ARTICLE
Estimation of stress intensity factor for surface cracks in the firtree groove structure of turbine disk using pool-based active learning with Gaussian Process Regression
,
 
,
 
,
 
,
 
,
 
Xiaojun Yan 2,3,4
 
 
 
More details
Hide details
1
Research Institute of Aero-Engine, Beihang University, Beijing, China
 
2
School of Energy and Power Engineering, Beihang University, Beijing, China
 
3
Beijing Key Laboratory of Aero-Engine Structure and Strength, Beijing, China
 
4
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beijing, China
 
 
Submission date: 2023-08-08
 
 
Final revision date: 2023-09-08
 
 
Acceptance date: 2023-10-31
 
 
Online publication date: 2024-01-12
 
 
Publication date: 2024-01-31
 
 
Corresponding author
Dawei Huang   

School of Energy and Power Engineering, Beihang University, China
 
 
Journal of Theoretical and Applied Mechanics 2024;62(1):89-101
 
KEYWORDS
TOPICS
ABSTRACT
Calculation of the stress intensity factor K is a crucial and difficult task in linear elastic fracture mechanics. With the capacity to solve complex input-output problems of an underlying system, machine learning is especially useful in the calculation of K. However, when faced with complex systems, such as the firtree groove structure of a turbine disk, the dataconsuming issue has always been a thorny problem in K-solutions combined with machine learning studies for a long time. In this paper, a novel K-solution method called PA-GPR (Pool-based Active learning with Gaussian Process Regression) for the calculation of the stress intensity factor for surface cracks in the firtree groove structure of a turbine disk is proposed. Using the pool-based active learning strategy, the proposed K-solution method could make the GPR model have a great regression performance with a few samples required. In the pool-based active learning strategy analysis, the learning function based on greedy sampling is proposed to select samples with a high contribution to the training of the GPR model. The calculation of K for a semi-elliptical surface crack in the firtree groove structure is evaluated to verify the accuracy and effectiveness of the proposed method. The results show that this novel method is accurate, time-saving and effective.
 
REFERENCES (25)
1.
Basista M., Węglewski W., 2006, Modelling of damage and fracture in ceramic matrix composites-an overview, Journal of Theoretical and Applied Mechanics, 44, 3, 455-484.
 
2.
Boulenouar A., Benseddiq N., Mazari M., Benamara N., 2014, FE model for linear-elastic mixed mode loading: estimation of SIFs and crack propagation, Journal of Theoretical and Applied Mechanics, 52, 2, 373-383.
 
3.
Cui W., Wang J., 2011, Probabilistic analysis of gas turbine disk multi-crack propagation, Turbo Expo: Power for Land, Sea, and Air.
 
4.
Huang D., Yan X., Li P., Qin X., Zhang X., Qi M., Liu Z., 2018, Modeling of temperature influence on the fatigue crack growth behavior of superalloys, International Journal of Fatigue, 110, 22-30.
 
5.
Huang D., Yan X., Qin X., Zhang X., Qi M., Liu Z., Tao Z., 2019, Scatter in fatigue crack growth behavior of a Ni-base superalloy at high temperature, International Journal of Fatigue, 118, 1-7.
 
6.
Huang X., Chen C., Xuan H., 2021, Experimental and analytical investigation for fatigue crack growth characteristics of an aero-engine fan disc, International Journal of Fatigue, 148.
 
7.
Keprate A., Chandima Ratnayake R. M., Sankararaman S., 2017, Comparison of various surrogate models to predict stress intensity factor of a crack propagating in offshore piping, Journal of Offshore Mechanics and Arctic Engineering, 139, 6.
 
8.
Li P., Cheng L., Yan X., Huang D., Qin X., Zhang X., 2018, A temperature-dependent model for predicting the fracture toughness of superalloys at elevated temperature, Theoretical and Applied Fracture Mechanics, 93, 311-318.
 
9.
Li Y., Wang J., Guo W., Guo J., 2019, A modified model of residual strength prediction for metal plates with through-thickness cracks, Journal of Theoretical and Applied Mechanics, 57, 3, 537-547.
 
10.
Liu X., Athanasiou C.E., Padture N.P., Sheldon B.W., Gao H., 2020, A machine learning approach to fracture mechanics problems, Acta Materialia, 190, 105-112.
 
11.
Liu Y., Mahadevan S., 2009, Probabilistic fatigue life prediction using an equivalent initial flaw size distribution, International Journal of Fatigue, 31, 3, 476-487.
 
12.
Meguid S.A., Kanth P.S., Czekanski A., 2000, Finite element analysis of fir-tree region in turbine discs, Finite Elements in Analysis and Design, 35, 4, 305-317.
 
13.
Moustabchir H., Alaoui M.A.H., Babaoui A., Dearn K.D., Pruncu C.I., Azari Z., 2017, The influence of variations of geometrical parameters on the notching stress intensity factors of cylindrical shells, Journal of Theoretical and Applied Mechanics, 55, 2, 559-569.
 
14.
Moustabchir H., Arbaoui J., Zitouni A., Hariri S., Dmytrakh I., 2015, Numerical analysis of stress intensity factor and T-stress in pipeline of steel P264GH submitted to loading conditions, Journal of Theoretical and Applied Mechanics, 53, 3, 665-672.
 
15.
Muñoz-Abella B., Rubio L., Rubio P., 2015, Stress intensity factor estimation for unbalanced rotating cracked shafts by artificial neural networks, Fatigue and Fracture of Engineering Materials and Structures, 38, 3, 352-367.
 
16.
Newman Jr J., Raju I., 1981, Stress-intensity factor equations for cracks in three-dimensional finite bodies, ASTM National Symposium on Fracture Mechanics., DOI: 10.1520/stp37074s.
 
17.
Rasmussen C.E., 2003, Gaussian processes in machine learning, Summer School on Machine Learning, 63-71, Springer.
 
18.
Rinaldi A., Krajcinovic D., Mastilovic S., 2006, Statistical damage mechanics - constitutive relations, Journal of Theoretical and Applied Mechanics, 44, 3, 585-602.
 
19.
Shlyannikov V., Zakharov A., Yarullin R., 2016, Structural integrity assessment of turbine disk on a plastic stress intensity factor basis, International Journal of Fatigue, 92, 234-245.
 
20.
Witek L., 2012, Numerical simulation of fatigue fracture of the turbine disc, Fatigue of Aircraft Structures, 1, 4, 114-122.
 
21.
Wu D., Lin C.-T., Huang J., 2019, Active learning for regression using greedy sampling, Information Sciences, 474, 90-105.
 
22.
Xu T., Ding S., Zhou H., Li G., 2021, Machine learning-based efficient stress intensity factor calculation for aeroengine disk probabilistic risk assessment under polynomial stress fields, Fatigue and Fracture of Engineering Materials and Structures, 45, 2, 451-465.
 
23.
Yang F., Pan C., Zhang D., Tang J, Yan J., 2017, Stress distribution and deformation analysis of gas turbine blades and disk with FEM method, ASME Power Conference.
 
24.
Yu H., Kim S., 2010, Passive sampling for regression, 2010 IEEE International Conference on Data Mining.
 
25.
Yuan R., Liao D., Zhu S.P., Yu Z.Y., Correia J., De Jesus A., 2021, Contact stress analysis and fatigue life prediction of turbine disc-blade attachment with fir-tree tenon structure, Fatigue and Fracture of Engineering Materials and Structures, 44, 4, 1014-1026.
 
eISSN:2543-6309
ISSN:1429-2955
Journals System - logo
Scroll to top