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材料导报  2026, Vol. 40 Issue (6): 24120214-6    https://doi.org/10.11896/cldb.24120214
  高分子与聚合物基复合材料 |
基于手糊铺层工艺的碳纤维复合材料翼梁设计与试验验证
刘福佳1,2,*, 李群芳1, 耿昊1, 马刚1, 郭晗1
1 辽宁通用航空研究院,沈阳 110136;
2 沈阳航空航天大学航空宇航学院,沈阳 110136
Design and Experimental Verification of Carbon Fiber Composite Spar Based on Hand Lay-up Process
LIU Fujia1,2,*, LI Qunfang1, GENG Hao1, MA Gang1, GUO Han1
1 Liaoning General Aviation Academy, Shenyang 110136, China;
2 College of Aerospace Engineering, Shenyang Aerospace University, Shenyang 110136, China
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摘要 作为机翼结构的主承力构件,翼梁的结构设计对机翼的承载能力起关键作用。考虑复合材料翼梁生产材料的性能要求、成型工艺、成本等因素,依据选材原则完成了复合材料选材,并通过试验获得了材料的基础力学性能参数,为翼梁的优化设计奠定了基础。针对机翼结构的设计要求,设计了一款适用于大展弦比机翼的复合材料“工”字梁,通过建立有限元模型,对复合材料翼梁进行铺层厚度设计、铺层顺序设计,并采用Tsai-Wu准则对翼梁结构进行了强度校核。利用静力试验对手糊工艺成型的翼梁的承载能力进行了验证,同时对有限元模型进行了校核。试验结果表明,翼梁结构设计方案满足设计载荷要求,仿真结果与试验结果有较好的一致性,表明对机翼进行静力学分析的参数设置基本合理,可以为后续翼梁结构减重设计提供依据。
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刘福佳
李群芳
耿昊
马刚
郭晗
关键词:  手糊铺层  碳纤维  翼梁设计  仿真分析  试验验证    
Abstract: As the primary load-bearing component of the wing structure, the structural design of the wing spar plays a key role in the load-bearing capacity of the wing. Considering the performance requirements, molding process, and cost factors of the composite materials, the selection of composite materials was based on the principle of material selection. The basic mechanical properties of the materials were obtained through experiments, which laid the foundation for the optimized design of the wing spar. In response to the design requirements of the wing structure, a composite I-beam was designed, which was suitable for high-aspect-ratio wings. The layup thickness and sequence of the composite wing spar were designed by establishing a finite element model, and the strength of the wing spar structure was checked by using the Tsai-Wu criterion. The load-bearing capacity of the wing spar formed by hand lay-up process was verified through the static test, and the finite element model was also validated. The test results showed that the wing spar structural design met the design load requirements, and there was good consistency between the simulation and test results, indicating that the parameter settings for the static analysis of the wing were basically reasonable. This provided a basis for the subsequent weight reduction design of the wing spar structure.
Key words:  hand lay-up    carbon fiber    wing spar design    simulation analysis    experimental validation
出版日期:  2026-03-25      发布日期:  2026-04-03
ZTFLH:  V224  
通讯作者:  *刘福佳,博士,沈阳航空航天大学航空宇航学院讲师,目前主要研究方向为飞机多学科优化设计和飞机复合材料结构设计等。718880677@qq.com   
引用本文:    
刘福佳, 李群芳, 耿昊, 马刚, 郭晗. 基于手糊铺层工艺的碳纤维复合材料翼梁设计与试验验证[J]. 材料导报, 2026, 40(6): 24120214-6.
LIU Fujia, LI Qunfang, GENG Hao, MA Gang, GUO Han. Design and Experimental Verification of Carbon Fiber Composite Spar Based on Hand Lay-up Process. Materials Reports, 2026, 40(6): 24120214-6.
链接本文:  
https://www.mater-rep.com/CN/10.11896/cldb.24120214  或          https://www.mater-rep.com/CN/Y2026/V40/I6/24120214
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