Standard designs for stress relief features and unmodified joints in n
on-magnetic (austenitic) drillcollar connections are investigated usin
g finite element stress analysis. An NC-61 connection containing API p
in and box stress relief grooves and box boreback features are compare
d, In addition to the recognized problem of fatigue failure from criti
cally loaded threads, instances of stress corrosion cracking in pin bo
res have focused attention on this region and the effect which the pre
sence of a pin stress relief groove has on the stresses there, The res
ults of the analyses confirm the failure sites noted in service, and p
redict that the pin stress relief groove gives considerable benefit in
terms of reducing the pin last engaged thread peak stress (fluctuatio
ns in which can cause fatigue), but causes an unexpected increase in t
he maximum pin bore axial stress (which can drive stress corrosion cra
cking). Copyright (C) 1996 Elsevier Science Ltd.