2018
DOI: 10.1007/s10973-018-7085-2
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Homogenization heat treatment and segregation analysis of equiaxed CMSX-4 superalloy for gas turbine components

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Cited by 10 publications
(4 citation statements)
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“…However, it has been stated that not all macroscopic LABs are eliminated by the heat treatment but also that new extra LABs may be created as a result of this treatment. All of the LABs decrease the strength of the rotor blades [24][25][26].…”
Section: Introductionmentioning
confidence: 99%
“…However, it has been stated that not all macroscopic LABs are eliminated by the heat treatment but also that new extra LABs may be created as a result of this treatment. All of the LABs decrease the strength of the rotor blades [24][25][26].…”
Section: Introductionmentioning
confidence: 99%
“…Investigations were carried out on other alloys, using the same methodology as in this paper. A combination of CALPHAD (CALculation of PHAse Diagrams) and differential scanning calorimetry (DSC) has been successfully used to determine the optimum homogenization parameters and to understand the phase transformations during this process [23][24][25]. In particular, the impact of homogenization on changes in the morphology of Fe-constituents, which are known to have a significant effect on formability, was investigated.…”
Section: Introductionmentioning
confidence: 99%
“…Owing to remarkable mechanical properties and oxidation resistance at high temperature, Nibased superalloys are commonly used materials for hightemperature applications such as turbine blades and disks in aircraft engines and industrial steam turbines [2,3]. In general, conventional Co-based superalloys possess superior corrosion resistance; however, they exhibit lower mechanical properties in comparison with those of c 0 -strengthened Ni-based superalloys; hence, these alloys are used for mechanically lower loaded gas turbine vanes, where appropriate performance in corrosive environments is required [4].…”
Section: Introductionmentioning
confidence: 99%