Reliability Assessment for Aeroengine Blisks Under Low Cycle Fatigue With Ensemble Generalized Constraint Neural Network

被引:5
作者
Huang, Chao [1 ,2 ]
Bu, Siqi [3 ,4 ]
Fei, Cheng-Wei [5 ]
Lee, Namkyoung [6 ]
Kong, Shu Wa [1 ,2 ]
机构
[1] Hong Kong Polytech Univ, Dept Elect & Elect Engn, Kowloon, Hong Kong, Peoples R China
[2] Ctr Adv Reliabil & Safety CAiRS, Hong Kong, Peoples R China
[3] Hong Kong Polytech Univ, Res Inst Smart Energy, Ctr Adv Reliabil & Safety CAiRS, Dept Elect & Elect Engn,Shenzhen Res Inst,Ctr Grid, Hong Kong, Peoples R China
[4] Hong Kong Polytech Univ, Policy Res Ctr Innovat & Technol, Kowloon, Hong Kong, Peoples R China
[5] Fudan Univ, Dept Aeronaut & Astronaut, Shanghai 200433, Peoples R China
[6] Univ Maryland, Ctr Adv Life Cycle Engn, College Pk, MD 20742 USA
关键词
Reliability; Kernel; Reliability engineering; Uncertainty; Probabilistic logic; Analytical models; Fatigue; Generalized constraint neural network (GCNN); interpretable machine learning; structural reliability assessment; surrogate model; TURBINE; DESIGN;
D O I
10.1109/TR.2023.3324896
中图分类号
TP3 [计算技术、计算机技术];
学科分类号
0812 ;
摘要
Aeroengine blisks operate in a harsh working environment and are prone to low cycle fatigue (LCF) failure. The probabilistic LCF life prediction considering multiple uncertainties needs to be performed for reliability assessment. To consider the combined effects of heterogeneous uncertainties, this article employs a unified reliability assessment method by processing the uncertainties simultaneously. To overcome the extremely time-consuming limitation of probabilistic finite-element model simulation, this article develops an ensemble generalized constraint neural network (EGCNN)-based unified reliability assessment method. The developed EGCNN surrogate model can conduct efficient, accurate, interpretable, and robust reliability assessments with nonlinear fitting capability, knowledge interpretability, and premature avoidance ability. The developed EGCNN-based unified reliability assessment method can also be applied to other assets and failure mechanisms, providing a new reliability-based design optimization tool.
引用
收藏
页码:922 / 936
页数:15
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