Abstract
Due to their unique advantages of high strength, high performance, and light weight, ultra-thin-walled (UTW) tubes have attracted increasing application in the aviation and aerospace industries. However, wrinkling, cracking, cross-section distortion, and even collapse easily occur in UTW tube bending process. In this study, a new mandrel design method with variation in the mandrel ball thickness for bending UTW tubes was proposed to improve the forming quality. First, a basic mandrel design scheme with a uniform mandrel ball thickness was determined according to engineering experiences and preliminary research. Then, three different mandrel ball thicknesses were determined based on the same mandrel support angle of the basic scheme (BS), and combination schemes (CSs) of mandrel balls with different thicknesses were designed. A 3D elastic–plastic finite element (FE) model of the numerical control (NC) bending process of UTW tubes was established and verified, and the influence of different combinations of mandrel ball thickness variation on the bending quality of UTW tubes was investigated. The results showed that compared with the BS, the CSs can effectively improve the von Mises stress distribution and wall thickness uniformity on the extrados, and significantly reduce the wall-thinning ratio, wall-thickening ratios, and ovality of the UTW bent tube. The combination scheme with as many thin mandrel balls as possible at the beginning of the bending and thick mandrel balls at the end of the support was beneficial to reduce the wall-thinning ratio. Increasing the number of medium or thick mandrel balls in combination scheme can increase the mandrel support angle and reduce the ovality of the UTW bent tubes. These results are of great significance for guiding the design of mandrels and improving the forming quality of UTW tubes.
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Funding
The work was supported by the Zhejiang Province Public Welfare Technology Application Research Project(LGG22E050027), the Open Foundation of the State Key Laboratory of Fluid Power and Mechatronic Systems (GZKF-202126), and the National Natural Science Foundation of China (Nos.U20A20287).
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Jiang LF conceived and designed the study; Wang YQ performed numerical simulation and analyzed the data; Lin YC performed the bending experiments; Sun M. edited the manuscript; Jiang LF, Li H., Zhang SY and Feng YX reviewed and improved the manuscript.
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Jiang, L., Lin, Y., Li, H. et al. A new mandrel design with mandrel ball thickness variation for the bending process of aviation ultra-thin-walled tubes. Int J Adv Manuf Technol 122, 1805–1819 (2022). https://doi.org/10.1007/s00170-022-09954-y
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DOI: https://doi.org/10.1007/s00170-022-09954-y