Evaluation of Compression after Impact on Composite Laminates Coated with PU

doi:10.11901/1005.3093.2016.588

Chinese Journal of Materials Research

2017, Vol. 31

Issue (7): 526-536 DOI: 10.11901/1005.3093.2016.588

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Evaluation of Compression after Impact on Composite Laminates Coated with PU

Ruiyan GUO¹, Guoli ZHANG¹(

), Hailiang YUE¹, Huan MA¹, Lianyun CHEN²

1 Key Laboratory of Advanced Textile Composites, Tianjin and Ministry of Education, Tianjin Polytechnic University, Tianjin 300387, China
2 AVIC Aerospace Life Support Industries, LED, Xiangyang, 441003, China

Cite this article:

Ruiyan GUO, Guoli ZHANG, Hailiang YUE, Huan MA, Lianyun CHEN. Evaluation of Compression after Impact on Composite Laminates Coated with PU. Chinese Journal of Materials Research, 2017, 31(7): 526-536.

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Abstract

The tests of repeated low-velocity impact and compression after impact on composites laminates coated with PU were carried out, and mainly focused on the factors of damage degree ,the thickness of composites and coating which could affect the compression strength after impact of composite laminates coated with PU. Moreover the process of compression after impact acting on laminated was tested via digital image correlation (DIC) which can gather the topography of specimens during testing in time, so the damage process and damage modes of specimens with various damage degrees were analyzed. Finally, the conclusions can be acquired：The damage inflection point exists by the increasing of impact numbers, and the compression strength decreased with increasing the thickness of composite laminates. In addition, the compression strength after impact of composite laminates coated with PU increased with increasing coating thickness. As for the specific damage position of different specimens, it is related with damage degree, which is also related with compression damage process.

Key words: composite polyurethane coating composite laminates thickness compression strength after impact damage inflection point compression damage mode

Received: 10 October 2016

ZTFLH:

TB332

Fund: Supported by the Planned Science and Technology Project of Tianjin (No. 16YFZCGX00190) and Tianjin City High School Science & Technology Fund Planning Project (No. 290ZD02)

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	Ruiyan GUO
	Guoli ZHANG
	Hailiang YUE
	Huan MA
	Lianyun CHEN

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https://www.cjmr.org/EN/10.11901/1005.3093.2016.588 OR https://www.cjmr.org/EN/Y2017/V31/I7/526

Table 1 Structure parameters of specimen

Fig.1 Testing facility for CAI (a) ARAMIS testing system and (b) universal testing machine

Fig.2 Schematic diagram of fixture (a) and the test diagram (b) of CAI

Fig.3 Comparison of specimen before (a) and after (b) spraying spot dealing

Fig.4 C-scan images of damage progression of repeatedly impacted on [0/90]₇ (a) and [0/90]₇-PU (b)

Fig.5 Load-deflection curves for CAI of [0/90]₇-PU (a) and [0/90]₇ (b) on different impact number

Fig.6 Compression stress-damage area curve after different impact number

Fig.7 Fracture load and compression strength of different structure laminates on different damage stage

Fig.8 Decline degree of CAI of laminates with different structure

Fig.9 Compression load-deflection curve of composite with different thickness of PU at penetration

Fig.10 Peak load (a) and compression strength (b) of laminates with different thickness of PU at different stage

Fig.11 The decline degree of laminates compared with impact before

Fig.12 Damage picture of specimen at matrix crack (a), at damage inflexion (b) and at penetration (c)

Fig.13 Strain distribution nephogram of specimen without impact in the compression process

Fig.14 Strain distribution nephogram of specimen without matrix crack in the compression process

Fig.15 Strain distribution nephogram of specimen after penetration in the compression process

[1]	Du S Y.Advanced composite materials and aerospace engineering[J]. Acta Mater. Compos. Sin., 2007, 24(1): 1(杜善义. 先进复合材料与航空航天[J]. 复合材料学报, 2007, 24(1): 1)
[2]	de Morais W A, Monteiro S N, d'Almeida J R M. Effect of the laminate thickness on the composite strength to repeated low energy impacts[J]. Compos. Struct., 2005, 70: 223
[3]	Aurrekoetxea J, Sarrionandia M, Mateos M, et al.Repeated low energy impact behaviour of self-reinforced polypropylene composites[J]. Polym. Test., 2011, 30: 216
[4]	Li J G.Composite material compression test after impact[J]. Fiber Compos., 2013, 30(2): 34(李建国. 复合材料冲击后压缩强度试验[J]. 纤维复合材料, 2013, 30(2): 34)
[5]	Andrew J J, Arumugam V, Saravanakumar K, et al.Compression after impact strength of repaired GFRP composite laminates under repeated impact loading[J]. Compos. Struct., 2015, 133: 911
[6]	Tooski M Y, Alderliesten R C, Ghajar R, et al.Experimental investigation on distance effects in repeated low velocity impact on fiber-metal laminates[J]. Compos. Struct., 2013, 99: 31
[7]	Adams D F, Zimmerman R S.Static and impact performance of polyethylene fiber/graphite fiber hybrid composites[J]. SAMPE J., 1986, 22: 10
[8]	Hart W G J, Ubels L C. Impact energy absorbing surface layers for protection of composite aircraft structures [A]. Proceedings of the 8th European Conference on Composite Materials:Science, Technologies and Applications [C]. Naples, Italy: Woodhead Publishing, Ltd, 1998
[9]	Düring D, Wei? L, Stefaniak D, et al.Low-velocity impact response of composite laminates with steel and elastomer protective layer[J]. Compos. Struct., 2015, 134: 18
[10]	Stelldinger E, Kühhorn A, Kober M.Experimental evaluation of the low-velocity impact damage resistance of CFRP tubes with integrated rubber layer[J]. Compos. Struct., 2016, 139: 30
[11]	Martins R D,Donadon M V,de Almeida S F M. The effects of curvature and internal pressure on the compression-after-impact strength of composite laminates[J]. J. Compos. Mater., 2016, 50: 825
[12]	Zhang Y.Testing and data analysis of laminates subjected to quasi-static indentation and compressive ultimate loads[J]. Fail. Anal. Prev., 2014, 9(1): 15(张颖. 层合板静压痕及压缩强度试验与其数据统计分析[J]. 失效分析与预防, 2014, 9(1): 15)
[13]	Cheng X Q, Li Z N.Damage progressive model of compression of composite laminates after low velocity impact[J]. Appl. Math. Mech., 2005, 26: 569(程小全, 郦正能. 复合材料层合板低速冲击后压缩的损伤累积模型[J]. 应用数学和力学, 2005, 26: 569)
[14]	Petit S, Bouvet C, Bergerot A, et al.Impact and compression after impact experimental study of a composite laminate with a cork thermal shield[J]. Compos. Sci. Technol., 2007, 67: 3286
[15]	Rahmé P, Bouvet C, Rivallant S, et al.Experimental investigation of impact on composite laminates with protective layers[J]. Compos. Sci. Technol., 2012, 72: 182
[16]	Nettles A T, Jackson J R, Hodge A J.Change in damage tolerance characteristics of sandwich structure with a thermal protection system (TPS)[J]. J. Compos. Mater., 2012, 46: 211
[17]	He W, Guan Z D, Wang J.Experimental study on the low-velocity impact and compression after impact performances of composite laminates with a surface protection layer[J]. Acta Mater. Compos. Sin., 2014, 31: 485(何为, 关志东, 王进. 带表面防护层复合材料层板的低速冲击及冲击后压缩性能试验研究[J]. 复合材料学报, 2014, 31: 485)

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