M-LFM: a multi-level fusion modeling method for shape−performance integrated digital twin of complex structure

Xiwang HE, Xiaonan LAI, Liangliang YANG, Fan ZHANG, Dongcai ZHOU, Xueguan SONG, Wei SUN

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Front. Mech. Eng. ›› 2022, Vol. 17 ›› Issue (4) : 52. DOI: 10.1007/s11465-022-0708-0
RESEARCH ARTICLE
RESEARCH ARTICLE

M-LFM: a multi-level fusion modeling method for shape−performance integrated digital twin of complex structure

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Abstract

As a virtual representation of a specific physical asset, the digital twin has great potential for realizing the life cycle maintenance management of a dynamic system. Nevertheless, the dynamic stress concentration is generated since the state of the dynamic system changes over time. This generation of dynamic stress concentration has hindered the exploitation of the digital twin to reflect the dynamic behaviors of systems in practical engineering applications. In this context, this paper is interested in achieving real-time performance prediction of dynamic systems by developing a new digital twin framework that includes simulation data, measuring data, multi-level fusion modeling (M-LFM), visualization techniques, and fatigue analysis. To leverage its capacity, the M-LFM method combines the advantages of different surrogate models and integrates simulation and measured data, which can improve the prediction accuracy of dynamic stress concentration. A telescopic boom crane is used as an example to verify the proposed framework for stress prediction and fatigue analysis of the complex dynamic system. The results show that the M-LFM method has better performance in the computational efficiency and calculation accuracy of the stress prediction compared with the polynomial response surface method and the kriging method. In other words, the proposed framework can leverage the advantages of digital twins in a dynamic system: damage monitoring, safety assessment, and other aspects and then promote the development of digital twins in industrial fields.

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Keywords

shape−performance integrated digital twin (SPI-DT) / multi-level fusion modeling (M-LFM) / surrogate model / telescopic boom crane / data fusion

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Xiwang HE, Xiaonan LAI, Liangliang YANG, Fan ZHANG, Dongcai ZHOU, Xueguan SONG, Wei SUN. M-LFM: a multi-level fusion modeling method for shape−performance integrated digital twin of complex structure. Front. Mech. Eng., 2022, 17(4): 52 https://doi.org/10.1007/s11465-022-0708-0

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Nomenclature

Abbreviations
3D Three-dimensional
DT Digital twin
FEM Finite element method
KRG Kriging
M-LFM Multi-level fusion modeling
NMAE Normalized maximum absolute error
NRMSE Normalized root mean square error
PRS Polynomial response surface
RUL Remaining useful life
SNR Signal-to-noise ratios
SPI-DT Shape–performance integrated digital twin
Variables
aUnknown coefficient used to change the result size of the predicted model
A Amplitude of the signal
AnoiseAmplitude of the noise
b Scale factor
DfRemaining useful life
eError between the training value and the predicted value at training point
EElastic modulus,
fi(∙) (i = 1,2,…,m)Unknown approximate function
Fi (i = 1,2,…,5)Thrust produced by the hydraulic cylinder and the pulling force produced by the transmission chain
Ffi (i = 2,3,4)Fraction between segments
FForce vector
g gth cycle
H Vector whose elements are ones
kNumber of measured data
Kt Elastic stress concentration factor
L Cost function
m Number of input variables
Mg Total cycle number
M, C, K Mass matrix, damping matrix, and stiffness matrix, respectively
ng, Ng Cycle number in practical and cycles to failure, respectively
Nf Cycle number to failure
Nt Test point number
P Signal power
Pnoise Noise power
Q,Q˙,Q¨ Displacement, velocity, and acceleration vector, respectively
r Related vector between the unknown predicted point and the trained point
R Relationship function
R2 Coefficient of determination
R Relationship matrix whose elements are the value of relationship function
t Time
Ttest Measured data
ui, vi, wi Space coordinates in the ith point
uC, vC, wC Space coordinates in the compensation point
xi (i = 1,2,…,m) ith input variable
XInput vector
y¯ Mean value of the true output at all test points
y^ Predicted value of output variable
yitrain Response value in the ith training point
y^PRS Predicted data of PRS model
y^CPRS,y^CKRG Predicted values of the PRS model and KRG model at the compensation point, respectively
ys True response value at samples.
Y Output vector
YPRS,YKRG Predicted vectors of the PRS model and the KRG model, respectively
z() Error function of KRG model
Cfi (i = 1,2,…,n) Compensation factor of the influence domain
Cfmin, Cfmax Minimum and maximum values of the compensation factor set, respectively
Cfinor Normalized compensation factor
Cfnor Compensation factor set
αi (i = 1,2,…,m) Unknown weight coefficient
αiδ,αiu,αia Unknown weight coefficient of different parameters model
α Vector of unknown coefficients
β^ Maximum likelihood estimation value of hyper-parameter
βi Unknown weighted coefficients of the KRG model
δ Parameter of the influence domain
δ^,μ^,a^ Predicted values of the model parameters under different sensor states
δl,δuUpper and lower bounds of the parameter δ, respectively
δopt, μopt,aopt Optimal parameters of δ, μ, and a, respectively
ε Vector of error function
μ Deviation coefficient of the compensation point
μl,μuUpper and lower bounds of the parameter μ, respectively
ρi (i = 1,2,…,n) Euclidean distance between the compensation point and the surrounding points
ρmin, ρmaxMinimum and maximum values of the Euclidean distance set, respectively
ρinor Normalized Euclidean distance
σ2 Variance of error function
σaStress amplitude
σmMean stress
σy Tensile yield stress
σe(Soder)Modified mean stress
σPerformance vector
σs, σh Predicted stresses in the extension and retraction processes, respectively
σnomNominal stress range
ψi (x) Function correlated with the physical properties of problem itself
ψiδ(x), ψiu(x), ψia(x) Functions correlated with the physical properties of different PRS model

Acknowledgements

This work was supported by the National Key R&D Program of China (Grant No. 2018YFB1700704) and the National Natural Science Foundation of China (Grant No. 52075068).

Electronic Supplementary Materials

The supplementary materials can be found in the online version of this article at https://doi.org/10.1007/s11465-022-0708-0 and are accessible to authorized users.

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