Aero-engine blisk welded by electron beam welding（EBW） method is a complicated structure. Fixtures were used to control the deformation of blisk during its manufacturing process. Finite element method was utilized t...Aero-engine blisk welded by electron beam welding（EBW） method is a complicated structure. Fixtures were used to control the deformation of blisk during its manufacturing process. Finite element method was utilized to study the evolution of the welding residual stress and deformation of this structure. In which an attenuation function was applied to the double ellipsoid heat source model based on the characteristic of EBW, and the effects of fixtures on the welding residual stresses and deforamtion were also reserached. The simulation results showed that the temperature contour of weld cross section vertical to the weld centerline followed a ＇＂ V＂ shape. Moreover, large welding residual stress and distortion were found in the interface between blisk and fixtures. The stress concentration was reduced sufficiently in starting and end part of weldment as the fixtures were renmved after welding process, while the removing operation had almost no effects on the welding residual stress in the middle section of weld bead.展开更多
The residual stresses distribution of 7075 aluminum alloy in vacuum electron beam welding joint was numerically simulated using nonlinear finite element method. The result shows that the longitudinal residual stress i...The residual stresses distribution of 7075 aluminum alloy in vacuum electron beam welding joint was numerically simulated using nonlinear finite element method. The result shows that the longitudinal residual stress is tension stress along weld center and the stress peak value appears in the middle of the welded seam; the transversal residual stress is compression stress ; the residual stress in thickness direction is very small.展开更多
基金This research was sponsored by China Postdoctoral Science Foundation （No. 20070410900） , Shandong Provincial Key Lab of Special Welding Technology, Harbin Institute of Technology at Weihai.
文摘Aero-engine blisk welded by electron beam welding（EBW） method is a complicated structure. Fixtures were used to control the deformation of blisk during its manufacturing process. Finite element method was utilized to study the evolution of the welding residual stress and deformation of this structure. In which an attenuation function was applied to the double ellipsoid heat source model based on the characteristic of EBW, and the effects of fixtures on the welding residual stresses and deforamtion were also reserached. The simulation results showed that the temperature contour of weld cross section vertical to the weld centerline followed a ＇＂ V＂ shape. Moreover, large welding residual stress and distortion were found in the interface between blisk and fixtures. The stress concentration was reduced sufficiently in starting and end part of weldment as the fixtures were renmved after welding process, while the removing operation had almost no effects on the welding residual stress in the middle section of weld bead.
基金The project is supported by the Found of Key Fields Project of Inner Mongolia Education Department (No ZL02021)
文摘The residual stresses distribution of 7075 aluminum alloy in vacuum electron beam welding joint was numerically simulated using nonlinear finite element method. The result shows that the longitudinal residual stress is tension stress along weld center and the stress peak value appears in the middle of the welded seam; the transversal residual stress is compression stress ; the residual stress in thickness direction is very small.
