2013
DOI: 10.3390/ma6031118
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Recent Advances in Creep Modelling of the Nickel Base Superalloy, Alloy 720Li

Abstract: Recent work in the creep field has indicated that the traditional methodologies involving power law equations are not sufficient to describe wide ranging creep behaviour. More recent approaches such as the Wilshire equations however, have shown promise in a wide range of materials, particularly in extrapolation of short term results to long term predictions. In the aerospace industry however, long term creep behaviour is not critical and more focus is required on the prediction of times to specific creep strai… Show more

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Cited by 31 publications
(26 citation statements)
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“…A wide range of materials [24,25,26,27] have now been studied for which optimised fits are obtained when the value of the apparent activation energy (Q c *) is allowed to vary either side of the break point. Interestingly, the most significant changes in the apparent activation energy observed have been in stainless steel grade 316, with values of 250 kJ/mol observed above the yield stress, decreasing to 150 kJ/mol below.…”
Section: Introductionmentioning
confidence: 99%
“…A wide range of materials [24,25,26,27] have now been studied for which optimised fits are obtained when the value of the apparent activation energy (Q c *) is allowed to vary either side of the break point. Interestingly, the most significant changes in the apparent activation energy observed have been in stainless steel grade 316, with values of 250 kJ/mol observed above the yield stress, decreasing to 150 kJ/mol below.…”
Section: Introductionmentioning
confidence: 99%
“…The microstructure consists of a grain size of approximately 6-32 µm with primary γ ' (Ni 3 (Al,Ti)) measuring 3-5 µm distributed on the grain boundaries, and secondary γ ' measuring 70-120 nm, shown in Fig. 1 [2]. The chemical composition of 720Li is reported in Table 1.…”
Section: Methodsmentioning
confidence: 99%
“…The Ni-based polycrystalline wrought superalloys have been developed to provide superior mechanical properties and good corrosion resistance at high temperatures, leading to a wide application on manufacturing turbine disks, blades and vanes in gas turbines and aero-engines. The high temperature strength is usually provided by a distribution of γ' (Ni 3 (Al, Ti)) precipitates which hinder dislocation movement [1]. To obtain the properties of these materials under the conditions of service, experimental investigations has been previously carried out and complex deformation behaviors have been exhibited [2][3][4][5][6].…”
Section: Introductionmentioning
confidence: 99%