Interfacial fatigue performance of hybrid titanium to composite joints reinforced with 3D printed pins

被引:1
作者
Bagnato, Tiana [1 ]
Ravindran, Anil R. [2 ]
Orifici, Adrian C. [1 ]
Kandare, Everson [1 ]
Ladani, Raj B. [1 ]
机构
[1] RMIT Univ, Sch Engn, GPO Box 2476, Melbourne, Vic 3001, Australia
[2] Univ Sydney, Sch Psychol, Camperdown, NSW 2050, Australia
关键词
Fatigue; Fracture toughness; Joints/Joining; 3D printing; EPOXY NANOCOMPOSITES; METAL; STRENGTH; BEHAVIOR; RESISTANCE; FRACTURE; DESIGN;
D O I
10.1016/j.compositesa.2025.108984
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Titanium micro-pins have been reported to enhance the modes I and II interlaminar fracture toughness of titanium-to-composite joints. In this study, we examined the enhancement of modes I and II interlaminar fatigue crack growth resistance of titanium-to-composite joints using 3D printed titanium micro-pins created using selective laser melting (SLM). The joints were formed by printing an orthogonal array of thin (1.0 mm diameter) titanium micro-pins over the titanium substrate using SLM, which were then embedded into a carbon-epoxy composite substrate to create a micro-pin reinforced bondline interface. Interlaminar fatigue experiments were conducted under cyclic displacement control conditions using the Double Cantilever Beam (DCB) and End Notch Flexure (ENF) test methods. Under modes I and II cyclic loading, pinned joints exhibited significantly higher strain energy release rates for equivalent crack growth rates due to the micro-pins forming a crack bridging zone behind the crack tip, enhancing fatigue crack growth resistance compared to unpinned joints. The micro-pins increased the modes I and II cyclic critical strain energy release rate value by 18-fold and 4-fold, respectively. A single micro-pin cyclic testing was also performed to investigate the efficacy of the SLM Ti-pins for generating bridging traction loads under fatigue loading. The fatigue test results are presented together with fractographic evidence of the fatigue strengthening and toughening mechanisms.
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页数:18
相关论文
共 47 条
[1]   Improving the delamination fatigue resistance of composites by 3D woven metal and composite Z-filaments [J].
Abbasi, S. ;
Ladani, R. B. ;
Wang, C. H. ;
Mouritz, A. P. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2021, 147
[2]   A Review of the As-Built SLM Ti-6Al-4V Mechanical Properties towards Achieving Fatigue Resistant Designs [J].
Agius, Dylan ;
Kourousis, Kyriakos I. ;
Wallbrink, Chris .
METALS, 2018, 8 (01)
[3]  
Alan Baker S. D., 2004, Composite materials for aircraft structures, VSecond
[4]  
[Anonymous], 2001, Fatigue
[5]  
[Anonymous], 2009, ISO 25217:2009
[6]   Superior interfacial toughening of hybrid metal-composite structural joints using 3D printed pins [J].
Bagnato, Tiana ;
Ravindran, Anil R. ;
Mirabedini, Azadeh ;
Ladani, Raj B. ;
Kandare, Everson ;
Orifici, Adrian C. ;
Chang, Paul ;
Wang, John ;
Mouritz, Adrian P. .
COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2023, 168
[7]   Static and Fatigue Characteristics of Pinned Metal-Composite Joints [J].
Beketova, G. ;
Shevtsova, M. ;
Symonov, V. .
MECHANICS OF COMPOSITE MATERIALS, 2019, 55 (05) :655-666
[8]   Increasing the fatigue resistance of epoxy nanocomposites by aligning graphene nanoplatelets [J].
Bhasin, Mukesh ;
Wu, Shuying ;
Ladani, Raj B. ;
Kinloch, Anthony J. ;
Wang, Chun H. ;
Mouritz, Adrian P. .
INTERNATIONAL JOURNAL OF FATIGUE, 2018, 113 :88-97
[9]   Hybrid bonded-fastened joints and their application in composite structures: A general review [J].
Bodjona, Kobye ;
Lessard, Larry .
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 2016, 35 (09) :764-781
[10]   High-value SLM aerospace components: From design to manufacture [J].
Brandt, M. ;
Sun, S. ;
Leary, M. ;
Feih, S. ;
Elambasseril, J. ;
Liu, Q. .
Advanced Materials Research, 2013, 633 :135-147