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Effect of tightening torque on the mechanical performance and damage form of hybrid bonded/bolted joints
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Jinyi SHEN1, Weixin HU2, Tianyu ZHANG2, Junshan HU1, Wenhe LIAO3, Wei TIAN1, Ye SHEN4
Journal of Mechanical Strength | 2025, 47(7) : 24 - 32
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Journal of Mechanical Strength | 2025, 47(7): 24-32
·Fatigue·Damage·Fracture·Failure Analysis·
Effect of tightening torque on the mechanical performance and damage form of hybrid bonded/bolted joints
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Jinyi SHEN1, Weixin HU2, Tianyu ZHANG2, Junshan HU1, Wenhe LIAO3, Wei TIAN1, Ye SHEN4
Affiliations
  • 1.College of Mechanical & Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • 2.AVIC Xi’an Aircraft Industry Group Company Ltd., Xi’an 710089, China
  • 3.School of Mechanical Engineering, Nanjing University of Science & Technology, Nanjing 210094, China
  • 4.Shanghai Aerospace Electronic Technology Research Institute, Shanghai 201109, China
Published: 2025-07-15 doi: 10.16579/j.issn.1001.9669.2025.07.003
Outline
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To investigate the mechanical properties of woven composite hybrid bonded/bolted joints, a mechanical failure model for hybrid bonded/bolted joints based on 3D progressive damage model and cohesive force model was developed to simulate the mechanical behavior and damage evolution of the joints. Based on the Abaqus finite element software, a finite element simulation model for hybrid bonded/bolted joints woven composites was established. The damage initiation and propagation of the composite material were judged using the three-dimensional Linde criterion. The cohesive force model was used to simulate the damage failure process of the adhesive layer. On the basis of test verification of the model accuracy, the strength and damage failure process of the joints were analyzed under different tightening torques. The test and simulation results indicate that as the tightening torque increases, the extension of adhesive layer damage can be effectively suppressed.However, the shear strength of the adhesive layer in the hybrid bonded/bolted joints firstly increases and then decreases,because increasing the tightening torque can reduce the peeling stress of the adhesive layer in the joints. However, the excessive tightening torque will strengthen the stress around the adhesive layer hole, leading to a decrease in the shear srength of the adhesive layer and a decrease in the strength of the connection structure. The load-displacement curve of the numerical simulation is consistent with the test results, and the predicted adhesive layer fracture load is equivalent to the test results. At the same time, the fiber damage, matrix damage, and delamination damage on the laminated plate can also be well reflected in the numerical model, which is similar to the damage form after the connection test, verifying the effectiveness of the damage prediction model.

Composite material  /  Hybrid bonded/bolted joint  /  Finite element analysis  /  Shear strength of adhesive layer  /  Damage evolution
Jinyi SHEN, Weixin HU, Tianyu ZHANG, Junshan HU, Wenhe LIAO, Wei TIAN, Ye SHEN. Effect of tightening torque on the mechanical performance and damage form of hybrid bonded/bolted joints[J]. Journal of Mechanical Strength, 2025 , 47 (7) : 24 -32 . DOI: 10.16579/j.issn.1001.9669.2025.07.003
  • Anhui Province Key Research and Development Program(202203a05020039)
  • China Postdoctoral Science Foundation(2022M720939)
  • Natural Science Fund for Jiangsu Province(BK20231444)
  • National Natural Science Foundation of China(52005259)
Year 2025 volume 47 Issue 7
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Article Info
doi: 10.16579/j.issn.1001.9669.2025.07.003
  • Receive Date:2023-10-24
  • Online Date:2026-03-19
  • Published:2025-07-15
Article Data
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History
  • Received:2023-10-24
  • Revised:2024-01-09
Funding
Anhui Province Key Research and Development Program(202203a05020039)
China Postdoctoral Science Foundation(2022M720939)
Natural Science Fund for Jiangsu Province(BK20231444)
National Natural Science Foundation of China(52005259)
Affiliations
    1.College of Mechanical & Electrical Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
    2.AVIC Xi’an Aircraft Industry Group Company Ltd., Xi’an 710089, China
    3.School of Mechanical Engineering, Nanjing University of Science & Technology, Nanjing 210094, China
    4.Shanghai Aerospace Electronic Technology Research Institute, Shanghai 201109, China

Corresponding:

HU Junshan, E-mail:
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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