2022
DOI: 10.1007/s00170-021-08531-z
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Machining deformation analysis of aircraft monolithic components based on the energy method

Abstract: He received his PhD degree from Shandong University, China, in 2015. His research interests is machining of aircraft monolithic components.

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Cited by 2 publications
(3 citation statements)
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References 24 publications
(27 reference statements)
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“…The transition structure and final part have acceptable maximum relative errors of 24.6 % and 23.1 %, respectively, between theoretical calculation results and experimental results. Error generation is primarily caused by three factors (Ye et al, 2020;Weber et al, 2022;Huang et al, 2022): (1) the residual stress brought on by machining is not considered; (2) the effects of clamping and cutting load on machining distortion are not considered;…”
Section: Machining Testmentioning
confidence: 99%
See 1 more Smart Citation
“…The transition structure and final part have acceptable maximum relative errors of 24.6 % and 23.1 %, respectively, between theoretical calculation results and experimental results. Error generation is primarily caused by three factors (Ye et al, 2020;Weber et al, 2022;Huang et al, 2022): (1) the residual stress brought on by machining is not considered; (2) the effects of clamping and cutting load on machining distortion are not considered;…”
Section: Machining Testmentioning
confidence: 99%
“…Findings demonstrate that the proposed technique clearly reduces the maximum and average deformations of thin-walled structures. Huang et al (2022) used the equivalent bending strain energy theory to develop a mathematical model of machining distortion. The accuracy of the model and the relationship between the distortion and the initial stress state in the removed material are demonstrated by finite-element simulation and machining results.…”
Section: Introductionmentioning
confidence: 99%
“…Therefore, assume that the structure is composed of a number of structural element units, the energy method is used to calculate the structural element deformation as [18]:…”
mentioning
confidence: 99%