2014
DOI: 10.1016/j.matdes.2014.08.035
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Effect of long time service exposure on microstructure and mechanical properties of gas turbine vanes made of IN939 alloy

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Cited by 55 publications
(15 citation statements)
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“…1. It is well known [10] that dynamic stresses and temperature are maximal in the convex part of the turbine blade airfoil, at the site termed the suction side (airfoil back). Another place with high stresses is the leading edge of the airfoil.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…1. It is well known [10] that dynamic stresses and temperature are maximal in the convex part of the turbine blade airfoil, at the site termed the suction side (airfoil back). Another place with high stresses is the leading edge of the airfoil.…”
Section: Resultsmentioning
confidence: 99%
“…Under severe deformation, the formation of defects occurs inside the strengthening -phase cuboids. The formation of a stable defect complex inside the '-phase indicates the softening of the intermetallic phase [10]. Planar structural defects may change the atomic positions in the intermetallic crystal lattice and promote a "cluster", a volume structural defect with ferromagnetic ordering [5].…”
Section: Transmission Electron Microscopy Studymentioning
confidence: 99%
“…The role of carbides has been proved complex, high temperature properties of superalloys can be improved effectively due to the preferred location of carbides at GBs and inhibition of GB sliding [20,21]. However, the continuous M 23 C 6 carbide films formed along the GBs dramatically reduced the stress-rupture life [22,23]. And the plate and strip-like Cr 23 C 6 carbide is found at the large and small transition region GBs (Fig.…”
Section: Schematic Precipitate Behavior Of C 0 and Carbidesmentioning
confidence: 99%
“…They have been widely used in aircraft and power-generation turbines as nozzle guide vanes, blades, rotating parts, etc. [1][2][3].…”
Section: Introductionmentioning
confidence: 99%