journal article·2014-07Open access

Degradation of titanium 6Al–4V fatigue strength due to electrical discharge machining

Todd M. Mower

Abstract

Electrical discharge machining (EDM) has been known for many years to induce degradation of fatigue strength. Outdated or coarse EDM processing methods can reduce the fatigue strength of titanium alloy Ti–6Al–4V by as much as factors of 2–5, but a paucity of fatigue data exists for this important aerospace alloy processed with modern EDM techniques. An experimental study is presented in which the degradation of fatigue strength of Ti–6Al–4V due to improved EDM processing is measured in axial tension at a load ratio of R = 0.1. It is shown that, relative to specimens finely milled, state-of-the-art EDM processing causes a reduction of fatigue strength by 15–30%. This strength degradation is found to correlate directly to the thickness and roughness of recast layers created by the solidification of melt material formed during EDM. Post-processing with either electrochemical polishing or bead blasting is demonstrated to remove the deleterious effects of EDM, such that specimens possessed intrinsic fatigue behavior as indicated by crack initiation at interior locations.
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Research context

OpenAlex topics: Advanced Machining and Optimization Techniques · Advanced machining processes and optimization · Advanced Surface Polishing Techniques

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (42)

Show source-provided references
1. Structure and properties of titanium and titanium alloys
2. Donachie · 1988
3. Machining of titanium alloys
4. Battelle Columbus. Metallic materials and elements for aerospace vehicle structures (MIL-HDBK-5H). U.S. Department of, Defense; 2003: 5–67–73.
5. Investigation of variability in fatigue crack nucleation and propagation in alpha+beta Ti–6Al–4V10.1016/j.proeng.2010.03.198 ↗
6. Characterization of fatigue crack-initiation facets in relation to lifetime variability in Ti–6Al–4V10.1016/j.ijfatigue.2011.11.017 ↗
7. Military handbook on titanium and titanium alloys (MIL-HDBK-697A); 1974. p. 44.
8. High cycle fatigue of electrical-discharge machined AISI D2 tool steel10.1504/IJMPT.2001.001286 ↗
9. Improvement of fatigue life of electrical discharge machined AISI D2 tool steel by TiN coating10.1016/S0921-5093(01)01268-0 ↗
10. Improving the fatigue life of electro-discharge-machined SDK11 tool steel via the suppression of surface cracks10.1016/j.ijfatigue.2008.07.013 ↗
11. Comparison of grinding and Wire EDM concerning fatigue strength and surface integrity of machined Ti6Al4V components10.1016/j.proeng.2011.11.099 ↗
12. Fatigue endurance of Ti–6Al–4V alloy with electro-eroded surface for improved bone in-growth10.1016/j.jmbbm.2010.12.001 ↗
13. The effect of microstructure on fatigue performance ofTi–6Al–4V alloy after EDM surface treatment for application in orthopaedics10.1016/j.jmbbm.2011.06.012 ↗
14. Process simulation and residual stress estimation of micro-electrodischarge machining using finite element method10.1143/JJAP.44.5254 ↗
15. Improvements in residual stress measurement by the incremental centre hole drilling technique10.1007/s11340-006-7686-8 ↗
16. Surface and sub-surface quality of steel after EDM10.1002/adem.200500211 ↗
17. Electrical discharge machining of titanium alloy (Ti–6Al–4V)10.1016/j.apsusc.2007.05.031 ↗
18. Surface integrity in electrical discharge machining of Ti–6Al–4V10.4028/www.scientific.net/AMR.76-78.613 ↗
19. Workpiece surface roughness and integrity after WEDM of Ti–6Al–4V and Inconel 718 using minimum damage generator technology10.1016/j.cirp.2008.03.054 ↗
20. Nicholas · 2006
21. Fatigue mechanics: an assessment of a unified approach to life prediction
22. Solutions to metal surface problems. Able Electropolishing. Chicago, IL; 2008.
23. Post-sintering heat treatments for porus coated Ti–6Al–4V alloy
24. Fatigue fracture behavior of Ti–6Al–4V PVD coated
25. The effect of a plasma-sprayed hydroxyapatite coating on the fatigue properties of Ti–6Al–4V10.1016/0167-577X(93)90189-5 ↗
26. Hydroxyapatite-coated Ti–6Al–4V Part 1: the effect of coating thickness on mechanical fatigue behavior10.1016/S0142-9612(01)00321-0 ↗
27. Influence of shot peening on surface integrity of some machined aerospace materials
28. Fatigue response of the various titanium alloy classes to shot peening
29. On the influence of mechanical surface treatments – deep rolling and laser shock peening – on the fatigue behavior of Ti–6Al–4V at ambient and elevated temperatures10.1016/S0921-5093(03)00069-8 ↗
30. Effects of precoating surface treatments on fatigue of Ti–6Al–4V10.1002/jab.770060305 ↗
31. Clauer AH. Laser shock peening for fatigue resistance. In: Gregory, Rack, Eylon, editors. Surface performance of titanium. Warrendale (PA): TMS; 1996. p. 217–230.
32. Fatigue crack nucleation and growth rate behavior of laser shock peened titanium10.1016/S0142-1123(99)00072-9 ↗
33. Fatigue life improvement of α-titanium by novel ultrasonically assisted technique10.1016/j.msea.2006.07.119 ↗
34. Jayaraman · 2005
35. Titanium hydride and hydrogen concentration in acid-etched commercially pure titanium and titanium alloy implants: a comparative analysis of five implant systems10.1111/j.1600-0501.2010.01938.x ↗
36. Polarization of modified titanium and titanium–zirconium creates nano-structures while hydride formation is modulated10.1016/j.apsusc.2013.04.059 ↗
37. Crystallograpic properties and mechanical behavior of titanium hydride layers grown on titanium implants10.1080/14786430310001627386 ↗
38. Ordered nano-scale dimple pattern formation on a titanium alloy (Ti–6Al–4V)
39. MTS Service Note. #100-161-434a Variability. MTS Systems Corp., Eden Prairie, MN; 2012.
40. ASTM Standard E1012. Standard practice for verification of testing frame and specimen alignment under tensile and compressive axial force application. ASTM Internatioinal, West Conshohocken, PA; 2012.
41. A study of cyclic fatigue, damage initiation, damage propagation, and fracture of welded titanium alloy plate10.1016/j.msea.2010.06.086 ↗
42. Measurements of stress by X-ray diffraction. TEC Materials Testing Division, White paper, Knoxville, TN; 2002.