Nitrogen-rich inclusions can lead to a reduction in fatigue life of highly
stressed titanium-alloy components (found in the compressor sections of pow
er generation gas turbines, turbine sections of power generation steam turb
ines, wing sections of aircraft air frames, and compressor and fan sections
of aircraft jet engines, for example). It is the "crack starting" nature o
f the nitrogen-rich inclusions that is the problem, not the presence of nit
rogen in the system, per se. This paper covers the theory and laboratory ex
periments used to evaluate ESR (electro-slag refining) as an alternative te
chnique for rapid dissolution of nitrogen-rich inclusions in titanium and t
itanium alloys, Five variations of melt rate, slag temperature and inclusio
n type were evaluated. One variant showed complete dissolution of the inclu
sions. Several of the other variants showed partial dissolution of the incl
usions. The kinetics were observed to occur at a rate 100 to 1000 times fas
ter than the rate of dissolution of nitrogen-rich inclusions by immersion i
n liquid titanium.