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Comparative Analysis of SS 301 with Current Scenarios of Gas Turbine Disc Material for Possible Use in Gas Turbine Disc

Author(s):

Vinay Kumar Soni , school of engg. & it / mats university; Brijesh Patel, school of engg. & it / mats university; Kamal Kumar Pradhan, school of engg. & it / mats university

Keywords:

SS 301, IN 718, IN 706, A 286, Gas Turbine Disc

Abstract

SS 301L (S30100), SS301 LN which contains up to 8 % of Nickel, and 18 % of chromium is most familiar and most frequently member of stainless steel family and a key limiting factor in early jet engines was the performance of the materials available for the hot section (disc) of the engine. The need for better materials spurred much research in the field of alloys and developing method and that research resulted in a long list of new materials and methods that make modern gas turbines possible.

Other Details

Paper ID: IJSRDV4I31085
Published in: Volume : 4, Issue : 3
Publication Date: 01/06/2016
Page(s): 1336-1338

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