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Mechanisms of high-temperature creep of nickel-based superalloys under low applied stresses
205
Citations
20
References
2004
Year
EngineeringSevere Plastic DeformationMechanical EngineeringHigh-temperature CreepNickel-based SuperalloysWork HardeningElectron MicroscopySuperalloys Cmsx-4Microstructure-strength RelationshipMaterials ScienceCrystalline DefectsHot WorkingPlasticityMicrostructureHigh Temperature MaterialsSuperalloyMechanical PropertiesPorosity GrowthDislocation InteractionMechanics Of Materials
[001] single-crystal specimens of the superalloys CMSX-4 and CMSX-10 were tested for creep at 1100°C under tensile stresses between 105 and 135 MPa, where they show pronounced steady creep. The deformed superalloys were analysed by density measurements, scanning electron microscopy and transmission electron microscopy which supplied information about porosity growth, evolution of the γ–γ′ microstructure, dislocation mobility and reactions during creep deformation. It is shown that, under the testing conditions used, steady creep strain mostly results from transverse glide–climb of (a/2) ⟨011⟩ interfacial dislocations. A by-product of the interfacial glide–climb are vacancies which diffuse along the interfaces to growing pores or to a ⟨100⟩ edge dislocations climbing in the γ′ phase. Climb of a ⟨100⟩ dislocations in the γ′ phase is a recovery mechanism which reduces the constraining of the γ phase by the γ′ phase, thus enabling further glide of (a/2) ⟨011⟩ dislocations in the matrix. Moreover the γ′ dislocations act as vacancy sinks facilitating interfacial glide–climb. The creep rate increases when the γ–γ′ microstructure becomes topologically inverted; connection of the γ′ rafts results in extensive transverse climb and an increase of the number of a⟨100⟩ dislocation segments in the γ′ phase.
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