Abstract

Aluminum structures, and in particular an element of aerostructures, are strongly exposed to the effects of weather conditions. In the case of using new techniques of joining these structural elements, the selection of proper corrosion protection without losing the required properties of the joint may determine its potential application. This paper presents the results of experimental research concerning the influence of corrosion protection on the microstructure and mechanical strength of resistance spot welded (RSW) and refill friction stir spot welded (RFSSW) joints. The tests were carried out on 2024 T3 aluminum alloy, both sides alcladed. For comparison purposes, the following joints were welded: without any protection, with the primer layer, with anodic oxide coating, and with anodic oxide coating plus sealant between the overlapping surface of the welded metal sheet. The samples were visually inspected, and metallographic and mechanical strength examination was conducted. The test results indicate that the application of the protective layers and its type have an impact on the strength of RSW and RFSSW joints. The use of an adhesive or sealant in welded joints provides an increase in the load capacity of the joint.

Highlights

  • Aluminum alloys are the basic group of metallic construction materials used to build aircraft structures

  • This study focuses on the characteristics of various types of joints of elements made of 2024 T3 alloy. This material is characterized by good strength, high yield strength, and formability, which is important in the case of aircraft construction

  • The sets of spot welded joints of 2024 T3 sheets with various types of anti‐corrosion protection were subjected to visual observations

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Summary

Introduction

Aluminum alloys are the basic group of metallic construction materials used to build aircraft structures. They are gradually displaced by more and more advanced composite materials. This study focuses on the characteristics of various types of joints of elements made of 2024 T3 alloy This material is characterized by good strength, high yield strength, and formability, which is important in the case of aircraft construction. The performance of this alloy is mainly the result of the chemical composition and morphology of microstructure phase components, which are directly affected by heat treatment

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