , David Garcia , Greg D. Hahn , Jim Lua , Nam Phan , Hang Z. Yu
The damage to fastener holes in aerospace aluminum structures presents significant challenges for aircraft durability, and conventional bushing methods for repairing oversized holes often fall short due to the lack of metallurgical bonding and limited edge distance availability. This study investigates additive friction stir deposition, a non-melting additive process, as a viable alternative for the structural repair of aerospace fastener holes. The repair process, demonstrated on AA7050 (Al-Zn-Mg-Cu-Zr) hole structures, involves filling oversized holes with new material and machining to restore the original hole size. The repaired hole coupons are defect-free and exhibit good fatigue performance under fully reversed tension-compression loading (R = -1). At a nominal stress amplitude of 123.5 MPa, the average number of cycles to failure is 12,666 for unrepaired baseline coupons and 17,372 for effectively repaired coupons. Restoring complex geometries without compromising fatigue performance has been difficult in aerospace applications; this study marks the first demonstration of additive repair that consistently outperforms the unrepaired baseline coupons. Notably, the result is achieved through a low-energy, cost-effective solution without the need for post-repair heat treatment. Except for a few outliers, the post-repair fatigue performance generally remains inferior to that of undamaged, pristine coupons, likely due to precipitate evolution in AA7050 caused by the thermomechanical processing nature of additive friction stir deposition. This evolution weakens the repair region and the adjacent base material, leading to faster crack initiation and growth compared to the properly aged base material, AA7050-T7451.
航空航天铝结构中紧固件孔的损坏对飞机的耐久性提出了重大挑战,而用于修复过大孔的传统衬套方法往往因缺乏冶金结合和有限的边缘距离而无法达到预期效果。本研究调查了添加剂搅拌摩擦沉积(一种非熔化添加剂工艺),将其作为航空航天紧固件孔结构修复的可行替代方法。该修复工艺在 AA7050(Al-Zn-Mg-Cu-Zr)孔结构上进行了演示,包括用新材料填充过大的孔并进行加工以恢复孔的原始尺寸。修复后的孔洞试样无缺陷,在完全反向拉伸-压缩加载(R = -1)条件下表现出良好的疲劳性能。在 123.5 兆帕的额定应力幅值下,未修复基线试样的平均失效循环次数为 12,666 次,有效修复试样的平均失效循环次数为 17,372 次。在航空航天应用中,很难在不影响疲劳性能的情况下修复复杂的几何结构;这项研究首次证明了添加剂修复的效果始终优于未修复的基线试样。值得注意的是,这一成果是通过低能耗、高成本效益的解决方案实现的,无需进行修复后热处理。除少数异常值外,修复后的疲劳性能总体上仍低于未损坏的原始试样,这可能是由于添加剂搅拌摩擦沉积的热机械加工性质导致 AA7050 中的沉淀演变。与适当老化的 AA7050-T7451 基体材料相比,这种演变削弱了修复区域和邻近基体材料的强度,导致裂纹的产生和增长速度加快。
{"title":"A non-melting additive approach to structural repair of aluminum aircraft fastener holes","authors":"R. Joey Griffiths ,&nbsp;David Garcia ,&nbsp;Greg D. Hahn ,&nbsp;Jim Lua ,&nbsp;Nam Phan ,&nbsp;Hang Z. Yu","doi":"10.1016/j.addlet.2024.100249","DOIUrl":"10.1016/j.addlet.2024.100249","url":null,"abstract":"<div><div>The damage to fastener holes in aerospace aluminum structures presents significant challenges for aircraft durability, and conventional bushing methods for repairing oversized holes often fall short due to the lack of metallurgical bonding and limited edge distance availability. This study investigates additive friction stir deposition, a non-melting additive process, as a viable alternative for the structural repair of aerospace fastener holes. The repair process, demonstrated on AA7050 (Al-Zn-Mg-Cu-Zr) hole structures, involves filling oversized holes with new material and machining to restore the original hole size. The repaired hole coupons are defect-free and exhibit good fatigue performance under fully reversed tension-compression loading (<em>R</em> = -1). At a nominal stress amplitude of 123.5 MPa, the average number of cycles to failure is 12,666 for unrepaired baseline coupons and 17,372 for effectively repaired coupons. Restoring complex geometries without compromising fatigue performance has been difficult in aerospace applications; this study marks the first demonstration of additive repair that consistently outperforms the unrepaired baseline coupons. Notably, the result is achieved through a low-energy, cost-effective solution without the need for post-repair heat treatment. Except for a few outliers, the post-repair fatigue performance generally remains inferior to that of undamaged, pristine coupons, likely due to precipitate evolution in AA7050 caused by the thermomechanical processing nature of additive friction stir deposition. This evolution weakens the repair region and the adjacent base material, leading to faster crack initiation and growth compared to the properly aged base material, AA7050-T7451.</div></div>","PeriodicalId":72068,"journal":{"name":"Additive manufacturing letters","volume":"11 ","pages":"Article 100249"},"PeriodicalIF":4.2,"publicationDate":"2024-10-23","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":null,"resultStr":null,"platform":"Semanticscholar","paperid":"142554068","PeriodicalName":null,"FirstCategoryId":null,"ListUrlMain":null,"RegionNum":0,"RegionCategory":"","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":"OA","EPubDate":null,"PubModel":null,"JCR":null,"JCRName":null,"Score":null,"Total":0}
引用次数: 0
Enabling tailored microstructures by hybrid directed energy deposition processing of a nickel-based superalloy 通过混合定向能沉积加工镍基超合金实现定制微结构
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-10-16 DOI: 10.1016/j.addlet.2024.100248
Clemens Johannes Müller , Klaus Büßenschütt , Alexander Schwedt , Johannes Henrich Schleifenbaum , Markus Sudmanns
The technological advances in additive manufacturing, particularly laser based directed energy deposition (DED), revolutionized the production of complex metal components. Despite this progress, the oriented heat flux and several reheating thermal cycles can induce a strongly textured microstructure, which induces an anisotropic mechanical behavior. In addition, considerable residual stresses typically require additional post-processing. Therefore, hybrid process chains for additive manufacturing (AM) are being developed, which aim at integrating conventional post-processing into the AM process. However, a detailed investigation of thermal and mechanical effects of such hybrid processes on the mechanical properties and their interrelation is lacking. In an experimental study, we explore the integration of thermal and mechanical processing steps within the DED process chain to locally tailor microstructures and mechanical properties. Through electron backscatter diffraction measurements, we demonstrate significant microstructural changes of DED-manufactured nickel-based superalloy samples using deep rolling and laser heat treatment. A mechanical surface deformation induces microstructural misorientation leading to an increase in hardness down to substantial depth of several hundred micrometers. Additionally, the targeted management of heat input during laser heat treatment results in different grain morphologies and sizes, affecting average microhardness within a significant depth. The results demonstrate the potential for microstructural tailoring using hybrid AM process chains, while a substantial sensitivity of the microstructure to thermal and mechanical load emphasizes the importance of a precise process control. This work provides an understanding of the process-microstructure-property relationship required for developing new process pathways in hybrid AM that integrate thermal and mechanical processes into DED manufacturing.
快速成型制造技术,特别是基于激光的定向能沉积(DED)技术的进步,彻底改变了复杂金属部件的生产。尽管取得了这一进步,但定向热通量和多次再加热热循环会导致微观结构产生强烈纹理,从而诱发各向异性的机械行为。此外,相当大的残余应力通常需要额外的后处理。因此,目前正在开发用于增材制造(AM)的混合工艺链,旨在将传统的后处理集成到增材制造工艺中。然而,目前还缺乏对这种混合工艺对机械性能的热效应和机械效应及其相互关系的详细研究。在一项实验研究中,我们探索了在 DED 工艺链中整合热加工和机械加工步骤,以局部定制微观结构和机械性能的方法。通过电子反向散射衍射测量,我们证明了使用深轧制和激光热处理的 DED 制造的镍基超合金样品发生了显著的微观结构变化。机械表面变形会引起微观结构错向,导致硬度增加,深度可达数百微米。此外,在激光热处理过程中对热输入进行有针对性的管理会产生不同的晶粒形态和尺寸,从而影响相当深度内的平均显微硬度。研究结果证明了利用混合 AM 工艺链定制微观结构的潜力,而微观结构对热负荷和机械负荷的高度敏感性则强调了精确工艺控制的重要性。这项工作让我们了解了在混合 AM 中开发新工艺途径所需的工艺-微结构-性能关系,这种新工艺途径将热工艺和机械工艺整合到了 DED 制造中。
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引用次数: 0
An integrated hybrid wire-arc directed energy deposition, friction stir processing, and milling system for multi-track, multi-layer part manufacturing 用于多轨道、多层零件制造的线弧定向能沉积、摩擦搅拌加工和铣削综合混合系统
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-10-11 DOI: 10.1016/j.addlet.2024.100247
Dinh Son Nguyen , Jie Song , Yao Fu , Albert C. To
Wire-based Directed Energy Deposition (DED) is a widely-used manufacturing method due to its high productivity and large part fabrication capability. Meanwhile, Friction Stir Processing (FSP) is a solid-state joining process that can modify microstructure and weld lightweight alloys. Additionally, wire-based DED printed parts need machining process to achieve the desired dimensional accuracy. To take advantage of all these three processes, this work proposes an integrated hybrid system by combining the wire-arc DED, FSP, and milling processes into a standalone system which can fabricate superior materials in a multi-track, multi-layer manner for the first time. The integrated system can improve dimensional accuracy and productivity by processing the workpiece without the need to move it between different systems. It is demonstrated that a 150 × 40 × 21 mm3 block of aluminum alloy AA5183 can be fabricated using the hybrid wire-DED/FSP/milling process from wire feedstock. Material characterization shows that the hybrid process is able to refine the grain size by two orders of magnitude to sub-micron scale, while eliminating all the pores and microcracks produced by the DED process. These enhancements result in significantly improved mechanical properties including Young's modulus (15 %), yield strength (161 %), ultimate strength (33 %), and hardness (55 %) without compromising ductility.
线基定向能沉积(DED)因其高生产率和大部件制造能力而成为一种广泛使用的制造方法。同时,摩擦搅拌加工(FSP)是一种固态连接工艺,可以改变微观结构并焊接轻质合金。此外,基于线材的 DED 印刷部件需要加工工艺来达到所需的尺寸精度。为了充分利用这三种工艺的优势,这项研究提出了一种集成混合系统,它将线弧 DED、FSP 和铣削工艺结合到一个独立的系统中,首次实现了以多轨道、多层次的方式制造优质材料。该集成系统无需在不同系统之间移动工件,即可进行加工,从而提高了尺寸精度和生产率。实验证明,使用线材-DED/FSP/铣削混合工艺,可以用线材原料制造出 150 × 40 × 21 mm3 的铝合金 AA5183 块。材料表征表明,混合工艺能将晶粒尺寸细化两个数量级,达到亚微米级,同时消除了 DED 工艺产生的所有孔隙和微裂纹。这些改进大大提高了机械性能,包括杨氏模量(15%)、屈服强度(161%)、极限强度(33%)和硬度(55%),同时不影响延展性。
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引用次数: 0
Effect of laser power during laser powder bed fusion on microstructure of joining interface between Tungsten and AISI 316L steel 激光粉末床熔融过程中的激光功率对钨和 AISI 316L 钢连接界面微观结构的影响
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-10-09 DOI: 10.1016/j.addlet.2024.100246
Seung-Hoon Lee , Ji-Hoe Koo , Omer Cakmak , Jung-Wook Cho
This study investigates the deposition of tungsten (W) onto a 316L steel substrate by laser powder bed fusion (L-PBF), to optimize process parameters and analyze the interface between W and 316L. To obtain high-density W structure (98.89%), the optimal laser power was 350 W, and scan speed was 500 mm/s, but these parameters cause significant dilution of W in the W-316L interface; as a result, Fe7W6 intermetallics form, despite L-PBF being a non-equilibrium solidification process. These intermetallics which are brittle could degrade joint strength. By reducing laser power below 250 W, the dilution of W can be mitigated, and potentially minimize formation of intermetallics and increase joint stability for advanced manufacturing applications.
本研究采用激光粉末床熔融(L-PBF)技术在 316L 钢基底上沉积钨(W),以优化工艺参数并分析 W 与 316L 之间的界面。为获得高密度的钨结构(98.89%),最佳激光功率为 350 W,扫描速度为 500 mm/s,但这些参数会导致 W-316L 界面中的钨被大量稀释;结果,尽管 L-PBF 是一种非平衡凝固过程,但仍形成了 Fe7W6 金属间化合物。这些金属间化合物很脆,会降低连接强度。通过将激光功率降至 250 W 以下,可减轻 W 的稀释,并有可能最大限度地减少金属间化合物的形成,提高先进制造应用中的接合稳定性。
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引用次数: 0
Preparation of continuous carbon fiber reinforced PA6 prepreg filaments with high fiber volume fraction 制备高纤维体积分数的连续碳纤维增强 PA6 预浸丝
IF 4.2 Q2 ENGINEERING, MANUFACTURING Pub Date : 2024-10-02 DOI: 10.1016/j.addlet.2024.100245
Ming Zhang , Zhonggang Sun , Yingbing Liang , Yanhua Guo , Guoqing Dai , Keyuan Wei , Ming Li , Xiping Li , Igor V. Alexandrov
High-performance continuous carbon fiber prepreg filaments have been a research hotspot in the field of additive manufacturing in recent years, and are considered to be an effective option for improving the mechanical strength of thermoplastic composite parts. However, the effect of fiber volume fraction on the microstructure and tensile properties of 3D printed prepreg filaments remains miss. Therefore, this study selected suitable impregnation processes and materials to prepare prepreg filaments with different fiber volume fraction and investigated their mechanical properties and microscopic morphologies. The results show that the increase of fiber volume fraction effectively promoted the interface bonding between fiber and resin, and increased capacity for load transfer. When the fiber volume fraction was 54.0 %, the tensile strength of the prepreg filaments and specimens reached 1977 MPa and 334 MPa, respectively. This study can provide a process optimization strategy for the preparation of more types of continuous fiber prepreg filaments with high fiber volume fraction, as well as a data reference for the preparation of high-performance 3D-printed thermoplastic composites.
高性能连续碳纤维预浸丝是近年来增材制造领域的研究热点,被认为是提高热塑性复合材料部件机械强度的有效选择。然而,纤维体积分数对三维打印预浸料长丝的微观结构和拉伸性能的影响仍然是个未知数。因此,本研究选择了合适的浸渍工艺和材料来制备不同纤维体积分数的预浸丝,并研究了它们的力学性能和微观形态。结果表明,纤维体积分数的增加能有效促进纤维与树脂之间的界面粘合,提高载荷传递能力。当纤维体积分数为 54.0 % 时,预浸丝和试样的拉伸强度分别达到 1977 兆帕和 334 兆帕。该研究为制备更多类型的高纤维体积分数连续纤维预浸长丝提供了工艺优化策略,也为制备高性能三维打印热塑性复合材料提供了数据参考。
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Additive manufacturing letters
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