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SBIR Phase I: Repair, Weld, and Build Metallic Parts with Fill Impact Welding

SBIR Phase I: Repair, Weld, and Build Metallic Parts with Fill Impact Welding
SBIR 第一阶段:使用填充冲击焊修复、焊接和构建金属零件
批准号:
2322343
负责人:
Anupam Vivek
金额:
$27.5万
依托单位:
依托单位国家:
美国
项目类别:
Standard Grant
财政年份:
2023
资助国家:
美国
项目状态:
已结题
起止时间:
2023-09-01 至 2024-08-31

项目摘要

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中文摘要
翻译
该小型企业创新研究 (SBIR) 第一阶段项目的更广泛/商业影响旨在开发一种焊接技术,以改善金属零件和功能的修复、连接和增材制造。首批应用包括在飞机生产和维修过程中添加材料来修复凿孔和误钻的孔,这两者都代表着巨大的经济机会。由于当前可用的修复方法通常由于极端温度而对基材性能产生不利影响,因此目前不允许在生产环境中对结构材料进行修复。航空结构制造商有强烈的动机来最大程度地减少飞机结构的重量,但通常会因报废整个面板而付出巨大的财务和环境代价。维护、修理和大修通常需要用新部件完全更换损坏的部件,因为关键部件的维修不当可能会造成灾难性的损害。由于航空航天工业的高价值、小批量的性质,更换零件成本高昂且交货时间长。该项目将开发一种有效的修复方法来修复金属部件,同时不受材料和零件几何形状的影响。回收由钛、镍和铝等材料制成的以前无法修复的零件会对环境产生巨大的积极影响。 此外,通过广泛实现固态连接,​​该技术将颠覆全球价值 200 亿美元的焊接行业。这个由美国主导的基础技术平台将在科学、技术和工程领域创造新的就业机会,同时加强国内制造业供应链。支撑该项目的创新涉及使用爆炸焊接进行连续、战术和受控的金属沉积。 爆炸焊接使用硬币大小的金属元件,以 300-1000m/s 的速度发射,无需爆炸物。虽然众所周知,爆炸焊接可以将大板焊接在一起,但该方法不适合自动化或传统工业环境。冲击焊接将发展为一种填充焊接技术,就像传统焊接中的填充金属一样,并将使用变形金属板材作为原料。在这里,电汽化金属箔将用作填充元件的驱动器,研究重点是这些元件是否可以重复发射以开发大粘合面积和可重复定位。在飞行过程中控制元件形状和方向以及产生完全焊接的界面的能力是该技术风险最高的方面。将进行机械测试、扫描电子显微镜和在线过程监控(例如光子多普勒测速)。这项工作将开发一个新的工艺-结构-性能循环,目标是生产比采用冷喷涂等竞争技术制造的零件更好的零件(从总能耗、成本和机械性能来衡量)。该奖项反映了 NSF 的法定使命,并通过使用基金会的智力优点和更广泛的影响审查标准进行评估,被认为值得支持。
英文摘要
The broader/commercial impact of this Small Business Innovation Research (SBIR) Phase I project seeks to develop a welding technology that will improve the repair, joining, and additive manufacturing of metallic parts and features. First applications include material additions to repair gouges and mis-drilled holes during aircraft production and service, both of which represent significant financial opportunities. Repairs to the structural material are not currently permissible in a production environment due to adverse effects of currently available repair methods on base material properties, usually due to extreme temperatures. Aerostructure manufacturers have a strong incentive to minimize the weight of the aircraft structure, often at the significant financial and environmental expense of scrapping a whole panel. Maintenance, repair and overhaul often entails total replacement of damaged components with new ones as improper repairs of critical components can cause catastrophic harm. Replacement of parts is expensive and has long lead times due to high-value, low-volume nature of the aerospace industry. This project will develop an effective restoration method to repair of metallic components, while being agnostic to the material and part geometry. Reclamation of previously unrepairable parts made from materials such as titanium, nickel, and aluminum has a large positive environmental impact. Additionally, by broadly enabling solid-state joining, this technology will disrupt the welding industry, globally valued at $20 billion. The foundational technology platform, led in the US, will produce new jobs in science, technology and engineering fields while bolstering domestic manufacturing supply chains.The innovation underpinning this project involves the sequential, tactical, and controlled deposition of metals using explosive welding. Explosive welding uses coin-sized metallic elements launched to speeds in the range of 300-1000m/s without explosives. While it is known that explosive welding can weld large plates together, the method is not suited to automation or conventional industrial settings. Impact welding will be developed as a fill-welding technique, much like a filler metal in conventional welding, and will use wrought sheet metal as feedstock. Here, electrically vaporized metallic foils will be used as the driver for the fill elements and the research will focus on whether those elements can be launched reproducibly to develop large bond areas and reproducible positioning. The ability to control element shape and orientation during flight and produce an interface that is fully welded are the most high-risk aspects of the technology. Mechanical testing, scanning electron microscopy, and inline process monitoring such as photonic Doppler velocimetry will be performed. This effort will develop a new process-structure-property loop, with the goal of producing parts that are better than those made with a competing technology such as cold spray as measured by total energy consumption, cost, and mechanical properties.This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.
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国内基金
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