Ambient-temperature, low-cycle dwell-time and conventional low-cycle fatigu
e tests were performed on Ti-6Al-2Sn-4Zr-2Mo-0.1Si (Ti-6242). Specimens wer
e solution annealed at various temperatures below the beta transus to contr
ol the volume fraction of primary alpha phase and were subsequently shot-pe
ened. The influence of the changes in primary alpha phase on the low-cycle
dwell-time fatigue life (LCDF) were determined and compared to the conventi
onal low-cycle fatigue (LCF) properties of the alloy. A 120-second dwell si
gnificantly decreased the number of cycles to failure, although the factor
decrease of LCF from a dwell, in general, diminished with decreasing stress
. The Increasing primary alpha phase associated with lower solution tempera
tures appears to increase susceptibility to low-cycle dwell-time fatigue. I
t also appears that the susceptibility to dwell fatigue may be associated w
ith ambient-temperature, time-dependent, cyclic (creep) plasticity.