Flexural Effects Evaluation on Hybrid Joints Under Uniaxial Tensile Load

Abstract

Hybrid joints are a wide diffused design solution in the manufacturing industry for mechanical parts connection. The simultaneous use of two different connection mechanisms, such as bonding and bolting, allows to exploit the advantages of both techniques. There are many industrial applications where such methodology is extensively used, such as the automotive and aerospace ones. In addition to the many advantages offered by the use of hybrid joints, there are some troubles that limit their use and require the scientific research support for the development of such connections. With reference to a single lap joint, the flexural effects induced by the joint geometry are not negligible. The inhomogeneity of the joint along the load application direction inevitably determines significant bending effects, the more evident the thinner the adherends that constitute the joint. The bending effects can also lead to excessive section rotation, inducing effects of binding between washer and adherend. Such effect is even more evident in the case of polymeric composite adherends, rapidly leading the joint to a catastrophic end. In the present work some interesting experimental tests are shown, varying geometrical parameters of the joint.

Damage Analysis of Hybrid Composites Under Multi-Impact Loads: An Experimental and Numerical Study

“…The anisotropic and heterogeneous character of Fiber Reinforced Polymers (FRP), together with their capability to offer high mechanical performance in terms of stiffness and strength in reduced weight, spread their application in the industrial field both for structural and non-structural purposes [1,2,3,4,5]. This drove many studies to investigate the FRP mechanical response under quasi-static and dynamic load conditions [6,7,8,9].Since not easily identifiable by visual inspection, or barely visible on the component surface, the damage from foreign object impact resulted to be a critical condition for this class of materials. Even when undetectable, the damage consequent to impact loads, can significantly reduce the laminate strength by promoting material failure also under operating loads [10,11,12].…”