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Full Length Article | Open Access

Safety lifetime analysis method for multi-mode time-dependent structural system

Yingshi HUZhenzhou LU( )Ning WEIXia JIANGChangcong ZHOU
School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China

Peer review under responsibility of Editorial Committee of CJA.

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Abstract

It is important to determine the safety lifetime of Multi-mode Time-Dependent Structural System (MTDSS). However, there is still a lack of corresponding analysis methods. Therefore, this paper establishes MTDSS safety lifetime model firstly, and then proposes a Kriging surrogate model based method to estimate safety lifetime. The first step of proposed method is to construct the Kriging model of MTDSS performance function by using extremum learning function. By identifying possible extremum mode of MTDSS, the performance function of MTDSS can be equivalently transformed into the one of Single-mode Time-Dependent Structure (STDS). The second step is to use the Advanced First Failure Instant Learning Function (AFFILF) to train the Kriging model constructed in the first step, so that the convergent Kriging model can identify the possible First Failure Instant (FFI) of STDS. Then safety lifetime can be searched quickly by dichotomy search. By using AFFILF, the minimum instant that the state is not accurately identified by the current Kriging model is selected as the training point, which avoids the unnecessary calculation which may be introduced into the existing First Failure Instant Learning Function (FFILF). In addition, the Candidate Sample Pool (CSP) reduction strategy is also adopted. By adaptively deleting the random candidate sample points whose FFI have been accurately identified by the current Kriging model, the training efficiency is further improved. Three cases show that the proposed method is accurate and efficient.

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Chinese Journal of Aeronautics
Pages 294-308

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Cite this article:
HU Y, LU Z, WEI N, et al. Safety lifetime analysis method for multi-mode time-dependent structural system. Chinese Journal of Aeronautics, 2022, 35(11): 294-308. https://doi.org/10.1016/j.cja.2022.01.019

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Received: 20 May 2021
Revised: 09 June 2021
Accepted: 06 July 2021
Published: 01 February 2022
© 2022 Chinese Society of Aeronautics and Astronautics.

This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).