Open Access
Review
Table 2.
Property comparisons between EBAM and wrought Ti-6Al-4V.
| Material | Application | Mechanical properties | Ref. |
|---|---|---|---|
| TiAl | High temperature, propulsion exhaust system | YS/UTS (700 °C): ~300 MPa, 360 MPa | [2, 45, 46] |
| H13 | Tool, die/mold | As-processed hardness of 48-50 HRC | [7] |
| Co-Cr based alloys | High temperature bearings, biomedical implants | Micro-hardness: 4.4 to 5.9 GPa | [47, 48] |
| Cu | Electrical | Micro-hardness: 88 HV | [50] |
| Ni based alloys | Jet engine parts | YS/UTS (538 °C): 300 MPa, 610 MPa | [51] |
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