Tensile Properties and Microstructures of Laser-Formed Ti-6Al-4V

被引:264
作者
Alcisto, J. [1 ]
Enriquez, A. [1 ]
Garcia, H. [1 ]
Hinkson, S. [1 ]
Steelman, T. [2 ]
Silverman, E. [2 ]
Valdovino, P. [2 ]
Gigerenzer, H. [3 ]
Foyos, J. [1 ]
Ogren, J. [1 ]
Dorey, J. [1 ]
Karg, K. [3 ]
McDonald, T. [3 ]
Es-Said, O. S. [1 ]
机构
[1] Loyola Marymount Univ, Dept Mech Engn, Los Angeles, CA 90045 USA
[2] Northrop Grumman Space Technol, Redondo Beach, CA 90278 USA
[3] Triton Syst Inc, Chelmsford, MA 01824 USA
基金
美国国家科学基金会;
关键词
laser free-form fabrication (LF3); mechanical properties; microstructure; Ti-6Al-4V;
D O I
10.1007/s11665-010-9670-9
中图分类号
T [工业技术];
学科分类号
120111 [工业工程];
摘要
The room temperature tensile properties of Ti-6Al-4V alloy prepared under two different processing routes were evaluated and compared. One group of samples was prepared by conventional casting-forging-rolling into flat plates. The other group was prepared by using Triton's Laser Free-Form Fabrication (LF3)(TM) processes, i.e., a laser was used to melt pre-alloyed powders of the required metallic composition as they were dropped onto a moveable substrate programmed to move in such a manner as to form a solid alloy plate. Five populations of Ti-6Al-4V were evaluated: a standard wrought form, an as-deposited form, a machined as-deposited form, a heat-treated as-deposited form, and a machined as-deposited and heat-treated form. The poorest mechanical properties occurred with the rough surfaces, likely due to existing microcracks and stress concentrations. The LF3 (TM) as-deposited material had mechanical properties comparable to, if not higher than, the mechanical properties of the wrought material. Further evaluations of the laser-formed material for complex spacecraft piece parts were warranted, specifically in regards to improving the surface finish of the materials.
引用
收藏
页码:203 / 212
页数:10
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