A review on aircraft joints design

Abstract

Purpose

The purpose of this paper is to present a review about sizing of joints, from the static and fatigue points of view. A discussion about advantages and disadvantages of each joining technology, among the ones mentioned above, will be presented.

Design/methodology/approach

Although many other aspects will be discussed, emphasis will be given to the joint fatigue behavior, and fatigue test results will be presented and discussed.

Findings

This paper is a subject review, where no new findings are presented. However, the comparison of fatigue test results for mechanically fastened joints and friction stir welding joints will show the advantages of the latter.

Practical Implications

With the information presented, the authors expect to provide some guidelines that will help to improve future joint designs.

Originality/value

The review information contained in this paper may be used as reference for aircraft joint design.

Citation

Chaves, C.E. and Fernandez, F.F. (2016), "A review on aircraft joints design", Aircraft Engineering and Aerospace Technology, Vol. 88 No. 3, pp. 411-419. https://doi.org/10.1108/AEAT-10-2012-0184