• Nikhil Dev
• Sandeep Kumar
• Rajesh Attri

Design and maintenance of gas turbine system is a very complex phenomena. Therefore, it is required to develop some methodology which is helpful for the cost saving and health monitoring of the gas turbine system. There are many points of deliberation for the maintenance. Such as blade casing is made soft. In case blade strikes with casing then casing must be rubbed off and blade must be saved. Blade design of gas turbine system is comprised of design of fan blade, compressor blade and gas turbine blade. Fan blade is pushing the air in the backward direction and in return air pushes it in the forward direction. A tip stresses are maximum. At the time of take-off maximum amount of thrust is required. Structure of gas turbine system is stretching type. To minimise the problem of maintenance a methodology for the assessment of maintenance criticality index (MCI) is proposed on the basis of GTA.

GTA, Gas turbine, Maintenance

"Gas Turbine Power System Maintenance Strategy", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 2, page no.951-955, February-2019, Available :http://www.jetir.org/papers/JETIRAB06179.pdf

"Gas Turbine Power System Maintenance Strategy", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 2, page no. pp951-955, February-2019, Available at : http://www.jetir.org/papers/JETIRAB06179.pdf