2019
DOI: 10.3139/146.111729
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Evolution of γ′ morphology and γ/γ′ lattice parameter misfit in a nickel-based superalloy during non-equilibrium cooling

Abstract: The change of γ′ phase morphology in quenched Ni-based superalloy strengthened by γ′ precipitates was investigated by means of scanning electron microscopy and X-ray diffraction. Lattice parameters of γ and γ′ phases and subsequently the δ parameter were calculated. Relatively high content of gamma prime formers resulted in a substantially high volume fraction of precipitates in the dendrite cores. The volume fraction of γ′ phase was significantly decreased due to dissolution of precipitates in the surrounding… Show more

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Cited by 11 publications
(12 citation statements)
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“…Indeed, the thermal expansion coefficient of Si is much lower than that of Al, with the difference being higher than most other light-alloy-precipitate combinations. These effects can combine to cause the same phase to form in two morphologies, as also shown for Ni-based superalloys, for instance [165][166][167][168]. depletes the matrix, leading to a slowed reaction.…”
Section: Alsi Binary Wrought Alloysmentioning
confidence: 96%
“…Indeed, the thermal expansion coefficient of Si is much lower than that of Al, with the difference being higher than most other light-alloy-precipitate combinations. These effects can combine to cause the same phase to form in two morphologies, as also shown for Ni-based superalloys, for instance [165][166][167][168]. depletes the matrix, leading to a slowed reaction.…”
Section: Alsi Binary Wrought Alloysmentioning
confidence: 96%
“…The unique combination of high strength and excellent oxidation resistance makes it an irreplaceable group of materials in aerospace, power, and nuclear industries. The usefulness of Ni-based superalloys during long-term service at harsh conditions depends strongly on the alloying elements, their concentrations, and the morphology of the main strengthening phases [ 1 , 2 , 3 , 4 ]. The development of the first Ni-based superalloys began over 100 years ago.…”
Section: Introductionmentioning
confidence: 99%
“…In the 1940s, engine components were manufactured by forging and air casting and so the strength and metallurgical purity were not the highest. The introduction of vacuum casting technology in 1952 was considered to be the most essential step towards improving the mechanical properties and purity of both cast and wrought superalloys [ 4 , 14 ]. Before the advent of vacuum melting and casting techniques, cast superalloys did not gain wide acceptance for a turbine blade application.…”
Section: Introductionmentioning
confidence: 99%
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“…The intermetallic phase is very rigid and impedes dislocation movement from the matrix, thus resulting in the required strength. By selecting appropriate technological parameters during casting and heat treatment, a microstructure favorable for the expected service temperature of the jet engines can be attained [2,3]. Service conditions often cause premature failure of components due to hot corrosion and LCF (low cycle fatigue) cracking.…”
Section: Introductionmentioning
confidence: 99%