低速冲击下FMLs、铝板和复合材料的损伤对比

doi:10.7527/S1000-6893.2013.0539

Abstract

Abstract:

In order to improve the damage tolerance and anti-impact properties of aircraft structures, fiber metal laminates (FMLs) developed in Europe are successfully applied in commercial aircraft structures. In this paper, drop-weight low-velocity impact tests are performed on FMLs which consist of 2024-T3 aluminium alloy sheets bonded together by glass fiber prepreg. For comparison purposes, similar tests are conducted on monolithic 2024-T3 sheets and F300 quasi-isotropic composite panels. The penetration energy of the FMLs shows respectively about 40% and 6 times higher than that of the 2024-T3 sheets and composite panels; and the back side crack length of the FMLs is 30%-50% shorter than that in the 2024-T3 sheets at the same level of impact energy. Finite element models are developed to simulate the impact response of the FMLs. Ductile and Hashin damage initiation criteria are used to simulate the aluminium and fiber failure mechanisms respectively. The dynamic response of the laminates is analyzed and the damage mode is summarized. The simulation results agree well with the experimental findings.

Key words: fiber metal laminate, low-velocity impact, crack length, dynamic response, damage evolution

CLC Number:

V214.8
TB333

MA Yu'e, HU Haiwei, XIONG Xiaofeng. Comparison of Damage in FMLs, Aluminium and Composite Panels Subjected to Low-velocity Impact[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2014, 35(7): 1902-1911.

References

[1] Schijve J. Development of fibre-mental laminates, arall and glare, new fatigue resistant materials, LR-715. Delft: Faculty of Aerospace Engineering, Delft University of Technology, 1993.

[2] Alaerliesten R C. Fatigue crack propagation and delamination growth in glare. Delft: Faculty of Aerospace Engineering, Delft University of Technology, 2005.

[3] Matthijs P. Crack closure in glare. Delft: Faculty of Aerospace Engineering, Delft University of Technology, 2005.

[4] Vlot A. Impact loading on fibre metal laminates[J]. International Journal of Impact Engineering, 1996, 18(3): 291-307.

[5] Vlot A, Krull M. Impact damage resistance of various fiber metal laminates//5th International Conference on Mechanical and Physical Behaviour of Materials Under Dynamic Loading, 1997: 1045-1050.

[6] Laliberte J F, Poon C, Straznicky P V, et al. Post-impact fatigue damage growth in fiber-metal laminates[J]. International Journal of Fatigue, 2002, 24(2-4): 249-256.

[7] Wu G, Yang J M, Thomas H H. The impact properties and damage tolerance and of bi-directionally reinforced fiber metal laminates[J]. Journal of Materials Science, 2007, 42(3): 948-957.

[8] Lawcock G D, Ye L, Mai Y W. Effects of fibre/matrix adhesion on carbon-fibre-reinforced mental laminates-Ⅱ, impact behaviour[J]. Composites Science and Technology, 1997, 57(12): 1621-1628.

[9] Caprino G, Spatarob G, DelLuongoa S. Low-velocity impact behavior of fiberglass-aluminum laminates[J]. Composites Part A: Applied Science and Manufacturing, 2004, 35(5): 605-616.

[10] Caprino G, Lopresto V, Iaccarino P. A simple mechanistic model to predict the macroscopic response of fiberglass-aluminum laminates under low-velocity impact[J]. Composites Part A: Applied Science and Manufacturing, 2007, 38(2): 290-300.

[11] Fan J Y, Guan Z W, Cantwell W J. Numerical modelling of perforation failure in fibre metal laminates subjected to low velocity impact loading[J]. Composite Structures, 2011, 93(9): 2430-2436.

[12] Hayato N, Tatsuro K, Katsuhiko O. Damage characterization of titanium/GFRP hybrid laminates subjected to low-velocity impact[J]. Composites Part A: Applied Science and Manufacturing, 2011, 42(7): 772-781.

[13] Sadighi M, Parnanen T, Alderliesten R C. Experimental and numerical investigation of metal type and thickness effects on the impact resistance of fiber metal laminates[J]. Applied Composite Materials, 2012, 19(3-4): 545-559.

[14] Wu X R, Guo Y J. Development of methodology for predicting fatigue life of fiber reinforced mental laminates[J]. Advances in Mechanics, 1999, 29(3): 304-316. (in Chinese) 吴学仁, 郭亚军. 纤维金属层板疲劳寿命预测的研究进展[J]. 力学进展, 1999, 29(3): 304-316.

[15] Liao J, Cao Z Q, Dai Y. The off-axis properties of glare plates[J]. Journal of Plasticity Engineering, 2007, 14(5): 67-70. (in Chinese) 廖建, 曹增强, 代瑛. GLARE层板偏轴拉伸性能[J]. 塑性工程学报, 2007, 14(5): 67-70.

[16] Zheng C L, Zhu G Z, Liu W B. Investigation into the tension properties of carbon fiber reinforced magnesium alloy laminates[J]. Journal of Materials Engineering, 2007(S1): 148-150. (in Chinese) 郑长良, 朱公志, 刘文博. 碳纤维增强镁合金层合板及其基本力学性能[J]. 材料工程, 2007(S1): 148-150.

[17] Fan Y, Liu W B, Wang R. Preparation and properties research of AI/CF/TDE85 laminate//15th National Conference on Composite Materials Academic. Harbin: Institute of Composite Material and Structure, Harbin Industrial University, 2008: 691-694. (in Chinese) 樊玉, 刘文博, 王荣. AI/CF/TDE85复合层合板的制备及性能研究//第十五届全国复合材料学术会议论文集. 哈尔滨: 哈尔滨工业大学复合材料与结构研究所, 2008: 691-694.

[18] Cheng Y F, Li Y L, Liu J, et al. Study of bird strike on an improved leading edge structure[J]. Acta Aeronautica et Astronautica Sinica, 2010, 31(9): 1781-1787. (in Chinese) 陈园方, 李玉龙, 刘军, 等.典型前缘结构抗鸟撞性能改进研究[J]. 航空学报, 2010, 31(9): 1781-1787.

[19] ASTM Committee. ASTM D 7136/D 7136M-05 Standard test method for measuring the damage resistance of a fiber-reinforced polymer matrix composite to a drop-weight impact event[S]. United States: ASTM International, 2005: 1-16.

[20] Hoopura H, Gese H, Dell H, et al. A comprehensive failure model for crashworthiness simulation of aluminium extrusions[J]. International Journal of Crashworthiness, 2004, 9(5): 449-464.

[21] Hillerborg A, Modeer M, Petersson P E. Analysis of crack formation and crack growth in concrete by means of fracture mechanics and finite elements[J]. Cement and Concrete Research, 1976, 6(6): 773-782.

[22] Hashin Z. Failure criteria for unidirectional fiber composites[J]. Journal of Applied Mechanics, 1980, 47(2): 329-334.

Comparison of Damage in FMLs, Aluminium and Composite Panels Subjected to Low-velocity Impact

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	DENG Yunfei, ZHOU Nan, TIAN Rui, WEI Gang. Response characteristics of sandwich structure with S-shaped CFRP folded core under low velocity impact [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(6): 525446-525446.
[2]	ZHAO Xiaojian, SHAO Xiao, YANG Mingsui. Equivalence of vibro-acoustic response based on scaled thin-walled structures [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 225146-225146.
[3]	FENG Zhenyu, LIU Xu, LIN Lanhui, YANG Yongpan, XIE Jiang, SHI Xiaopeng, XIAO Pei, LI Leizi, YI Pengfei, LIU Xiaochuan, BAI Chunyu. Impact of seatbelts on impact characteristics of aviation seats and occupants [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(1): 224808-224808.
[4]	CAO Qikai, WANG Yan, YAO Niankui, HE Gang, CHEN Zhongming, ZHANG Guijiang, TIAN Zhiliang, WU Xinyue. Development and application of strength design technology of advanced carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(8): 525793-525793.
[5]	WU Zhihui, NIU Gongjie, QIAN Jianping, LIU Rongzhong. Thermodynamics-based damage constitutive model and its application to damage analysis for HTPB/AP composite base bleed grain [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(3): 223855-223855.
[6]	GUO Yidong, MA Yu'e, LI Peiyao. Low velocity impact response of additively manufactured titanium alloy micro-truss sandwich panels [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 423820-423820.
[7]	SHEN Gaofeng, WANG Zhenjun, LIU Fenghua, ZHANG Yingfeng, CAI Changchun, XU Zhifeng, YU Huan. Quasi-static tensile behavior and failure mechanism of laminated puncture CF/Al composites [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(12): 424816-424816.
[8]	ZHAO Yanqin, CHEN Renliang. Systematical modelling of low-altitude windshear and its qualitative threat analysis to helicopter flight safety [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(7): 123413-123413.
[9]	CUI Wenbin, CHEN Xuan, CHEN Chao, CHENG Li, DING Junliang, ZHANG Hui. Damage evolution process of CFRP in very high cycle fatigue [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(1): 223212-223212.
[10]	DU Maohua, CHENG Zheng, WANG Shensong, ZHANG Yanfei. Effects of damage evolution on simulation results of high speed machining of Ti6Al4V [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(7): 422787-422787.
[11]	HE Min, ZHU Xiaolong, LIU Xiaoming, LIU Fan, YAO Xiaohu. Impact response of ground ejection of front fuselage structure of carrier-based aircraft [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(5): 221711-221711.
[12]	CHEN Shangjun, QIN Qinghua, ZHANG Wei, XIA Yuanming, YU Xuehui, ZHANG Jianxun, WANG Binwen, WANG Tiejun. Experimental investigation on against penetration of metallic honeycomb sandwich plates under low-velocity impact [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(2): 221483-221483.
[13]	ZOU Xuefeng, GUO Dingwen, PAN Kai, QU Chao, TAO Yongqiang, ZHANG Xudong. Test technique for multi-load combined strength of hypersonic vehicle structure under complex loading environment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(12): 222326-222326.
[14]	XUE Shuaijie, LIU Hongjun, HONG Liu, CHEN Pengfei. Experimental on dynamic characteristics of an open-end swirl injector with thick liquid film [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(12): 122534-122534.
[15]	FANG Xingbo, NIE Hong, ZHANG Zhao, WEI Xiaohui, ZHANG Ming. Dynamic response analysis on carrier-based UAV considering catapult shuttle mass [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2018, 39(12): 222237-222237.