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Tensile Properties and Microstructures of Laser-Formed Ti-6Al-4V
Authors:J. Alcisto  A. Enriquez  H. Garcia  S. Hinkson  T. Steelman  E. Silverman  P. Valdovino  H. Gigerenzer  J. Foyos  J. Ogren  J. Dorey  K. Karg  T. McDonald  O. S. Es-Said
Affiliation:1. Mechanical Engineering Department, Loyola Marymount University, One LMU Drive, Los Angeles, CA, 90045, USA
2. Northrop Grumman, Space Technology, One Space Park, Redondo Beach, CA, 90278, USA
3. Triton Systems Incorporated, 200 Turnpike Road, Chelmsford, MA, 01824, USA
Abstract:
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)? 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? 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.
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