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