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Creep and Tensile Behavior of a Nickel-Based Single Crystal Superalloy With a Bimodal γ′ Precipitation
High temperature aircraft engines components made from single crystal nickel-based superalloys typically have homogenous γ / γ ′ microstructure after conventional solution and aging heat treatments. However, manufacturing processes as well as service conditions may alter the material’s microstructur...
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Published in: | Metallurgical and materials transactions. A, Physical metallurgy and materials science Physical metallurgy and materials science, 2023-05, Vol.54 (5), p.1496-1508 |
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Main Authors: | , , , , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | High temperature aircraft engines components made from single crystal nickel-based superalloys typically have homogenous
γ
/
γ
′ microstructure after conventional solution and aging heat treatments. However, manufacturing processes as well as service conditions may alter the material’s microstructure which can lead to a multimodal
γ
′ precipitation with regular secondary precipitates (400 to 500 nm) and smaller (10 to 100 nm) tertiary precipitates. In this study, such a bimodal microstructure was first obtained after a heat treatment study and the impact of such a microstructure on mechanical behavior was then investigated. Tensile and creep properties are sensitive to such a bimodal microstructure below 900 °C with a 60 to 120 MPa reduction in yield stress and a creep lifetime reduced by factors of 2 to 15 compared to a unimodal reference microstructure. It is suggested that tertiary
γ
′ precipitates facilitates secondary
γ
′ shearing reducing tensile and creep properties. Above 900 °C, no difference in tensile and creep behavior has been observed between both kinds of microstructure as tertiary precipitates are rapidly dissolving. |
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ISSN: | 1073-5623 1543-1940 |
DOI: | 10.1007/s11661-023-07022-y |