Study on the bending properties of composite sandwich sheets embedded with magnetorheological elastomer smart grids
-
摘要:
对基于磁流变弹性体智能格栅单元的复材三明治板的弯曲特性进行了分析和实验研究。基于一阶剪切变形理论、能量法、最小势能原理、正交多项式法,建立了该三明治板的弯曲特性分析模型,在确定了总应变能的基础上,推导了结构的控制方程,并成功求解了悬臂边界下该三明治板在线分布载荷作用下的弹性弯曲变形。在分别完成上、下面板和磁流变弹性体格栅功能芯层的制备后,基于所建立的弯曲特性测试平台,对试件在不同磁感应强度和磁场控制区域作用下的弯曲变形进行了测试。验证结果表明:理论模型的最大计算误差不超过8.2%,处在误差允许的范围内,可有效预测结构的弯曲特性。研究发现随着内部磁场强度和磁场控制区域数量的增大,可提升结构的抗弯性能约15%~21%。
Abstract:The bending properties of composite sandwich sheets embedded with magnetorheological elastomer smart grid units were theoretically and experimentally investigated. A model was proposed to predict the bending characteristics of such sandwich sheets using the first-order shear deformation theory, energy technique, minimal potential energy principle, and the orthogonal polynomial methodology. After the total strain energy was obtained, the governing equation of the structure was deduced. As a result, the elastic bending deformation of such a sheet under the cantilever boundary subjected to the linearly distributed load can be successfully solved. When the preparation work of the upper and lower panels and the magnetorheological elastomer grid functional core was completed, the structural bending deformation was tested at different magnetic induction amplitudes and magnetic field control regions, based on an established test platform of such a specimen. The verification results showed that the maximum calculation error of the theoretical model did not exceed 8.2%, which was within an allowable error range. Hence, this model is trustworthy to predict the bending characteristics of such composite sandwich structures. It was also found that with the increase of the internal magnetic field amplitude and the number of magnetic field control regions, the structural bending resistance can be further improved by about 15%—21%.
-
Key words:
- magnetorheological elastomer /
- smart grid /
- bending property /
- composite material /
- sandwich sheet
-
表 1 理论分析时的材料与尺寸参数
Table 1. Material and dimensional parameters in theoretical analysis
类型 参数和数值 铜线圈层 $ {a_{\text{c}}}{\text{ = 80 mm}} $, $ {b_{\text{c}}}{\text{ = 80 mm}} $, $ {h_{\text{c}}}{\text{ = 2 mm}} $,
$ {E_{\text{c}}} = {\text{120}} \times {\text{1}}{{\text{0}}^{\text{3}}}{\text{ MPa}} $, $ {G_{\text{c}}} = {\text{3}} \times {\text{1}}{{\text{0}}^{\text{3}}}{\text{ MPa}} $,
$ {\upsilon _{\text{c}}} = {\text{0}}{\text{.25}} $, $ {\rho _{\text{c}}} = {{7\;800 \;{\mathrm{kg}}/}}{{\text{m}}^{\text{3}}} $肋条 $ {a_{{\text{gb}}}}{\text{ = 278 mm}} $, $ {b_{{\text{gb}}}}{\text{ = 13 mm}} $, $ {h_{{\text{gf}}}}{\text{ = 1 mm}} $
$ {E_{{\text{gb}}}} = {\text{110}} \times {10^2}{\text{ MPa}} $, $ {G_{{\text{gb}}}} = {\text{2}}{\text{.5}} \times {10^{\text{2}}}{\text{ MPa}} $
$ {\upsilon _{{\text{gb}}}} = {\text{0}}{\text{.4}} $, $ {\rho _{{\text{gb}}}} = {{2\;500\;{\mathrm{kg}}/}}{{\text{m}}^{\text{3}}} $MRE层 $ {a_{\text{v}}}{\text{ = 80 mm}} $, $ {b_{\text{v}}}{\text{ = 80 mm}} $, $ {h_{\text{v}}}{\text{ = 5 mm}} $,
$ {E_{\text{v}}} = {\text{1}}2{\text{ MPa}} $, $ {G_{\text{v}}} = 6{\text{ MPa}} $,
$ {\upsilon _{\text{v}}} = {\text{0}}{\text{.47}} $, $ {\rho _{\text{v}}} = {{4\;000 \;{\mathrm{kg}}/}}{{\text{m}}^{\text{3}}} $压电层 $ {a_{\text{p}}}{\text{ = 80 mm}} $,$ {b_{\text{p}}}{\text{ = 80 mm}} $,$ {h_{\text{p}}}{\text{ = 1 mm}} $,
$ {E_{\text{p}}} = {\text{76}} \times {\text{1}}{{\text{0}}^{\text{3}}}{\text{ MPa}} $,$ {G_{\text{p}}} = 4{\text{ MPa}} $,
$ {\upsilon _{\text{p}}} = 0.{\text{32}} $, $ {\rho _{\text{p}}} = {{3\;500 \;{\mathrm{kg}}/}}{{\text{m}}^{\text{3}}} $矩形格栅框 $ {a_{{\text{gf}}}}{\text{ = 84 mm}} $,$ {b_{{\text{gf}}}}{\text{ = 84 mm}} $,$ {h_{{\text{gf}}}}{\text{ = 9 mm}} $
$ {E_{{\text{gf}}}} = {\text{1}}{\text{.1}} \times {10^4}{\text{ MPa}} $,$ {G_{{\text{gf}}}} = {\text{2}}{\text{.5}} \times {10^{\text{2}}}{\text{ MPa}} $
$ {\upsilon _{{\text{gf}}}} = {\text{0}}{\text{.4}} $, $ {\rho _{{\text{gf}}}} = 2\;500{\text{ kg/}}{{\text{m}}^{\text{3}}} $碳纤维/
树脂面板层$ {a_{\text{f}}}{\text{ = 278 mm}} $, $ {b_{\text{f}}}{\text{ = 181 mm}} $, $ {h_{\text{f}}}{\text{ = 1}}{\text{.4 mm}} $,
$ {E_{{\text{f1}}}}{\text{ = 150}} \times {\text{1}}{{\text{0}}^{\text{3}}}{\text{ MPa}} $, $ {E_{{\text{f2}}}} = {\text{8}} \times {\text{1}}{{\text{0}}^{\text{3}}}{\text{ MPa}} $,
$ {G_{{\text{f}}12}} = {G_{{\text{f}}13}} = {G_{{\text{f23}}}} = {\text{4}} \times {\text{1}}{{\text{0}}^{\text{3}}}{\text{ MPa}} $,
$ {\upsilon _{\text{f}}} = {\text{0}}{\text{.3}} $, $ {\rho _{\text{f}}} = {{1\;618\; {\mathrm{kg}}/}}{{\text{m}}^{\text{3}}} $ -
[1] 李晖,孙伟,许卓,等. 纤维增强复合薄板振动测试与分析方法[M]. 北京: 机械工业出版社,2019. LI Hui,SUN Wei,XU Zhuo,et al. Test and analysis method for vibration of fiber reinforced composite sheet[M]. Beijing: China Machine Press,2019. (in ChineseLI Hui, SUN Wei, XU Zhuo, et al. Test and analysis method for vibration of fiber reinforced composite sheet[M]. Beijing: China Machine Press, 2019. (in Chinese) [2] HUDA Z,EDI P. Materials selection in design of structures and engines of supersonic aircrafts: a review[J]. Materials & Design,2013,46: 552-560. [3] YEH J Y. Vibration analysis of sandwich rectangular plates with magnetorheological elastomer damping treatment[J]. Smart Materials and Structures,2013,22(3): 035010. doi: 10.1088/0964-1726/22/3/035010 [4] YARALI E,ALI FARAJZADEH M,NOROOZI R,et al. Magnetorheological elastomer composites: modeling and dynamic finite element analysis[J]. Composite Structures,2020,254: 112881. doi: 10.1016/j.compstruct.2020.112881 [5] LI Hui,WANG Xintong,HU Xiaoyue,et al. Vibration and damping study of multifunctional grille composite sandwich plates with an IMAS design approach[J]. Composites Part B: Engineering,2021,223: 109078. doi: 10.1016/j.compositesb.2021.109078 [6] 李晖,孙伟,常永乐,等. 具有振幅依赖性的纤维增强复合薄板非线性阻尼的时域测试方法[J]. 振动与冲击,2018,37(5): 169-174,187. LI Hui,SUN Wei,CHANG Yongle,et al. Time domain test method for nonlinear damping of a fiber-reinforced composite thin plate with amplitude dependence[J]. Journal of Vibration and Shock,2018,37(5): 169-174,187. (in ChineseLI Hui, SUN Wei, CHANG Yongle, et al. Time domain test method for nonlinear damping of a fiber-reinforced composite thin plate with amplitude dependence[J]. Journal of Vibration and Shock, 2018, 37(5): 169-174, 187. (in Chinese) [7] CHANG Wanshu,VENTSEL E,KRAUTHAMMER T,et al. Bending behavior of corrugated-core sandwich plates[J]. Composite Structures,2005,70(1): 81-89. doi: 10.1016/j.compstruct.2004.08.014 [8] ZENKOUR A M,ALGHAMDI N A. Bending analysis of functionally graded sandwich plates under the effect of mechanical and thermal loads[J]. Mechanics of Advanced Materials and Structures,2010,17(6): 419-432. doi: 10.1080/15376494.2010.483323 [9] LI Dongdong,DENG Zongbai,XIAO Huaizhi. Thermomechanical bending analysis of functionally graded sandwich plates using four-variable refined plate theory[J]. Composites: Part B Engineering,2016,106: 107-119. doi: 10.1016/j.compositesb.2016.08.041 [10] LI Tiantian,WANG Lifeng. Bending behavior of sandwich composite structures with tunable 3D-printed core materials[J]. Composite Structures,2017,175: 46-57. doi: 10.1016/j.compstruct.2017.05.001 [11] ZAMANIFAR H,SARRAMI-FOROUSHANI S,AZHARI M. Static and dynamic analysis of corrugated-core sandwich plates using finite strip method[J]. Engineering Structures,2019,183: 30-51. doi: 10.1016/j.engstruct.2018.12.102 [12] MOHAMMADABADI M,YADAMA V,SMITH L. The effect of plate theories and boundary conditions on the bending behavior of a biaxial corrugated core sandwich panel[J]. Composite Structures,2020,241: 112133. doi: 10.1016/j.compstruct.2020.112133 [13] FARROKHABADI A,AHMAD TAGHIZADEH S,MADADI H,et al. Experimental and numerical analysis of novel multi-layer sandwich panels under three point bending load[J]. Composite Structures,2020,250: 112631. doi: 10.1016/j.compstruct.2020.112631 [14] KRISHNA P S,VEMULA A M,AHAMED P U,et al. Bending analysis of honeycomb sandwich panels with metallic face sheets and GFRP core[J]. Materials Today: Proceedings,2022,60: 1537-1547. doi: 10.1016/j.matpr.2021.12.050 [15] ZHANG Zhijia,WEI Xin,WU Ke,et al. Failure analysis of brazed sandwich structures with square honeycomb-corrugation hybrid cores under three-point bending[J]. Thin-Walled Structures,2022,170: 108591. doi: 10.1016/j.tws.2021.108591 [16] VEMULURI R B,RAJAMOHAN V,ARUMUGAM A B. Dynamic characterization of tapered laminated composite sandwich plates partially treated with magnetorheological elastomer[J]. Journal of Sandwich Structures & Materials,2018,20(3): 308-350. [17] 沈观林,胡更开. 复合材料力学[M]. 北京: 清华大学出版社,2006. SHEN Guanlin,HU Gengkai. Mechanics of composite materials[M]. Beijing: Tsinghua University Press,2006. (in ChineseSHEN Guanlin, HU Gengkai. Mechanics of composite materials[M]. Beijing: Tsinghua University Press, 2006. (in Chinese) [18] MAHI A,ADDA BEDIA E A,TOUNSI A. A new hyperbolic shear deformation theory for bending and free vibration analysis of isotropic,functionally graded,sandwich and laminated composite plates[J]. Applied Mathematical Modelling,2015,39(9): 2489-2508. doi: 10.1016/j.apm.2014.10.045 [19] LI Hui,WANG Wenyu,WANG Xintong,et al. A nonlinear analytical model of composite plate structure with an MRE function layer considering internal magnetic and temperature fields[J]. Composites Science and Technology,2020,200: 108445. doi: 10.1016/j.compscitech.2020.108445 [20] LI Hui,WU Tengfei,GAO Zhijiang,et al. An iterative method for identification of temperature and amplitude dependent material parameters of fiber-reinforced polymer composites[J]. International Journal of Mechanical Sciences,2020,184: 105818. doi: 10.1016/j.ijmecsci.2020.105818 -

下载: