LI Bo1, YUAN Qiwei1, JIN Kai2, WAN Bofang3, WANG Hui2, GUO Xunzhong1, TAO Jie1. Numerical Simulation and Experiment Study on Tube Spinning of GH625 Reducer Tube. Aeronautical Manufacturing Technology, 2017, 60(18): 36-42.
LI Bo1, YUAN Qiwei1, JIN Kai2, WAN Bofang3, WANG Hui2, GUO Xunzhong1, TAO Jie1. Numerical Simulation and Experiment Study on Tube Spinning of GH625 Reducer Tube. Aeronautical Manufacturing Technology, 2017, 60(18): 36-42. DOI: 10.16080/j.issn1671-833x.2017.18.036.
Numerical Simulation and Experiment Study on Tube Spinning of GH625 Reducer Tube
The elastic-plastic finite element model for the GH625 neck-spinning process was established by ABAQUS/Explicit software. The distribution of the stress
strain and the variation of the cross section of tube spinning process were analyzed. Furthermore
the effect of the spinning parameters on forming quality was obtained
such as axial feed rate
roller nose radius and roller installation angle. The spinning process results showed that the cross-sections in different zone of tube were generated different deformation. The results also reflected that the thickness increased with the increasing of the axial feed rate and roller nose radius. The roller installation angle had little influence on the tube thickness. The ellipticity became larger as the axial feed rate and roller nose radius increased. Located away from the free end
the ellipticity increased as the roller installation angle decreased. The distribution of the ellipticity was uneven when the roller was near the free end of the tube. Finally
the process parameters was selected based on the simulation: 0.25mm/r of axial feed rate
2-4mm of roller nose radius
90º of roller installation angle. The experiment was conducted and the accuracy quality tube was manufactured by neck-spinning experiment.