A Study of Erosion Rate of Homogenized Structural AL7175 Alloy for Aircraft Application

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Authors

  • Sujeet Magi
     PG Scholar, Department of Mechanical Engineering, RIT, Bengaluru, Karnataka ,IN
  • C.M. Ramesha
     Department of Mechanical Engineering, RIT, Bengaluru, Karnataka ,IN
  • Girish V Kulkarni
     Department of Mechanical Engineering, RIT, Bengaluru, Karnataka ,IN
  • Rajendra. P
     Department of Mechanical Engineering, RIT, Bengaluru, Karnataka ,IN
  • Anil Kumar P.
     Department of Mechanical Engineering, RIT, Bengaluru, Karnataka ,IN
  • Mohanraju. S
     Research scholar, Department of Mechanical Engineering, RIT, Bengaluru, Karnataka ,IN

Keywords:

Structural Alloys, Aircraft, light weight, Aviation, fine grain structure, heat-treated, erodent discharge.

Abstract

Structural alloys (Al7175) are widely used in aviation, marine, automobile and aerospace application due to their special characteristics such as high strength to weight ratio, high ductility, light weight, good corrosion resistance, low density, good thermal and electrical conductivity. Improvement in the microstructural, mechanical properties of this alloy can be achieved by homogenization process. Aluminum alloys were subjected to heat treatment to obtain a fine grain structure. Heat treated and as-cast aluminium alloy processed material were characterized using scanning electron microscope, x-ray diffraction, hardness test and erosion test. Material loss in structural materials is aggravated by erosive action and create a massive problem in industrial application such as turbine, agriculture equipment, pumps etc. Study of erosion behaviour on the structural aluminum alloy composite, erosion test of structural aluminum alloy composites was performed at different impingement angle (30º and 90º) and at specified velocity of erodent using erosion test machine (Air Jet Erosion Tester TR-471-800). Investigation was carried out as-cast aluminium alloy Al7175 and homogenized alloys, then set of reading were recorded at 50 m/s velocity of erodent by keeping other parameters like erodent discharge, impingement angle and temperature are variables parameters to obtain the erosion rate.

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Published

2023-09-12

How to Cite

Magi, S., C.M. Ramesha, Kulkarni, G. V., Rajendra. P, Anil Kumar P., & Mohanraju. S. (2023). A Study of Erosion Rate of Homogenized Structural AL7175 Alloy for Aircraft Application. Journal of Mines, Metals and Fuels, 71(7), 900–907. Retrieved from http://www.informaticsjournals.com/index.php/jmmf/article/view/34731

Issue

Volume 71, Issue 7, July 2023

Section

Articles

License

Creative Commons License

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.

 

References

Hirsch, Juergen. (1997): “Aluminium alloys for automotive application.” Materials Science Forum. Vol. 242. Trans Tech Publications Ltd.

Jawalkar, C. S., and Suman Kant. (2015): “A review on use of aluminium alloys in aircraft components.” i-Manager’s Journal on Material Science 3.3 (2015): 33.

Wanhill, R. J. H. (2013): Aluminum-Lithium Alloys: Chapter 15. Aerospace Applications of Aluminum–Lithium Alloys. Elsevier Inc. Chapters.

Gohardani, Omid. (2011): “Impact of erosion testing aspects on current and future flight conditions.” Progress in Aerospace Sciences 47.4 (2011): 280-303.

Kleis I, Kulu P. (2007): Solid particle erosion: occurrence, prediction and control. Springer. p.206. ISBN: 1848000286

Federal Aviation Administration, Airport Foreign Object Debris (FOD). US Department of Transportation. 2009.

Spiro CL, Fric TF, Leon RM. (1997): Aircraft anti-insect system. US Patent 5,683,062.

Zagainov GI, Lozino-Lozinsky GE. (1996): Composite materials in aerospace design. Springer. p.445. ISBN: 0412584700.

Ramesh, M. R., et al. (2010): “Solid particle erosion of HVOF sprayed WC-Co/NiCrFeSiB coatings.” Wear 269.3-4 (2010): 197-205.

Arul, Sanjivi. (2020): “Effect of nickel reinforcement on micro hardness and wear resistance of aluminium alloy Al7075.” Materials Today: Proceedings 24 (2020): 1042-1051.

Yamano R. Journal of Mining and Metallurgy. Section B: Metallurgy 50.1 (2014) 45-52

Davis, Joseph R. (1993): Aluminum and aluminum alloys. ASM international.

Ke L, Huang C, Xing L, Huang K. J Alloys Compd503 (2010) 494–499

Matsumuro M, Kitsudo T. Mater Trans47 (2006) 2972–2979.