Assessment of the possibility of replacing solid rivets in joints of aircraft structure
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Keywords

riveted joints, double-sided rivets and one-sided rivets, fatigue durability of riveted joints

How to Cite

Rośkowicz, M., Tkaczuk, S., Komorek, A., & Gąsior, J. (2018). Assessment of the possibility of replacing solid rivets in joints of aircraft structure. Technologia I Automatyzacja Montażu (Assembly Techniques and Technologies), 100(2), 53-56. Retrieved from https://czasopisma.prz.edu.pl/tiam/article/view/987

Abstract

The paper presents the results of experimental research, the aim of which was to assess the possibility of replacing rivets with solid one-sided rivets in connections of aircraft structures. Because one-sided rivets, in contrast to solid rivets, consist of many elements, the evaluation as a comparative criterion assumes not only the load capacity of connections, but also the resistance to the phenomenon of automatic dismantling of one-sided rivets subjected to a variable load. In fatigue tests, it was found that there is a possibility of replacing rivets with solid one-sided rivets, but the fatigue life of joints of one-sided joint connections depends significantly on the place of rupture of the one-sided blind pin in its heading process.

This is an Open Access article distributed under the terms of the Creative Commons Attribution License CC BY 4.0 (https://creativecommons.org/licenses/by/4.0/)

PDF (Polish)

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