Abstract Out-of-plane mechanical properties of the riveted joints restrict performance wing box assembly airplane. It is necessary to investigate pull-through composite/metal in order guide riveting design and ensure safety assembly. The progressive failure mechanism composite/aluminum joint subjected loading was investigated by experiments finite element method. A damage model based on Hashin-...

Carbon riveted Pt/C catalyst was designed and prepared by in situ carbonized glucose in this paper. Characterization results show that carbon riveted Pt/C prevents Pt nanoparticles from coalescence. Its stability is markedly enhanced due to the anchoring effect of the carbon layers formed during the carbon riveting process.

Two kinds of self-piercing riveted (SPR) joints were prepared with DP590 and AA6061 plates. The forming qualities the studied using finite element method. relationships between fatigue life failure forms different upper plates discussed. Finally, mechanisms analyzed. results show that maximum static tension DA32 (with an plate DP590) is significantly greater than other kind, always longer AA40 ...