ACTA AERONAUTICAET ASTRONAUTICA SINICA >
High⁃velocity impact performance of thin⁃ply carbon fiber/ ultra⁃thin stainless⁃steel strips fiber metal laminates
Received date: 2023-08-09
Revised date: 2023-10-08
Accepted date: 2023-11-13
Online published: 2023-11-22
Supported by
National Natural Science Foundation of China(51974196);Key Program of Joint Funds of the National Natural Science Foundation of China(U22A20188);Major Science and Technology Project of Shanxi Province(202101120401008);Youth Foundation for Basic Research of Shanxi Province(20210302124691)
To increase the toughness and high-velocity impact performance of carbon fiber composites, a new type of fiber metal laminates—thin-ply Carbon fiber/Ultra-thin Stainless-steel strips Fiber Metal Laminates (CUSFML) was proposed, which consisted of 30 μm thick thin-ply carbon fiber prepreg and 50 μm thick ultra-thin stainless-steel strips. Three types of thin-ply CUSFML were prepared in the range of Metal Volume Fraction (MVF) from 0.250 to 0.625. The high-velocity impact experiments of the pure carbon fiber laminates and three types of thin-ply CUSFML were carried out in the velocity range of 45–120 m/s by using an air gun. Moreover, the high-velocity impact responses of thin-ply CUSFML were also numerically simulated in ABAQUS/Explicit combined with the modified 3D Hashin failure criteria. The influence of MVF values on the dynamic response characteristics and energy absorption of thin-ply CUSFML under high-velocity impact was systematically analyzed. The results show that the high-velocity impact performance of thin-ply CUSFML can be significantly improved compared with that of traditional carbon fiber laminates. Through experimental data analysis and numerical calculation, the maximum specific absorption energy of prepared thin-ply CUSFML can reach 8.51 J·m2/kg, which is 19.2% higher than that of pure carbon fiber laminates. The impact load can reach up to 6 713 N, about 2.5 times that of pure carbon fiber laminates.Results also show that increasing the volume content of ultra-thin stainless-steel strips in the thin-ply CUSFML in a certain range could enhance the leading role of plastic deformation of the metal layer and fracture in the energy absorption mechanism, and improve the high-velocity impact performance of the laminates. However, with the continuous increase of MVF value, the specific energy absorption of thin-ply CUSFML would decrease slightly. After comparing the dynamic response characteristics of various laminates, it is found that the thin-ply CUSFML have the best impact resistance and energy absorption performance near MVF of 0.455.
Shibo WEI , Hongji SHU , Xiaoqiong ZHANG , Tingting ZHAO , Tao WANG , Zhihua WANG , Qingxue HUANG . High⁃velocity impact performance of thin⁃ply carbon fiber/ ultra⁃thin stainless⁃steel strips fiber metal laminates[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2024 , 45(14) : 429420 -429420 . DOI: 10.7527/S1000-6893.2023.29420
1 | CHAI G B, MANIKANDAN P. Low velocity impact response of fibre-metal laminates—A review[J]. Composite Structures, 2014, 107: 363-381. |
2 | 佟安时, 谢里阳, 白恩军, 等. 纤维金属层板的静力学性能测试与预测模型[J]. 航空学报, 2017, 38(11): 221193. |
TONG A S, XIE L Y, BAI E J, et al. Test and prediction model of statics property of fiber metal laminates[J]. Acta Aeronautica et Astronautica Sinica, 2017, 38(11): 221193 (in Chinese). | |
3 | VLOT A, ALDERLIESTEN R C, HOOIJMEIJER P A, et al. Fibre metal laminates: A state of the art[J]. International Journal of Materials and Product Technology, 2002, 17(1-2): 79-98. |
4 | 陈勇, 廖高健, 任立海, 等. 玻璃纤维增强铝合金层板高速冲击损伤容限[J]. 航空学报, 2018, 39(7): 221733. |
CHEN Y, LIAO G J, REN L H, et al. Damage tolerance of GLARE laminates subjected to high-velocity impact[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(7): 221733 (in Chinese). | |
5 | BANAT D, MANIA R J. Damage analysis of thin-walled GLARE members under axial compression-Numerical and experiment investigations[J]. Composite Structures, 2020, 241: 112102. |
6 | KHAN S H, SHARMA A P, KITEY R, et al. Effect of metal layer placement on the damage and energy absorption mechanisms in aluminium/glass fibre laminates[J]. International Journal of Impact Engineering, 2018, 119: 14-25. |
7 | HU C Z, SANG L, JIANG K, et al. Experimental and numerical characterization of flexural properties and failure behavior of CFRP/Al laminates[J]. Composite Structures, 2022, 281: 115036. |
8 | NAKATANI H, KOSAKA T, OSAKA K, et al. 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. |
9 | 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. |
CHEN 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). | |
10 | LEE D W, PARK B J, PARK S Y, et al. Fabrication of high-stiffness fiber-metal laminates and study of their behavior under low-velocity impact loadings[J]. Composite Structures, 2018, 189: 61-69. |
11 | K?TTER B, YAMADA K, K?RBELIN J, et al. Steel foil reinforcement for high performance bearing strength inThin-Ply composites [J]. Composites Part C: Open Access, 2021, 4: 085-100. |
12 | P?RN?NEN T, KANERVA M, SARLIN E, et al. Debonding and impact damage in stainless steel fibre metal laminates prior to metal fracture[J]. Composite Structures, 2015, 119: 777-786. |
13 | LIU C, YANG G L, XIAO Y, et al. Experimental and numerical investigation on the impact resistance of fiber metal laminates[J]. Vibroengineering Procedia, 2021, 36: 78-82. |
14 | PATELM, PATELS, AHMADS. Blast analysis of efficient honeycomb sandwich structures with CFRP/Steel FML skins[J]. International Journal of Impact Engineering, 2023, 178: 104609. |
15 | LU F, ZHONG Q P, CAO C X, et al. Galvanic corrosion and protection of GECM/LY12CZ couples under different atmospheric exposure conditions[J]. Acta Metallurgica Sinica (English Letters), 2003, 16(1): 41-45. |
16 | 吴国清, 潘英才, 张宗科, 等. 超轻纤维金属层合板的研究进展[J]. 航空制造技术, 2016, 59(S2): 133-136. |
WU G Q, PAN Y C, ZHANG Z K, et al. Research progress of ultra-light fiber metal laminates[J]. Aeronautical Manufacturing Technology, 2016, 59(S2): 133-136 (in Chinese). | |
17 | 曹勇, 张超. 薄层复合材料冲击损伤行为研究进展[J]. 航空学报, 2022, 43(6): 525323. |
CAO Y, ZHANG C. Impact damage behavior of thin-ply composites: A review[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(6): 525323 (in Chinese). | |
18 | JAKUBCZAK P, BIENIA? J, DADEJ K. Experimental and numerical investigation into the impact resistance of aluminium carbon laminates[J]. Composite Structures, 2020, 244: 112319. |
19 | 赵天, 李营, 张超, 等. 高性能航空复合材料结构的关键力学问题研究进展[J]. 航空学报, 2022, 43(6): 526851. |
ZHAO T, LI Y, ZHANG C, et al. Fundamental mechanical problems in high-performance aerospace composite structures: State-of-art review[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(6): 526851 (in Chinese). | |
20 | SHARMA A P, VELMURUGAN R, SHANKAR K, et al. High-velocity impact response of titanium-based fiber metal laminates. Part I: Experimental investigations[J]. International Journal of Impact Engineering, 2021, 152: 103845. |
21 | SHARMA A P, KHAN S H. Influence of metal layer distribution on the projectiles impact response of glass fiber reinforced aluminum laminates[J]. Polymer Testing, 2018, 70: 320-347. |
22 | DECICCOD, TAHERIF. Performances of magnesium- and steel-based 3D fiber-metal laminates under various loading conditions[J]. Composite Structures, 2019, 229: 111390. |
23 | SEYED YAGHOUBI A, LIAW B. Thickness influence on ballistic impact behaviors of GLARE 5 fiber-metal laminated beams: Experimental and numerical studies[J]. Composite Structures, 2012, 94(8): 2585-2598. |
24 | KUBITA, TRZEPIECI?SKI T, KICI?SKI R, et al. Three-dimensional smooth particle hydrodynamics modeling and experimental analysis of the ballistic performance of steel-based FML targets[J]. Materials, 2022, 15(10): 3711. |
25 | 唐小军, 回天力, 王振清, 等. 碳纤维-不锈钢层板热载条件下冲击动态响应及层间损伤仿真研究[J]. 应用数学和力学, 2016, 37(10): 1026-1038. |
TANG X J, HUI T L, WANG Z Q, et al. Numerical simulation of impact dynamic responses and interlayer failure of CFRMLs under thermal loads[J]. Applied Mathematics and Mechanics, 2016, 37(10): 1026-1038 (in Chinese). | |
26 | PANG Y Z, YAN X J, WU L Z, et al. Experiment study of basalt fiber/steel hybrid laminates under high-velocity impact performance by projectiles[J]. Composite Structures, 2022, 280: 114848. |
27 | REN Z K, FAN W W, HOU J, et al. A numerical study of slip system evolution in ultra-thin stainless steel foil[J]. Materials, 2019, 12(11): 1819-1831. |
28 | REYES VILLANUEVA G, CANTWELL W J. The high velocity impact response of composite and FML-reinforced sandwich structures[J]. Composites Science and Technology, 2004, 64(1): 35-54. |
29 | KHORAMISHAD H, ALIKHANI H, DARIUSHI S. An experimental study on the effect of adding multi-walled carbon nanotubes on high-velocity impact behavior of fiber metal laminates[J]. Composite Structures, 2018, 201: 561-569. |
30 | 李应刚, 张雨, 朱凌, 等. 船用蜂窝金属夹芯板重复冲击实验研究[J]. 船舶力学, 2021, 25(5): 637-644. |
LI Y G, ZHANG Y, ZHU L, et al. Experimental study on the dynamic behaviours of honeycomb sandwich plates under repeated impacts[J]. Journal of Ship Mechanics, 2021, 25(5): 637-644 (in Chinese). | |
31 | SHIBUYA Y, ZHANG J W, SATO Y, et al. Evaluation of the mechanical properties and deformability of metal-based composite sheets made of thin stainless-steel sheets and carbon fiber reinforced plastics[J]. International Journal of Material Forming, 2022, 15(4): 47. |
32 | JAKUBCZAK P. The comparison of the veritable response to impact load of conventional and thin-ply types of fibre metal laminates[J]. Composite Structures, 2021, 257: 113151. |
33 | KONG D W, WANG D F, ZHANG X P. Study on the forming process and shear mechanical behavior of CFRP/Al self-piercing riveting employed 3D modeling[J]. Proceedings of the Institution of Mechanical Engineers, Part L: Journal of Materials: Design and Applications, 2023, 237(8): 1771-1787. |
34 | ZHU Q, ZHANG C, CURIEL-SOSAJ L, et al. Finite element simulation of damage in fiber metal laminates under high velocity impact by projectiles with different shapes[J]. Composite Structures, 2019, 214: 73-82. |
35 | ORIFICI A C, HERSZBERG I, THOMSON R S. Review of methodologies for composite material modelling incorporating failure[J]. Composite Structures, 2008, 86(1-3): 194-210. |
36 | JAKUBCZAK P. The impact behaviour of hybrid titanium glass laminates—Experimental and numerical approach[J]. International Journal of Mechanical Sciences, 2019, 159: 58-73. |
37 | BIENIAS J, JAKUBCZAK P, DADEJ K. Low-velocity impact resistance of aluminium glass laminates—Experimental and numerical investigation[J]. Composite Structures, 2016, 152: 339-348. |
38 | ZHANG F K, LIN Y, WU J A, et al. Comparison of stacking sequence on the low-velocity impact failure mechanisms and energy dissipation characteristics of CFRP/Al hybrid laminates[J]. Polymer Composites, 2022, 43(8): 5544-5562. |
/
〈 |
|
〉 |