基于材料时变参量的挖补修理胶层内剪应力研究
作者:
作者单位:

1.中国民用航空飞行学院航空工程学院,广汉 618307;2.中国民用航空飞行学院,四川省通用航空器维修工程技术研究中心,广汉 618307

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中图分类号:

TB333.2

基金项目:

国家自然科学基金民航联合基金重点资助项目 (U1333201);四川省科技计划项目 (2019YJ0722);四川省通用航空器维修工程技术研究中心资助课题 (GAMRC2021YB10);高校基本科研业务费专项资金项目(XSY2022-10)


Shear Stress in the Adhesive Layer During Scarf Repairing Based on Time-varying Parameters of Materials
Author:
Affiliation:

1.Aviation Engineering College Civil Aviation Flight University of China, Guanghan 618307;2.Sichuan Province Engineering Technology Research Center of General Aircraft Maintenance, Civil Aviation Flight University of China, Guanghan 618307

Fund Project:

The Key Program of the Civil Aviation Joint Funds of the National Natural Science Foundation of China,The Sichuan Province Science and Technology Program,Project supported by Sichuan Province Engineering Technology Research Center of General Aircraft Maintenance。

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    摘要:

    以AS4/3501-6材料的挖补修理为研究背景,基于材料热、力学参数的时变特性,分别为补片和胶层建立了热-力-化学多物理场耦合的有限元模型,研究了不同挖补角度和胶层厚度对胶层残余剪应力的影响,探索了不同挖补修理设计方案下的修理过程中胶层残余剪应力分布。结果表明:挖补角度、胶层厚度的增大均会加剧胶层残余剪应力集中;减小挖补角度,可有效降低胶层残余剪应力及沿胶层径向平均剪应力梯度;3°挖补角度下胶层径向中点残余剪应力比15°下降低17%,径向平均剪应力梯度降低92%;减小胶层厚度,胶层残余剪应力减小但平均剪应力梯度增大,0.3 mm胶层厚度下胶层径向中点残余剪应力比1.5 mm下降低15%,径向平均剪应力梯度升高30%。经验证三维有限元模型及计算方法正确,为改进修理工艺、提高修复质量提供了依据。

    Abstract:

    Taking the scarf repair of AS4/3501-6 materials as the research background,based on the time-dependent properties of the thermodynamic parameters of materials, the finite element model of thermal-mechanical-chemical multi physical field was established for the patch and the adhesive layer. The effects of different scarf angles and adhesive layer thickness on the residual shear stress of the adhesive layer were studied and the residual shear stress distribution of the adhesive layer under different program was explored. The results show that the residual shear stress concentration of the adhesive layer will be aggravated by increasing the scarf angle and the thickness of the adhesive layer.The residual shear stress and the radial average shear stress gradient along the adhesive layer can be effectively reduced by reducing the scarf angle; The residual shear stress at the radial midpoint of the adhesive layer is 17% lower and the radial average shear stress gradient is 92% lower for 3° scarf angle than that at 15° scarf angle; When the thickness of the adhesive layer is reduced, the residual shear stress of the adhesive layer decreases,while the average shear stress gradient increases. For 0.3 mm adhesive thickness, the residual shear stress at the radial midpoint of the layer is 15% lower and the average radial shear stress gradient is 30% higher than that for 1.5 mm adhesive thickness. It is verified that the 3D finite element model and calculation method are correct, which provides a basis for improving the repair process and improving the repair quality.

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引用本文

闫登杰,陈淑仙,丁镇源.基于材料时变参量的挖补修理胶层内剪应力研究[J].宇航材料工艺,2023,53(3):36-43.

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历史
  • 收稿日期:2022-06-16
  • 最后修改日期:2022-07-13
  • 录用日期:2022-07-13
  • 在线发布日期: 2023-06-26
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