Effect of Cycling Low Velocity Impact on Mechanical and Wear Properties of CFRP Laminate Composites

Yang Sun; Zhen-Bing Cai; Song-Bo Wu; Jian-Hua Liu; Jia-Xin Yu

doi:10.1186/s10033-018-0305-7

Chinese Journal of Mechanical Engineering >

2018 , Vol. 31 >Issue 6: 112 - 112

DOI: https://doi.org/10.1186/s10033-018-0305-7

Mechanism and Robotics

Effect of Cycling Low Velocity Impact on Mechanical and Wear Properties of CFRP Laminate Composites

Yang Sun ,
Zhen-Bing Cai ,
Song-Bo Wu ,
Jian-Hua Liu ,
Jia-Xin Yu

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1. Tribology Research Institute, Key Lab of Advanced Technologies of Materials, Southwest Jiaotong University, Chengdu 610031, China;
2. Key Laboratory of Testing Technology for Manufacturing Process of Ministry of Education, Southwest University of Science and Technology, Mianyang 621010, China

Received date: 2018-02-03

Online published: 2019-07-23

Supported by

Supported by National Natural Science Foundation of China (Grant Nos. U1530136, 51627806), Young Scientifc Innovation Team of Science and Technology of Sichuan Province of China (Grant No. 2017TD0017), and Opening Project of Key Laboratory of Testing Technology for Manufacturing Process of China (Grant Nos. 2016-01, Southwest University of Science and Technology)

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Abstract

The mechanical and wear properties of CFRP laminate were investigated using a method of cycling low velocity impact, to study the trend and mechanism of impact resistance of the CFRP laminate under repeated impact during its service process. The interface responses of CFRP laminate under different impact kinetic energy during the cycling impact process were studied were studied experimentally, such as impact contact duration, deformation and energy absorption. The worn surface morphologies were observed through optical microscopy and a 3-D surface profiler and the cross-sectional morphologies were observed through SEM to investigate the mechanism of impact material damage. Based on a single-degree-of-freedom damping vibration model, the normal contact stiffness and contact damping of the material in different wear stages were calculated. It shows the failure process of CFRP laminate damaged by accumulated absorption energy under the cycling impact of different initial kinetic energy. The results indicate that the stiffness and damping coefficients will change at different impact velocities or cycle numbers. The damage mechanism of CFRP laminates under cycling low kinetic energy is delamination. After repeated experiments, it was found that there was a threshold value for the accumulated absorption energy before the failure of the CFRP laminate.

Key words： CFRP laminate; Low velocity impact; Impact resistance; Accumulated absorption energy threshold; Delamination

Cite this article

Yang Sun , Zhen-Bing Cai , Song-Bo Wu , Jian-Hua Liu , Jia-Xin Yu . Effect of Cycling Low Velocity Impact on Mechanical and Wear Properties of CFRP Laminate Composites[J]. Chinese Journal of Mechanical Engineering, 2018 , 31(6) : 112 -112 . DOI: 10.1186/s10033-018-0305-7

References

[1] F Schäfer, R Destefanis, S Ryan, et al. Hypervelocity impact testing of CFRP/Al honeycomb satellite structures. In:4th European Conference on Space Debris, 2005, 587:407.
[2] Y Miyano, M Nakada, K Nishigaki. Prediction of long-term fatigue life of quasi-isotropic CFRP laminates for aircraft use. Int. J. Fatigue, 2006, 28(10):1217-1225.
[3] J R Duflou, J De Moor, I Verpoest, et al. Environmental impact analysis of composite use in car manufacturing. CIRP Ann. Manuf. Techn., 2009; 58(1):9-12.
[4] W X Wang, T Matsubara, J Hu, et al. Experimental investigation into the influence of the flanged diffuser on the dynamic behavior of CFRP blade of a shrouded wind turbine. Renew Energy, 2015, 78:386-397.
[5] J López-Puente, R Zaera, C Navarro. The effect of low temperatures on the intermediate and high velocity impact response of CFRPs. Compos. Part B-Eng., 2002, 33(8):559-566.
[6] D D R Cartie, P E Irving. Effect of resin and fibre properties on impact and compression after impact performance of CFRP. Compos. Part A-Appl. S., 2002, 33(4):483-493.
[7] A Kim, I Kim. Solid particle erosion of CFRP composite with different laminate orientations. Wear, 2009, 267(11):1922-1926.
[8] X Xie, Y F Zhu, Y G Shen. Study on vibration of long-span cable-stayed bridge with steel and CFRP cables due to moving vehicles. Eng. Mech., 2007, 24:53-61.
[9] M Wicklein, S Ryan, D M White, et al. Hypervelocity impact on CFRP:testing, material modelling, and numerical simulation. Int. J. Impact Eng., 2008, 35(12):1861-1869.
[10] S Ryan, F Schaefer, W Riedel. Numerical simulation of hypervelocity impact on CFRP/Al HC SP spacecraft structures causing penetration and fragment ejection. Int. J. Impact Eng., 2006, 33(1):703-712.
[11] K Iqbal, S U Khan, A Munir, et al. Impact damage resistance of CFRP with nanoclay-filled epoxy matrix. Compos. Sci. Technol., 2009, 69(11):1949-1957.
[12] S Heimbs, S Heller, P Middendorf, et al. Low velocity impact on CFRP plates with compressive preload:Test and modelling. Int. J. Impact Eng., 2009, 36(10):1182-1193.
[13] P Gao, X Gu, A S Mosallam. Flexural behavior of preloaded reinforced concrete beams strengthened by prestressed CFRP laminates. Compos. Struct., 2016, 157:33-50.
[14] N Korneeva, V Kudinov, I Krylov, et al. Properties of fiber reinforced plastics under static and dynamic loading conditions. Polym. Eng. Sci., 2017, 57(7):693-696.
[15] S Genna, C Leone, N Ucciardello, et al. Increasing adhesive bonding of carbon fiber reinforced thermoplastic matrix by laser surface treatment. Polym. Eng. Sci., 2017, 57(7):658-692.
[16] D Feng, F Aymerich. Finite element modelling of damage induced by low-velocity impact on composite laminates. Compos. Struct., 2014, 108:161-171.
[17] Y T Obaidat, S Heyden, O Dahlblom. The effect of CFRP and CFRP/concrete interface models when modelling retrofitted RC beams with FEM. Compos. Struct., 2010, 92(6):1391-1398.
[18] Y He, G Tian, M Pan, et al. Impact evaluation in carbon fiber reinforced plastic (CFRP) laminates using eddy current pulsed thermography. Compos. Struct., 2014, 109:1-7.
[19] Y He, R Yang, H Zhang, et al. Volume or inside heating thermography using electromagnetic excitation for advanced composite materials. Int. J. Therm. Sci., 2017:41-49.
[20] Y He, R Yang. Eddy current volume heating thermography and phase analysis for imaging characterization of interface delamination in CFRP. IEEE T. Ind. Inform., 2015, 11(6):1287-1297.
[21] Y Petronyuk, E Morokov, V Levin, et al. Study of failure mechanisms of CFRP under mechanical load by impulse acoustic microscopy. Polym. Eng. Sci., 2017, 57(7):703-708.
[22] S Boccardi, G M Carlomagno, N D Boffa, et al. Infrared thermography to locate impact damage in thin and thicker carbon/epoxy panels. Polym. Eng. Sci., 2017, 57(7):657-664.
[23] B W Jang, S O Park, Y G Lee, et al. Detection of impact damage in composite structures using high speed FBG interrogator. Adv. Compos. Mater., 2012, 21(1):29-44.
[24] B W Jang, Y G Lee, C G Kim, et al. Impact source localization for composite structures under external dynamic loading condition. Adv. Compos. Mater., 2015, 24(4):359-374.
[25] B W Jang, C G Kim. Impact localization on a composite stiffened panel using reference signals with efficient training process. Compos. Part B-Eng., 2016, 94:271-285.
[26] B W Jang, C G Kim. Real-time detection of low-velocity impact-induced delamination onset in composite laminates for efficient management of structural health. Compos. Part B-Eng., 2017, 123(15):124-135.
[27] R Palazzetti, A Zucchelli, I Trendafilova. The self-reinforcing effect of Nylon 6, 6 nano-fibres on CFRP laminates subjected to low velocity impact. Compos. Struct., 2013, 106:661-671.
[28] R Palazzetti, A Zucchelli, C Gualandi, et al. Influence of electrospun Nylon 6, 6 nanofibrous mats on the interlaminar properties of Gr-epoxy composite laminate. Compos. Struct., 2012, 94(2):571-579.
[29] R Palazzetti, X Yan, A Zucchelli. Influence of geometrical features of electrospun nylon 6, 6 interleave on the CFRP laminates mechanical properties. Polym. Composite, 2014, 35(1):137-150.
[30] H Saghafi, A Zucchelli, R Palazzetti, et al. The effect of interleaved composite nanofibrous mats on delamination behavior of polymeric composite materials. Compos. Struct., 2014, 109:41-47.
[31] H Saito, M Morita, K Kawabe, et al. Effect of ply-thickness on impact damage morphology in CFRP laminates. J. Reinf. Plast. Comp., 2011, 30(13):1097-1106.
[32] Y Aoki, K Yamada, T Ishikawa. Effect of hygrothermal condition on compression after impact strength of CFRP laminates. Compos. Sci. Technol., 2008, 68(6):1376-1383.
[33] K Morioka, Y Tomita. Effect of lay-up sequences on mechanical properties and fracture behavior of CFRP laminate composites. Mater. Charact., 2000, 45(2):125-136.
[34] M Masoumi, I F de Barros, L F G Herculano, et al. Effect of microstructure and crystallographic texture on the Charpy impact test for maraging 300 steel. Mater. Charact., 2016, 120:203-209.
[35] Y T Tsai, H T Chang, B M Huang, et al. Microstructural characterization of Charpy-impact-tested nanostructured bainite. Mater. Charact., 2015, 107:63-69.
[36] Z Cai, Z Chen, H Qian, et al. Impact fretting wear behavior of 304 stainless steel thin-walled tubes under low-velocity. Tribol. Int., 2017, 105:219-228.
[37] Y Lin, Z Cai, Z Chen, et al. Influence of diameter-thickness ratio on alloy Zr-4 tube under low-energy impact fretting wear. Materials Today Communications, 2016, 8:79-90.
[38] Y Sun, Z Cai, Z Chen, et al. Impact fretting wear of Inconel 690 tube with different supporting structure under cycling low kinetic energy. Wear, 2017, 376:625-633.

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