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Development of heat-treatment process for a P/M superalloy for turbine blades

โœ Scribed by Zainul Huda


Publisher
Elsevier Science
Year
2007
Weight
332 KB
Volume
28
Category
Article
ISSN
0261-3069

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The stress rupture characteristics of bare and thermal barrier coated (TBC) superalloy AE 437A were determined in air at temperatures between 600 and 850 โ€ข C with both short and long term testing undertaken at 800 โ€ข C. Because the bond coat contributed an addition โˆผ10% cross-sectional area and was a