Study of SCC Mechanism by Direct Observation and Analysis of Dislocation Substructure in α Phase of Ti-8Al-1Mo-1V in Stress Corrosion Cracking
1) Milled Ti-8Al-1Mo-1V bar, which had α2 precipitates and crystallographic texture.
2) Hot isostatic pressed (HIPped) Ti-8Al-1Mo-1V, which had α2 precipitates but no texture.
3) HIPped Ti-8Al-1Mo-1V was heat-treated to supress α2 phase transformation, and it did not have any crystallographic texture.
Presence of crystallographic texture (sample 1) increases the SCC crack velocity by 1 magnitude and decreases the SCC stress intensity factor more than 50% compared to sample without (sample 2). There is no SCC crack propagation in sample 3 due to the absence of texture and α2 precipitates.
In the SCC tests of sample 1 and 2, there was a fracture mode transition from ductile failure during pre-cracking where dimples are dominated on fracture surface to brittle failure during NaCl environment where facets are dominated. In order to understand the SCC fracture mechanisms, transmission electron backscatter diffraction (T-EBSD) and transmission electron microscope (TEM) analysis were applied on focus ion beam (FIB) lift-out lamellas cut from pre-cracking region and SCC fractured region to investigate the relationship between the fracture surface and crystallographic orientation of sub-grains, and nature of activated dislocation underneath the fracture surface.
It has been found that:
- Ti-8Al-1Mo-1V does not suffer SCC when crystallographic texture and α2 precipitates are eliminated.
- In pre-cracking region where failure occurred in air, slip was the dominate slip system and slip with component was also activated.
- The SCC fracture surfaces were either parallel to or inclined 15o away from basal planes of a. Dislocations containing component are observed to contribute to such failure and surprisingly no dislocations are observed.