2022
DOI: 10.1007/s41230-022-1092-4
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Optimization of investment casting process for K477 superalloy aero-engine turbine nozzle by simulation and experiment

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Cited by 9 publications
(3 citation statements)
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“…(2) vp (1) vp e (3) vp where, is the strain rate under uniaxial load; C and j are the coefficients correlated to the strain rate.…”
Section: Perzyna Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…(2) vp (1) vp e (3) vp where, is the strain rate under uniaxial load; C and j are the coefficients correlated to the strain rate.…”
Section: Perzyna Modelmentioning
confidence: 99%
“…which are widely used in aerospace fields, such as aeroengines, turbine blades and disks, etc [1] . As the engine thrust increases, the inlet temperature of the turbine increases accordingly, which puts forward higher requirements for the mechanical properties of the alloy.…”
mentioning
confidence: 99%
“…
Ni-based single-crystal superalloys have been extensively utilized in aero-engines for the production of hot-end components due to their excellent high-temperature mechanical properties [1][2][3][4] . In the pursuit of heightened thermal efficiency, single-crystal superalloys are progressively being introduced into industrial gas turbines (IGTs) [5][6][7] to fabricate single-crystal blades, thereby enhancing the turbine front-end temperature.
…”
mentioning
confidence: 99%