Abstract
The high-pressure rotor of aero-engine is assembled by numerous bolts under high manufacture precision. The connected structure is subjected to both axial force and transverse vibration during service, which may result in individual bolt loosen. In this study, the influence of bolt missing on the dynamic characteristics is analyzed by numerical simulation. A test rig capable of impact and frequency swee** experiment under axial tension was constructed. The vibration response features in the simulation were then extracted. The loss function of the mean absolute error and the decision method of extreme gradient boosting were used to predict the bolt missing position. The results show that the proposed model can reach a prediction precision of more than 90%. Moreover, the coefficient of determination evaluation index of the prediction effect reaches 0.9, which is significantly higher than those of other conventional models such as multivariate linear regression and multivariate adaptive regression spliness.
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The data that support the findings of this study are available on request from the corresponding author. The data are not publicly available due to their containing information that could compromise the privacy of research participant.
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Funding
This research was sponsored by the National Natural Science Foundation of China (51905334), Shanghai Sailing Program (19YF1452400 and 19YF1418600).
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Conceptualization, C.Y. and HS.C.; methodology, C.Y.; validation, ZX.M. and JY.F..; formal analysis, ZL.Z.; investigation, C.Y.;. All authors have read and agreed to the published version of the manuscript.
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Yue, C., Chi, H., Fan, J. et al. Prediction of bolt missing fault for multistage rotor by experimental test and analysis. Int J Adv Manuf Technol 124, 4551–4562 (2023). https://doi.org/10.1007/s00170-022-10356-3
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DOI: https://doi.org/10.1007/s00170-022-10356-3