Abstract
This paper investigates the level of properties enhancement achievable by heat-treating Ti-6Al-4V alloy produced from a blended powder mixture using a thermomechanical powder consolidation route involving warm uniaxial pressing and vacuum sintering followed by extrusion at super transus temperature (1150°C). The as-extruded material with a higher oxygen content of 0.55 wt.% was subjected to two different sub-transus annealing treatments: HT-A: 955°C/1h furnace cooling and HT-B: 925°C/4h-cooling @ 50°C/h to 760°C-FCfurnace cooling. Room temperature Charpy v-notch impact toughness tests and tensile tests were performed to ascertain the effect of microstructural changes during post-extrusion annealing treatments. After impact tests, analysis of microstructures and fracture surfaces of samples after impact tests were was carried out using optical microscopy and scanning electron microscopy. The as-extruded material displayed mean impact toughness of 4 J along with a yield strength of 956 MPa, an ultimate tensile strength of 22 1150 MPa, and an elongation to fracture of 2.4%. The annealing treatments gave a noticeable enhancement in the impact toughness (average values 5.3-6.3 J obtained) while maintaining a yield strength and ultimate tensile strength level of about 992 MPa and 1164-1181 MPa, respectively. Additionally, the level of change in ductility was limited for each sub-transus annealing treatment, and HT-A has given only a 30% increase compared to as-extruded material.
Original language | English |
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Article number | 173 |
Number of pages | 20 |
Journal | Metals |
Volume | 13 |
Issue number | 1 |
Early online date | 14 Jan 2023 |
DOIs | |
Publication status | Published - 14 Jan 2023 |
Funding
This research was funded by the Ministry of Business, Innovation, and Employment (MBIE), New Zealand, grant number UOWX1402.
Keywords
- titanium alloys
- thermochemical powder consolidation
- microstructures
- impact toughness
- tensile properties
- crack propagation
- fracture behaviour