2022
DOI: 10.1007/s11661-022-06620-6
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Influence of the Co/Ni Ratio and Dendritic Segregations on the High-Temperature Oxidation Resistance of Multinary Co-Rich Superalloys at 850 °C and 1050 °C

Abstract: Excellent inherent oxidation resistance is a prerequisite for the use of superalloys in many high-temperature applications. To achieve this goal, typically continuous alumina and chromia scale growths are assured through sufficient Cr and Al additions. Since the intended γ/γ′-microstructure of superalloys is only stable within a certain compositional window, the maximum concentrations of these protective scale forming elements are, however, dependent on the overall alloy composition. The latter is a severe dra… Show more

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Cited by 4 publications
(2 citation statements)
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“…The sections of the γ phase and γ ′ phase are shown in Figure 8a,b, respectively, and the blue atoms in Figure 8b are Al atoms. Due to the deviation in lattice constants between the γ phase and the γ ′ phase, there are mismatched dislocations in the interface of the model, and the dislocation density is an important factor affecting the performance of Ni-based single crystal alloys [10][11][12][13][14][15]. The corresponding γ/γ ′ phase interfaces of the six models are shown in Figure 9, and the yellow atoms are Re atoms.…”
Section: Resultsmentioning
confidence: 99%
“…The sections of the γ phase and γ ′ phase are shown in Figure 8a,b, respectively, and the blue atoms in Figure 8b are Al atoms. Due to the deviation in lattice constants between the γ phase and the γ ′ phase, there are mismatched dislocations in the interface of the model, and the dislocation density is an important factor affecting the performance of Ni-based single crystal alloys [10][11][12][13][14][15]. The corresponding γ/γ ′ phase interfaces of the six models are shown in Figure 9, and the yellow atoms are Re atoms.…”
Section: Resultsmentioning
confidence: 99%
“…The manufacture of finished products from intermetallic materials is a promising direction in the aerospace and automotive industries for turbine blades, bearings, and exhaust valves [4][5][6]. The replacement of currently existing nickel-based superalloys [7][8][9] with alloys based on titanium aluminides will make it possible to reduce the weight of gas turbine engine parts by up to 1.5-2 times (density of nickel superalloys is about 9 g/cm 3 , whereas that for alloys based on γ-TiAl is about 4 g/cm 3 ). In addition, this will also reduce the cost of their manufacture by up to 30%.…”
Section: Introductionmentioning
confidence: 99%