Stress corrosion cracking and fatigue crack growth behavior were determined
in 17-4 PH stainless steel under various metallurgical conditions, includi
ng the H900 (482 degreesC/1 h), H1025 (552 degreesC/4 h) aging and laser su
rface annealing treatments. Peak-aged (H900) specimens locally irradiated b
y laser beam consisted of a portion of composite region (CR), in which comp
rised of soft laser-annealed (LA) zones on the outer surfaces and the hard
base metal in between. Slow extension rate tensile tests were performed at
room temperature in a saturated H,S solution to evaluate the: hydrogen embr
ittlement susceptibility of various specimens. H900 specimens show an obvio
us improvement in impact toughness after irradiating by laser. Regardless o
f testing environments, H900 specimens exhibited better tensile properties
than the other specimens. Experimental results also indicated that H900 spe
cimens had the highest fatigue crack growth rates among the specimens, part
icularly at low stress intensity factor range. The retardation of crack gro
wth in the region ahead of the CR in the LA specimens was rather pronounced
. For compact tension specimens tested in gaseous hydrogen, enhanced crack
growth was correlated with quasi-cleavage fracture in contrast to transgran
ular fatigue fracture in air. (C) 2001 Elsevier Science B.V. All rights res
erved.