Effects of High Productivity Machining on Ti-6Al-4V Surface Topography

2004-01-2827

09/21/2004

Event
SAE 2004 Aerospace Manufacturing & Automated Fastening Conference & Exhibition
Authors Abstract
Content
Surface defects were demonstrated to result from high productivity machining (HPM) as well as conventional machining of a titanium alloy Ti-6Al-4V, with HPM causing the larger sized defects. These defects could act as initiation sites for fatigue cracks showing that machining would affect fatigue strength and life of the part produced. A finishing pass appears to remove the defects. Better understanding is needed of the relationships between machining, surfaces, and strength.
Meta TagsDetails
DOI
https://doi.org/10.4271/2004-01-2827
Pages
7
Citation
Modgil, A., Schueller, J., Ziegert, J., and Bhattacharyya, A., "Effects of High Productivity Machining on Ti-6Al-4V Surface Topography," SAE Technical Paper 2004-01-2827, 2004, https://doi.org/10.4271/2004-01-2827.
Additional Details
Publisher
Published
Sep 21, 2004
Product Code
2004-01-2827
Content Type
Technical Paper
Language
English