Multi-task learning application for predicting impact damage-related information using surface profiles of CFRP laminates

被引:12
作者
Hasebe, Saki [1 ]
Higuchi, Ryo [1 ]
Yokozeki, Tomohiro [1 ]
Takeda, Shin-ichi [2 ]
机构
[1] Univ Tokyo, Dept Aeronaut & Astronaut, Bunkyo Ku, Tokyo 1138656, Japan
[2] Japan Aerosp Explorat Agcy JAXA, Aeronaut Technol Directorate, Mitaka, Tokyo 1810015, Japan
关键词
A; Carbon fiber; Laminate; B; Impact behavior; COMPOSITE; DELAMINATIONS;
D O I
10.1016/j.compscitech.2022.109820
中图分类号
TB33 [复合材料];
学科分类号
摘要
Impact damage prediction has been considered a critical issue for several years, especially in manufacturing or maintenance. Several researchers have been studying on impact detection or damage prediction on composite materials applying machine learning, a data driven analysis methodology. This study develops the decision tree based multi-task learning scheme for the prediction of impact damage information solely from an external surface profile. Multi-task learning enables effective learning; in other words, it can integrate the relationships among objective variables. Low-velocity impact tests and damage measurement were conducted to create the dataset and investigate the correlations between the impact damage and impact conditions. Using the features designed from the surface profile data, multi-task learning was applied to predict the impactor shape and delamination extent. By comparing the effectiveness of the proposed method and that of the original single -task learning method, it was inferred that the multi-task learning has advantages in the prediction accuracy and model plausibility, considering the impact phenomenon.
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页数:9
相关论文
共 30 条
[1]  
Abrate Serge., 1998, IMPACT COMPOSITE STR, DOI [10.1017/CBO9780511574504, DOI 10.1017/CBO9780511574504]
[2]  
[Anonymous], 2007, ASTM D7136
[3]   Machine Learning for industrial applications: A comprehensive literature review [J].
Bertolini, Massimo ;
Mezzogori, Davide ;
Neroni, Mattia ;
Zammori, Francesco .
EXPERT SYSTEMS WITH APPLICATIONS, 2021, 175
[4]  
Bouarfa S., 2020, AIAA SCITECH 2020 FO, P1
[5]   Low velocity impact modeling in composite laminates capturing permanent indentation [J].
Bouvet, C. ;
Rivallant, S. ;
Barrau, J. J. .
COMPOSITES SCIENCE AND TECHNOLOGY, 2012, 72 (16) :1977-1988
[6]   COMPARISON OF THE LOW AND HIGH-VELOCITY IMPACT RESPONSE OF CFRP [J].
CANTWELL, WJ ;
MORTON, J .
COMPOSITES, 1989, 20 (06) :545-551
[7]   Low velocity impact behavior of interlayer hybrid composite laminates with carbon/glass/basalt fibres [J].
Chen, Dongdong ;
Luo, Quantian ;
Meng, Maozhou ;
Li, Qing ;
Sun, Guangyong .
COMPOSITES PART B-ENGINEERING, 2019, 176
[8]   Impact on composite structures [J].
Davies, GAO ;
Olsson, R .
AERONAUTICAL JOURNAL, 2004, 108 (1089) :541-563
[9]   Dent depth visibility versus delamination damage for impact of composite panels by tips of varying radius [J].
Delaney, Mac P. ;
Fung, Sarah Y. K. ;
Kim, Hyonny .
JOURNAL OF COMPOSITE MATERIALS, 2018, 52 (19) :2691-2705
[10]   Energy-based approach to impact damage in CFRP laminates [J].
Delfosse, D ;
Poursartip, A .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 1997, 28 (07) :647-655