材料融合位置对层合智能结构疲劳性能的提升
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南京航空航天大学直升机动力学全国重点实验室/直升机研究院,南京 210016

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通讯作者:

韩东,男,教授,博士生导师,E-mail: donghan@nuaa.edu.cn。

中图分类号:

V214.8

基金项目:

国家自然科学基金(11972181)。


Fatigue Performance Improvement of Laminated Smart Structures by Different Material Conjunction Positions
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National Key Laboratory of Helicopter Aeromechanics/Helicopter Research Institute, Nanjing University of Aeronautics & Astronautics, Nanjing 210016, China

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    摘要:

    为研究智能材料融合位置对层合智能结构疲劳性能的影响,本文针对宏纤维复合材料(Macro fiber composite, MFC)与玻纤增强复合材料(Glass fiber reinforced polymer, GFRP)基体组成的层合智能结构展开研究。对两种融合位置的智能结构试验件进行了疲劳测试,结果表明,中间层融合智能结构的疲劳寿命高于最外层融合智能结构。建立了智能结构有限元模型(Finite element model, FEM),其载荷-应变预测结果与试验数据的误差小于7%,验证了模型有效性。通过线性疲劳寿命曲线对智能结构的疲劳寿命进行预测,预测寿命与试验结果吻合良好。进一步分析了不同载荷下融合位置对智能结构疲劳寿命的影响。单轴拉伸、扭转载荷下,随融合位置由最外层向中间层移动,界面应力水平降低,疲劳寿命提高,其中,拉应力的显著降低占主导作用。单轴拉伸载荷下,界面应力集中出现于矩形智能材料短边;单轴扭转载荷下,界面应力集中出现于智能材料四周。多轴载荷下,相较最外层融合,中间层融合几乎消除了层间拉应力并不同程度地降低了有效剪应力,使疲劳寿命提高;疲劳寿命提升效果受载荷比影响,载荷比为0.273 4时,疲劳寿命提升效果最好。

    Abstract:

    To investigate the effect of conjunction position on fatigue performance of laminated smart structures, a study of macro fiber composite(MFC) and glass fiber reinforced polymer (GFRP) laminated smart structure is presented. Experiments on two types of specimens with different conjunction positions are carried out, and the results indicate that the fatigue life of smart structure is higher when MFC is in the middle layer of structure than at the outermost layer. A finite element model (FEM) model is established and validated by the error within 7% comparing with the load-strain data during experiment. Fatigue life prediction using a linear S-N curve shows good agreement with experimental results. The effect of the MFC conjunction position on the fatigue life of the smart structure under different load is further analyzed. Under uniaxial load, the interfacial stress decreases and the fatigue life increases as the MFC conjunction position shifts from the outermost layer to the middle layer, and this improvement is dominated by a significant reduction in tensile stress. Besides, stress concentration occurs near the short edges of the rectangular MFC under uniaxial tensile load, and around the perimeter of the MFC under uniaxial torsional load. Under multiaxial load, compared to the outermost-layer conjunction, the middle-layer conjunction almost eliminates interlaminar tensile stress and reduces the effective shear stress to varying degrees, leading to enhanced fatigue life. The degree of fatigue life improvement is significantly affected by the load ratio, and the optimal improvement occurs at a load ratio of 0.273 4.

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刘润甫,韩东,王天健,朱尹.材料融合位置对层合智能结构疲劳性能的提升[J].南京航空航天大学学报,2026,58(3):647-654

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  • 收稿日期:2025-06-10
  • 最后修改日期:2025-12-12
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  • 在线发布日期: 2026-06-18
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