首页> 外文会议>International Congress on Applications of Lasers and Electro-Optics >INVESTIGATION OF LASER CONSOLIDATION FOR MANUFACTURING FUNCTIONAL NET-SHAPE COMPONENTS FOR POTENTIAL ROCKET ENGINE APPLICATIONS
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INVESTIGATION OF LASER CONSOLIDATION FOR MANUFACTURING FUNCTIONAL NET-SHAPE COMPONENTS FOR POTENTIAL ROCKET ENGINE APPLICATIONS

机译:用于制造潜在火箭发动机应用的功能性网状部件激光固结的研究

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Laser consolidation is an emerging novel computer-aided manufacturing process that produces net-shape functional metallic parts layer by layer directly from a CAD model by using a laser beam to melt the injected powder and re-solidifying it on the substrate or previous layer. As an alternative to the conventional machining process, this novel manufacturing process builds net-shape functional parts or features on an existing part by adding instead of removing material. In this paper, laser consolidation of IN-625 and Ti-6Al-4V alloys has been investigated to build several generic shapes representing parts that may have potential rocket engine applications. Laser consolidation produces components with good surface finish, dimensional accuracy and mechanical properties, and demonstrates the potential for direct manufacturing of functional net-shape components and tooling. In addition, some preliminary results demonstrate that the laser consolidation, in combination with solid-state, net-shape powder metallurgy processing, may provide a unique manufacturing capability to make very complex components for the rocket engines.
机译:激光固结是一种新的新型计算机辅助制造工艺,通过使用激光束将注入的粉末熔化并将其重新固化在基板或前一层上,通过直接从CAD模型直接从CAD模型产生网状功能金属部件层。作为传统加工过程的替代方案,通过添加代替除去材料,该新颖的制造过程在现有部分构建了净形功能部件或特征。在本文中,研究了625 in-625和Ti-6AL-4V合金的激光固结,以构建几种通用形状,代表可能具有潜在的火箭发动机应用的部件。激光固结产生具有良好表面光洁度,尺寸精度和机械性能的组件,并演示了直接制造功能性网状部件和工具的可能性。此外,一些初步结果表明,激光固结与固态,净形粉末冶金加工组合可以提供独特的制造能力,为火箭发动机制造非常复杂的部件。

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