The Strength Analysis of Hybrid (Bolted and Bonded) Single Lap joints for Composite Materials
Mahesh J. Patil1, Rajendrakumar N. Patil2
1Mahesh J. Patil*, Mechanical department, Bharati Vidyapeeth (Deemed to be University) College of Engineering, Pune, India.
2Prof. Dr. Rajendra Kumar N. Patil, Principal, Bharati Vidyapeeth’s College of Engineering, Lavale, Pune, India.
Manuscript received on September 17, 2019. | Revised Manuscript received on 28 September, 2019. | Manuscript published on October 10, 2019. | PP: 4689-4692 | Volume-8 Issue-12, October 2019. | Retrieval Number: L3580081219/2019©BEIESP | DOI: 10.35940/ijitee.L3580.1081219
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© The Authors. Blue Eyes Intelligence Engineering and Sciences Publication (BEIESP). This is an open access article under the CC-BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)
Abstract: The two joining techniques i.e. adhesive bonding and mechanical fastening combined are termed as hybrid joints. These kinds of joints mix the benefits of each the joining ways. The composite materials are used in structures at larger extend because of its properties like high strength to weight ratio, high fatigue resistance, high impact strength etc. The paper evaluates the mechanical behavior of Hybrid joint using composite as adherents subjected to tensile loading. The joint was observed to fail in two stages. Initially because of failure of adhesive and later by the failure of the bolt. The different parameters like overlap length, bolt size, tightening torque and adhesive thickness were studied and the significant factor were found to be overlap length, bolt size and tightening torque
Keywords: Adhesive, Bolt, Composite Material, Hybrid Joint.
Scope of the Article: Composite Material