Push-pull law-cycle fatigue tests were carried out on annealed and hot-roll
ed commercially pure titanium under total strain control at 77 K. Very obvi
ous cyclic-hardening behaviour was observed at the beginning of fatigue for
the strain amplitudes employed. A large number of twins with various appea
rances was observed in the microstructure of fatigued specimens of annealed
and hot-rolled titanium. Three twinning systems, (11 (2) over bar(1) over
bar), (1 (1) over bar 02) and (1 (2) over bar 12) types, are operative in t
he cyclic deformation of titanium. Twinning is considered to be the main de
formation mode of pure titanium fatigued at 77 K and to be the main reason
for the cyclic hardening of pure titanium at low temperature. (C) 2001 Else
vier Science Ltd. All rights reserved.