Life extension of high pressure and intermediate pressure rotors by we
ld repair is a viable alternative considering the latest developments.
Our objective is to select a filler wire that will produce a weld wit
h mechanical properties compatible with those of the rotor material. T
hree filler metals, (CrMoV, 12 percent Cr and 5 percent Cr) were used
in the investigation. Multipass submerged are groove welds were produc
ed, post weld heat treated at 677-degrees-C (1250-degrees-F), and subm
itted to a series of mechanical tests at room and elevated temperature
s. The tests samples were machined parallel to the weld direction (lon
gitudinal), which included only weld metal, and perpendicular to the w
eld metal (crossweld) so that the test sample includes portions of the
weld metal, heat-affected zone (HAZ) and base metal. A limited metall
urgical evaluation was also performed. The room temperature tensile pr
operties of the CrMoV and 12 percent Cr crossweld samples exceeded tho
se of the rotor metal, but the tensile properties of the 5 percent Cr
crosswelds did not match those of the rotor metal. The 12 percent Cr c
rossweld samples failed in the weld metal during hot tensile and stres
s rupture testing, and these failures were attributed to slag entrapme
nt; yet the yield and tensile strengths of these weldments just exceed
ed those of the rotor base metal. The CrMoV crossweld specimens perfor
med the best at the high temperature testing; the failure for the hot
tensile specimens occurred in the weld metal and the values matched th
ose of the all weld metal (longitudinal) specimens which greatly excee
ded the rotor base metal strengths. The crossweld stress rupture sampl
es failed outside the weld metal at the heat affected zone (HAZ) near
the unaffected base metal with rupture lives lower than the rotor base
metal. Microhardness evaluations in the CrMoV and 12 percent Cr cross
weldments about the HAZ/base metal boundary identify a soft region at
this location. The mechanical properties of the 5 percent weldment we
re in general inferior to the rotor base metal. The weld metal's hardn
ess was lower than the rotor base metal given its superior Charpy ener
gy values; however, the creep rupture strength was inferior.