Understanding deformation and fracture mechanism of Ti-55531 alloy under complex loading conditions: a case of pre-tensioned torsion
摘要
The deformation and fracture failure of aerospace structural components are primarily affected by complex loading conditions. This study aims to investigate how various pre-tension strains (0%, 4% and 6%) influence the torsional properties, deformation and fracture mechanism of the Ti–5Al–5Mo–5V–3Cr–1Zr (Ti-55531) alloy with the bimodal microstructure. The results indicate that increasing the pre-tension strain gradually decreases the torsional strength of specimens. However, their torsional ductility initially increases (from 0 to 4% pre-tension strain) and then decreases (from 4 to 6% pre-tension strain). This can be attributed to the significant influence of different pre-tension strains on the deformation mechanism of each phase in the alloy. Under pure torsion loading, the primary α (αp) phase mainly undergoes the {0002} basal slip for deformation. However, at a pre-tension strain of 4%, the torsional deformation mechanism of αp transforms into crossing reaction between the {