Low Damage Riveting Process Parameters of Multi-Layer Consisting of GFRP Composite and Aluminum Alloy
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1.Tianjin Long March Launch Vehicle Manufacturing Co.Ltd.,Tianjin 300462;2.Nanjing University of Aeronautics and Astronautics,Nanjing 210016;3.Capital Aerospace Machinery Company Limited,Beijing 100076;4.China Academy of Launch Vehicle Technology,Beijing 100076

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V461

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    Abstract:

    In order to solve the damage to GFRP composite during the riveting process of multi-layer consisting of GFRP composite and aluminum alloy,the dynamic damage analysis of GFRP composite have been simulated by ABAQUS on the effects of diameter of pre-drilled hole and riveting squeeze of Φ4 mm 2A10 aluminum alloy rivet.On the basis of the simulation the experimental investigations on multi-layer consisting of GFRP composite and aluminum alloy were performed.The non-destructive test and shear test of the specimens were conducted.Results of the analysis indicate that the adequate process parameters of Φ4.2 mm pre-drilled hole and (18.5±0.2) kN riveting force can achieve the requirements of low damage to GFRP composite.

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History
  • Received:July 29,2019
  • Revised:May 25,2020
  • Adopted:November 15,2019
  • Online: June 17,2020
  • Published: