Affiliation:
1. Institute of Aeronautical Engineering
2. Sri Shakthi Institute of Engineering and Technology
3. Sri Ramakrishna Engineering College
4. Sri Krishna College of Engineering and Technology, Mechanica
5. Sona College of Technology
Abstract
<div class="section abstract"><div class="htmlview paragraph">The increased adoption of AA2014 Aluminum alloy within the manufacturing sector
can be attributed to its lightweight properties and other attributes that
position it as an appealing substitute for steel. Notably, AA2014 Aluminum alloy
is employed in the production of components and frameworks for aircraft engines.
However, conventional welding techniques do not always seamlessly apply to
aluminum alloys due to aluminum's high thermal conductivity, pronounced
susceptibility to oxidation, and comparatively low melting point. These
characteristics can give rise to challenges such as burn-through and porosity
during welding. To tackle these issues, the application of friction stir welding
(FSW), a solid-state welding method, has been embraced. In the creation of lap
joints, five distinct tools, each featuring a different ratio of tool shoulder
diameter (D) to pin diameter (d), ranging from 2 to 4, were employed. An
exhaustive evaluation of the mechanical and metallurgical properties of these
lap joints was conducted, establishing correlations with the microstructure and
microhardness of the stir zone. The outcomes of this investigation disclose that
the lap joint crafted using a D/d ratio of 3.0 showcases superior mechanical
attributes when compared to lap joints produced at other D/d ratios. This
enhancement is attributed to the emergence of finely refined grain structures
within the stir zone during the friction stir welding process, coupled with
heightened levels of hardness. These elevated hardness levels are identified as
the primary contributors to the favorable mechanical and metallurgical qualities
observed within the joint.</div></div>