Riveting is a well established technology in the manufacturing of aeronautical structures as well as in the automotive industries. Despite its simplicity, the rivet presents a local stiffness that is not easy to properly model within a large finite element analysis. However, precision in the local stiffness evaluation is essential to perform any structural analysis when several rivet are applied in a joint structure. The result is that any rivet requires a local mesh refinement or, and this is the most common case, a drastic simplification of its structural modelling characteristics. In the present paper the structural behavior of a riveted lap joint connection was investigated experimentally and numerically using a new rivet finite element. The Rivet Element, based on a closed-form solution of a theoretical model of the rivet joint, is able to precisely evaluate, in FE analysis, both local and overall stiffness of riveted joints with a very low contribution of dofs. A comparison with a joint model performed with very refined non-linear 3D model of rivet and with experimental data is performed and a good agreement is demonstrated.
[1]
Michael Urban,et al.
Analysis of the fatigue life of riveted sheet metal helicopter airframe joints
,
2003
.
[2]
N. Sefa Kuralay,et al.
Stress analysis of a truck chassis with riveted joints
,
2002
.
[3]
Eric Markiewicz,et al.
Riveted joint modeling for numerical analysis of airframe crashworthiness
,
2001
.
[4]
Robert Kliger,et al.
FE analysis of stringer-to-floor-beam connections in riveted railway bridges
,
2003
.
[5]
Y. Xiong,et al.
Analytical and Finite Element Modeling of Riveted Lap Joints in Aircraft Structure
,
1999
.
[6]
Pietro Salvini,et al.
Fatigue Life Prediction On Complex Spot Welded Joints
,
1997
.
[7]
K. T. Chau,et al.
An infinite plane loaded by a rivet of a different material
,
1997
.
[8]
Pietro Salvini,et al.
Enforcing of an analytical solution of spot welds into finite element analysis for fatigue-life estimation
,
2002
.
[9]
Pietro Salvini,et al.
A spot weld finite element for structural modelling
,
2000
.