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Cui Da, Zhang Minghao, Li Daokui. Design and experimental verification of composite bend-twist coupled structure based on asymmetric stacking sequence. Chinese Journal of Theoretical and Applied Mechanics, 2024, 56(10): 2888-2901. DOI: 10.6052/0459-1879-24-230
Citation: Cui Da, Zhang Minghao, Li Daokui. Design and experimental verification of composite bend-twist coupled structure based on asymmetric stacking sequence. Chinese Journal of Theoretical and Applied Mechanics, 2024, 56(10): 2888-2901. DOI: 10.6052/0459-1879-24-230

DESIGN AND EXPERIMENTAL VERIFICATION OF COMPOSITE BEND-TWIST COUPLED STRUCTURE BASED ON ASYMMETRIC STACKING SEQUENCE

  • Received Date: May 14, 2024
  • Accepted Date: September 17, 2024
  • Available Online: September 17, 2024
  • Published Date: September 18, 2024
  • The composite bend-twist coupled structure has important application value in the structural design of forward-swept wing aircrafts. The existing research mainly design bend-twist coupled structure based on symmetric composite materials, and there are some limitations such as narrow design domain and limited coupling effect. Asymmetric composite could solve the above problems, but because of its curing deformation, it has not been widely applied in engineering. In this paper, geometric factors and material constants of laminates are introduced to derive the analytical conditions of hygro-thermal stability of extension-shearing multi-coupled laminates. Secondly, a bend-twist coupled box structure model was constructed using extension-shearing multi-coupled laminates, and genetic algorithm-sequential quadratic program (GA-SQP) was used to complete the asymmetric optimization design of the box structure, which significantly improves the coupling effect of the structure. Then, the hygro-thermal stability and coupling effect of the bend-twist coupled structure is verified by numerical simulation, and its robustness is verified by Monte Carlo method. Finally, the experimental test of the coupling effect of the asymmetric bend-twist coupled structure is designed and completed, and the correctness of the theory is further verified. The results show that the asymmetric bend-twist coupled structure will not undergo curing deformation when the fiber angles meet conditions of hygro-thermal stability, and the introduction of asymmetry can significantly improve the coupling effect of bend-twist coupled structures and maximum increase is above 90%.
  • [1]
    薛程, 李彦斌, 杭晓晨等. 复合材料机翼热气弹剪裁研究及分析系统研发. 东南大学学报(自然科学版), 2022, 52(5): 899-906 (Xue Cheng, Li Yanbin, Hang Xiaochen, et al. Aerothermoelastic tailoring research of composite wing and analysis system development. Journal of Southeast University (Natural Science Edition), 2022, 52(5): 899-906 (in Chinese) doi: 10.3969/j.issn.1001-0505.2022.05.010

    Xue Cheng, Li Yanbin, Hang Xiaochen, et al. Aerothermoelastic tailoring research of composite wing and analysis system development. Journal of Southeast University (Natural Science Edition), 2022, 52(5): 899-906 (in Chinese) doi: 10.3969/j.issn.1001-0505.2022.05.010
    [2]
    李金洋. 大展弦比复合材料机翼气动弹性剪裁研究. [硕士论文]. 汉中: 陕西理工大学, 2023 (Li Jinyang. Research on aeroelastic tailoring of high aspect ratio composite wing. [Master Thesis]. Hanzhong: Shanxi University of Technology, 2023 (in Chinese)

    Li Jinyang. Research on aeroelastic tailoring of high aspect ratio composite wing. [Master Thesis]. Hanzhong: Shanxi University of Technology, 2023 (in Chinese)
    [3]
    宁蕙, 谭志勇, 张宏宇. 复合材料螺栓连接结构疲劳问题研究进展. 强度与环境, 2023, 50(3): 1-9 (Ning Hui, Tan Zhiyong, Zhang Hongyu. Research progress on fatigue properties of composite bolted structures. Structure and Environment Engineering, 2023, 50(3): 1-9 (in Chinese)

    Ning Hui, Tan Zhiyong, Zhang Hongyu. Research progress on fatigue properties of composite bolted structures. Structure and Environment Engineering, 2023, 50(3): 1-9 (in Chinese)
    [4]
    韩剑, 孙士勇, 牛斌等. 树脂基复合材料点阵结构的制造技术研究进展. 航空学报, 2023, 44(9): 42-62 (Han Jian, Sun Shiyong, Niu Bin, et al. Progress in manufacturing technologies of resin-based composite lattice structures. Acta Aeronautica et Astronautica Sinica, 2023, 44(9): 42-62 (in Chinese)

    Han Jian, Sun Shiyong, Niu Bin, et al. Progress in manufacturing technologies of resin-based composite lattice structures. Acta Aeronautica et Astronautica Sinica, 2023, 44(9): 42-62 (in Chinese)
    [5]
    姜志平. 弯扭耦合复合材料机翼的静气动弹性结构优化设计. [硕士论文]. 南京: 南京航空航天大学, 2015 (Jiang Zhiping. Static aeroelasticity structure optimization for composite wing structures with bend-twist coupling. [Master Thesis]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015 (in Chinese)

    Jiang Zhiping. Static aeroelasticity structure optimization for composite wing structures with bend-twist coupling. [Master Thesis]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2015 (in Chinese)
    [6]
    李谨. 基于非对称复合材料的弯曲-扭转耦合结构设计方法研究. [博士论文]. 长沙: 国防科技大学, 2016 (Li Jin. Investigation on design method for bending-twisting coupled structure with asymmetric composite laminates. [PhD Thesis]. Changsha: National University of Defense Technology, 2016 (in Chinese)

    Li Jin. Investigation on design method for bending-twisting coupled structure with asymmetric composite laminates. [PhD Thesis]. Changsha: National University of Defense Technology, 2016 (in Chinese)
    [7]
    Fowser SW, Pipes RB, Wilson DW. On the determination of laminate and lamina shear response by tension tests. Composites Science and Technology, 1986, 26(1): 31-36 doi: 10.1016/0266-3538(86)90054-0
    [8]
    York CB. On extension-shearing coupled laminates. Composite Structures, 2015, 120: 472-482 doi: 10.1016/j.compstruct.2014.10.019
    [9]
    York CB. On tapered warp-free laminates with single-ply terminations. Composites Part A : Applied Science and Manufacturing, 2015, 72: 127-138
    [10]
    York CB, Almeida SFM. On extension-shearing bending-twisting coupled laminates. Composite Structures, 2017, 164: 10-22 doi: 10.1016/j.compstruct.2016.12.041
    [11]
    York CB, Almeida SFM. Tapered laminate designs for new non-crimp fabric architectures. Composites Part A: Applied Science and Manufacturing, 2017, 100: 150-160 doi: 10.1016/j.compositesa.2017.04.023
    [12]
    洪岩. 先进复合材料机翼静气动弹性稳定性分析. [硕士论文]. 西安: 西安交通大学, 2011 (Hong Yan. Static aeroelastic stability analysis of advanced composite wings. [Master Thesis]. Xi'an: Xi'an Jiaotong University, 2011 (in Chinese)

    Hong Yan. Static aeroelastic stability analysis of advanced composite wings. [Master Thesis]. Xi'an: Xi'an Jiaotong University, 2011 (in Chinese)
    [13]
    Li J, Li DK. Extension-shear coupled laminates with immunity to hygro-thermal shearing distortion. Composite Structures, 2015, 123: 401-407 doi: 10.1016/j.compstruct.2014.12.032
    [14]
    胡晓强, 黄政, 刘志华. 复合材料螺旋桨弯扭耦合刚度特性分析. 中国舰船研究, 2022, 17(1): 25-35 (Hu Xiaoqiang, Huang Zheng, Liu Zhihua. Numerical analysis on bending-torsional coupling stiffness characteristics of composite propeller. Chinese Journal of Ship Research, 2022, 17(1): 25-35 (in Chinese)

    Hu Xiaoqiang, Huang Zheng, Liu Zhihua. Numerical analysis on bending-torsional coupling stiffness characteristics of composite propeller. Chinese Journal of Ship Research, 2022, 17(1): 25-35 (in Chinese)
    [15]
    苏傲男. 大型柔性风电叶片弯扭耦合模型研究. [硕士论文]. 成都: 电子科技大学, 2023 (Su Aonan. Research on bend-twist coupling model of large flexible wind turbine blade. [Master Thesis]. Chengdu: University of Electronic Science and Technology of China, 2023 (in Chinese)

    Su Aonan. Research on bend-twist coupling model of large flexible wind turbine blade. [Master Thesis]. Chengdu: University of Electronic Science and Technology of China, 2023 (in Chinese)
    [16]
    罗涛, 巫发明, 黄剑锋等. 弯扭耦合长柔叶片颤振速度分析. 太阳能学报, 2024, 45(3): 90-94 (Luo Tao, Wu Faming, Huang Jianfeng, et al. Flutter speed analysis of bend-twist coupled long flexible blade. Acta Energiae Solaris Sinica, 2024, 45(3): 90-94 (in Chinese)

    Luo Tao, Wu Faming, Huang Jianfeng, et al. Flutter speed analysis of bend-twist coupled long flexible blade. Acta Energiae Solaris Sinica, 2024, 45(3): 90-94 (in Chinese)
    [17]
    王子文, 杨涛, Riziotis V. 基于ANSYS的10 MW风力机叶片弯扭耦合特性研究. 应用能源技术, 2019, 6: 33-37 (Wang Ziwen, Yang Tao, Riziotis V. Research on bend-twist coupling properties of 10 MW wind turbine blade based on ANSYS. Applied Energy Technology, 2019, 6: 33-37 (in Chinese)

    Wang Ziwen, Yang Tao, Riziotis V. Research on bend-twist coupling properties of 10 MW wind turbine blade based on ANSYS. Applied Energy Technology, 2019, 6: 33-37 (in Chinese)
    [18]
    王海生, 缪维跑, 张立等. 基于主梁腹板构型的大型风力机弯扭耦合叶片结构性能研究. 太阳能学报, 2023, 44(3): 29-38 (Wang Haisheng, Miao Weipao, Zhang Li, et al. Research on main girder web configuration of bend-twist coupling blade of large wind turbine with composite laying. Acta Energiae Solaris Sinica, 2023, 44(3): 29-38 (in Chinese)

    Wang Haisheng, Miao Weipao, Zhang Li, et al. Research on main girder web configuration of bend-twist coupling blade of large wind turbine with composite laying. Acta Energiae Solaris Sinica, 2023, 44(3): 29-38 (in Chinese)
    [19]
    付凌峰, 姜鑫, 孙震等. 碳/玻混杂纤维铺层结构对风力机叶片弯扭耦合特性的影响. 复合材料学报, 2023, 40(7): 3912-3920 (Fu Lingfeng, Jiang Xin, Sun Zhen, et al. Influence of carbon/glass hybrid fiber layup structure on the bending-twisting coupling behavior of wind turbine blades. Acta Materiae Compositae Sinica, 2023, 40(7): 3912-3920 (in Chinese)

    Fu Lingfeng, Jiang Xin, Sun Zhen, et al. Influence of carbon/glass hybrid fiber layup structure on the bending-twisting coupling behavior of wind turbine blades. Acta Materiae Compositae Sinica, 2023, 40(7): 3912-3920 (in Chinese)
    [20]
    Haynes RA, Armanios EA. New families of hygrothermally stable composite laminates with optimal extension-twist coupling. AIAA Journal, 2010, 48(12): 2954-2961 doi: 10.2514/1.J050596
    [21]
    Haynes RA, Armanios EA. The challenge of achieving hygrothermal stability in composite laminates with optimal couplings. International Journal of Engineering Science, 2012, 59: 74-82 doi: 10.1016/j.ijengsci.2012.03.013
    [22]
    秦国锋, 秦锐坚, 糜沛纹等, 复合材料带孔板孔形与铺层优化设计. 交通运输工程学报, 2022, 22(4): 223-231 (Qin Guofeng, Qin Ruijian, Mi Peiwen, et al. Optimal designs of hole shape and ply composite plates with holes. Journal of Traffic and Transportation Engineering, 2022, 22(4): 223-231 (in Chinese)

    Qin Guofeng, Qin Ruijian, Mi Peiwen, et al. Optimal designs of hole shape and ply composite plates with holes. Journal of Traffic and Transportation Engineering, 2022, 22(4): 223-231 (in Chinese)
    [23]
    谭培林. 基于响应面法的CG231复合材料机翼的铺层优化设计. [硕士论文]. 重庆: 重庆理工大学, 2022 (Tan Peiling. Lamination optimization design of CG231 composite wing based on response surface method. [Master Thesis]. Chongqing: Chongqing University of Technology, 2022 (in Chinese)

    Tan Peiling. Lamination optimization design of CG231 composite wing based on response surface method. [Master Thesis]. Chongqing: Chongqing University of Technology, 2022 (in Chinese)
    [24]
    赵博伟, 赖辉. 基于遗传算法的复合材料进气道铺层角度优化及分析验证. 科技创新与应用, 2022, 12(4): 133-135, 138 (Zhao Bowei, Lai Hui. Optimization and analysis of lamination angle of composite inlet based on genetic algorithm. Technology Innovation and Application, 2022, 12(4): 133-135, 138 (in Chinese)

    Zhao Bowei, Lai Hui. Optimization and analysis of lamination angle of composite inlet based on genetic algorithm. Technology Innovation and Application, 2022, 12(4): 133-135, 138 (in Chinese)
    [25]
    白国栋, 童小燕, 姚磊江. 基于深度学习的复合材料铺层优化方法. 复合材料科学与工程, 2020, 7: 68-73 (Bai Guodong, Tong Xiaoyan, Yao Leijiang. Layup optimization method of composite wing based on deep learning. Composites Science and Engineering, 2020, 7: 68-73 (in Chinese)

    Bai Guodong, Tong Xiaoyan, Yao Leijiang. Layup optimization method of composite wing based on deep learning. Composites Science and Engineering, 2020, 7: 68-73 (in Chinese)
    [26]
    Shamsudin MH, Chen J, York CB. Bounds on the compression buckling strength of hygro-thermally curvature-stable laminate with extension-twisting coupling. International Journal of Structural Integrity, 2013, 4(4): 477-486 doi: 10.1108/IJSI-09-2012-0025
    [27]
    Shamsudin MH, Rousseau J, Verchery G, et al. Experimental validation of the mechanical coupling response for hygro-thermally curvature-stable laminated composite materials//6th International Conference “Supply on the Wings” in Conjunction with AIRTEC 2011 International Aerospace Supply Fair. Exhibition Center, Frankfurt/Main, Germany, 2011
    [28]
    Carvalho NV, Chen BY, Pinho ST. Modeling delamination migration in cross-ply tape laminates. Composites Part A: Applied Science and Manufacturing, 2015, 71: 192-203 doi: 10.1016/j.compositesa.2015.01.021
    [29]
    梁言, 龙连春. 结合DIC技术的开孔复合材料层合板屈曲实验测试//北京力学会第二十五届学术年会会议论文集. 北京力学会第二十五届学术年会, 北京, 2019-1-6 (Liang Yan, Long Lianchun. Experimental testing of buckling of laminates with open holes combined with DIC technology//Proceedings of the 25th Annual Conference of Beijing Society of Mechanics. The 25th Annual Conference of Beijing Society of Mechanics, Beijing, 2019-1-6 (in Chinese)

    Liang Yan, Long Lianchun. Experimental testing of buckling of laminates with open holes combined with DIC technology//Proceedings of the 25th Annual Conference of Beijing Society of Mechanics. The 25th Annual Conference of Beijing Society of Mechanics, Beijing, 2019-1-6 (in Chinese)
    [30]
    崔达. 复合材料弯扭耦合结构优化设计. [硕士论文]. 长沙: 国防科技大学, 2018 (Cui Da. Optimization design of bending-twisting coupled composite structure. [Master Thesis]. Changsha: National University of Defense Technology, 2018 (in Chinese)

    Cui Da. Optimization design of bending-twisting coupled composite structure. [Master Thesis]. Changsha: National University of Defense Technology, 2018 (in Chinese)
    [31]
    李勇, 韩非非, 张昕喆等. 基于遗传算法-序列二次规划的涡扇发动机最低油耗性能寻优控制. 推进技术, 2020, 41(7): 1638-1648 (Li Yong, Han Feifei, Zhang Xinzhe, et al. Performance seeking control of turbofan engine minimum fuel consumption model based on GA-SQP. Journal of Propulsion Technology, 2020, 41(7): 1638-1648 (in Chinese)

    Li Yong, Han Feifei, Zhang Xinzhe, et al. Performance seeking control of turbofan engine minimum fuel consumption model based on GA-SQP. Journal of Propulsion Technology, 2020, 41(7): 1638-1648 (in Chinese)
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