Abstract
A plasma chromizing treatment was conducted on Ti6Al4V samples by employing the recently developed double glow plasma surface alloying technology. The Cr-Alloyed layer consisted of four sub-layers, namely the Cr deposition, Cr 2 Ti, CrTi 4 , and Cr-Ti solid-solution layers. The local hardness and moduli were determined via nanoindentation. In addition, the fatigue properties of the samples were evaluated by using a rotating-bending fatigue machine under a given load. The results showed that the hardness or elastic moduli of the adjacent sub-layers differed significantly and the fatigue properties of the Ti6Al4V alloy deteriorated with the plasma chromizing treatment. This deterioration stemmed mainly from cracks initiated at the interfaces between the sub-layers and the microstructural changes of the substrate; these changes were induced by the high temperature used in the plasma chromizing process. However, the fatigue life of the plasma-chromized samples was increased by a shot peening post-treatment. The fatigue life of the samples resulting from this combination of treatments was slightly higher than that of the single-shot-peened Ti6Al4V substrate. In fact, the sample retaining only the Cr-Ti solid-solution layer (that is, the first three sub-layers were removed), when shot-peened, exhibited the highest fatigue life among all the tested samples; this was attributed to that sample having the highest residual compressive stress, the significant work hardening, and the good hardness to toughness balance.
| Original language | English |
|---|---|
| Pages (from-to) | 995-1002 |
| Number of pages | 8 |
| Journal | Applied Surface Science |
| Volume | 353 |
| DOIs | |
| State | Published - 30 Oct 2015 |
Keywords
- Plasma chromizing
- Residual stress
- Rotating-bending fatigue
- Shot peening
- Ti6Al4V
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