Nickel Nano Particle Composite by Electrodeposition Method

Authors

  • P. R. Ramsheed Student, Department of Aeronautical Engineering, Srinivas Institute of Technology, Mangalore, India
  • S. Jeevan Shetty Student, Department of Aeronautical Engineering, Srinivas Institute of Technology, Mangalore, India
  • S. M. Sachin Student, Department of Aeronautical Engineering, Srinivas Institute of Technology, Mangalore, India
  • M. N. Sunil Kumar Student, Department of Aeronautical Engineering, Srinivas Institute of Technology, Mangalore, India
  • Purshotham P. Katti Student, Department of Aeronautical Engineering, Srinivas Institute of Technology, Mangalore, India

Keywords:

Electrodeposition

Abstract

A turbine blades are the individual component which makes up the turbine section of a gas turbine or stream engine. The turbine blades are responsible for extracting energy from the high temperature, high pressure gas produced by the combustor the turbine is often the limiting component of gas turbine to survive in this difficult environment. Nickel coatings are commonly applied to steel, Nickel and other metal to provide protection against corrosion and abrasion, however most nickel is consumed in decorative finishes, our main aim is to change the characteristics of turbine blades which can withstand high temperature and availability of the material. At present they are using Ni and Rh composite material, we are replacing nickel with mild steel which is easily available in nature and we are giving Ni coating on it.

 

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Published

22-08-2020

How to Cite

[1]
P. R. Ramsheed, S. J. Shetty, S. M. Sachin, M. N. S. Kumar, and P. P. Katti, “Nickel Nano Particle Composite by Electrodeposition Method”, IJRESM, vol. 3, no. 8, pp. 351–355, Aug. 2020.

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Articles