Publication Type:

Conference Paper

Source:

IOP Conference Series: Materials Science and Engineering, Institute of Physics Publishing, Volume 225 (2017)

URL:

https://www.scopus.com/inward/record.uri?eid=2-s2.0-85032182574&doi=10.1088%2f1757-899X%2f225%2f1%2f012037&partnerID=40&md5=fbeaa0b3b3c67633e028e9ffa0972e8d

Keywords:

Aircraft materials, Aluminum, Aluminum alloys, Automobile manufacture, corrosion, Corrosion resistance, Corrosive conditions, Corrosive environment, electric conductivity, Electrical conductivity, exfoliation corrosion, Experimental analysis, Fighter aircraft, Grain boundaries, Heat treatment, High strength alloys, High-tensile strength, Industrial environments, Intergranular corrosion, stress corrosion cracking, Tensile strength

Abstract:

<p>Aluminium alloys are increasingly being used in the manufacture of structures of airplanes and automobiles due to their superior properties such as high strength to weight ratio and excellent mechanical properties. AA7010 Al alloy is a 7xxx series alloy that is mainly used in the aircraft industries. Al 7010 is said to have high tensile strength as well as high fatigue strength. It is also stress corrosion resistant. However due to exposure to extreme marine and industrial environments, the metal may be subjected to corrosion such as exfoliation corrosion. Exfoliation is a special form of intergranular corrosion that proceeds laterally from the sites of initiation along planes parallel to the surface, generally at grain boundaries, forming corrosion products that force metal away from the body of the material, giving rise to a layered appearance. Exfoliation corrosion may cause heavy damage to aircrafts in the long run. In the present work, the test has been conducted on A17010 samples for the determination of rate and extent of exfoliation corrosion by subjecting them to artificial corrosive conditions that mimic the actual marine and industrial environments. The samples are heat treated to T6 and T7 tempers prior subjecting them to the corrosive environments, as most of the aircraft materials are subjected to T6 and T7 tempers to enhance the properties before being put to commercial use. Samples are tested according to ASTM G34 and rated by comparing them with standard photographs. Also electrical conductivity tests on the samples have been carried out which reveals that the electrical conductivity of the Al 7010 alloy increases upon heat treatment.</p>

Notes:

cited By 0; Conference of 1st International Conference on Materials, Alloys and Experimental Mechanics, ICMAEM 2017 ; Conference Date: 3 July 2017 Through 4 July 2017; Conference Code:130336

Cite this Research Publication

A. Choudhury, Gopakumar, A., Athul, K. P., Adinath, D. R., and Prashanth, M., “Experimental analysis of exfoliation rate on aluminum alloy Al7010”, in IOP Conference Series: Materials Science and Engineering, 2017, vol. 225.

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