Experimental determination of the residual stresses in a spiral weld overlay tube

Neutron diffraction was used to determine the residual stresses in a spiral weld overlay tube. The specimen was a 2.5 in. OD carbon steel tube covered with a layer of alloy 625 weld overlay. Residual strains in the carbon steel and weld overlay layers were determined using the ferritic (211) and austenitic (311) reflections, respectively. The residual stresses in each material were derived from the measured strains using Hookeʹs law and appropriate elastic constants. Tensile stress regions were found not only in the weld metal but also in the heat-affected zone in the carbon steel. The maximum tensile stress was located in the weld overlay layer and amounted to 360 MPa, about 75% of the 0.2% yield strength of the weld metal. The experimental data were compared with a finite element analysis based on an uncoupled thermal-mechanical formulation. Overall, the modeling results are in satisfactory agreement with the experimental data, although the hoop strain (stress) seems to have been overestimated by the finite element model. Additional neutron diffraction measurements reveal that these welding residual stresses vanished after annealing at 900°C for 20 min.