A Finite Element Model for Predicting the Static Strength of a Composite Hybrid Joint with Reinforcement Pins

Author:

Bianchi Francesco1,Liu Yiding2ORCID,Joesbury Adam M.1ORCID,Ayre David1,Zhang Xiang3ORCID

Affiliation:

1. Composites and Advanced Materials Centre, School of Aerospace, Transport and Manufacturing, Cranfield University, Bedford MK43 0AL, UK

2. School of Physics, Engineering & Computer Science, University of Hertfordshire, Hatfield AL10 9AB, UK

3. Centre for Manufacturing and Materials, Coventry University, Coventry CV1 5FB, UK

Abstract

This paper presents a finite element model for predicting the performance and failure behaviour of a hybrid joint assembling fibrous composites to a metal part with reinforcement micro pins for enhancing the damage tolerance performance. A unit-strip model using the cohesive elements at the bond interface is employed to simulate the onset and propagation of debonding cracks. Two different traction–separation laws for the interface cohesive elements are employed, representing the fracture toughness properties of the plain adhesive bond and a pin-reinforced interface, respectively. This approach can account for the large-scale crack-bridging effect of the pins. It avoids using concentrated pin forces in the numerical model, thus removing mesh-size dependency, and permitting more accurate and robust computational analysis. Lap joints reinforced with various pin arrays were tested under quasi-static load. Predicted load versus applied displacement relations are in good agreement with the test results, especially for the debonding onset and early stage of crack propagation.

Funder

Cranfield University Innovative Manufacturing Research Centre project “Bridging the Divide”

Publisher

MDPI AG

Subject

General Materials Science

Reference43 articles.

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3. Hart-Smith, L.J. (1973). Adhesive-Bonded Double-Lap Joints, NASA-CR-112235.

4. Review on Adhesive Joints and Their Application in Hybrid Composite Structures;Jeevi;J. Adhes. Sci. Technol.,2019

5. Review of Z-Pinned Composite Laminates;Mouritz;Compos. Part A Appl. Sci. Manuf.,2007

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