2018
DOI: 10.1016/j.ijmecsci.2018.04.018
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Prediction method for creep life of thin-wall specimen with film cooling holes in Ni-based single-crystal superalloy

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Cited by 66 publications
(13 citation statements)
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“…NSCS is the most commonly used material for turbine blades of advanced aero-engines today [1][2][3][4][5][6], and most single crystal turbine blades are produced by casting that entails controlling the growth direction of the principal stress axis [7]. Generally, the direction of the main stress axis is called primary orientation, which has a significant impact on the arm spacing of primary dendrites, creep properties or stress fracture life, etc.…”
Section: Introductionmentioning
confidence: 99%
“…NSCS is the most commonly used material for turbine blades of advanced aero-engines today [1][2][3][4][5][6], and most single crystal turbine blades are produced by casting that entails controlling the growth direction of the principal stress axis [7]. Generally, the direction of the main stress axis is called primary orientation, which has a significant impact on the arm spacing of primary dendrites, creep properties or stress fracture life, etc.…”
Section: Introductionmentioning
confidence: 99%
“…The increase of inlet temperature of turbine engine will inevitably lead to a sharp increase of heat load on the hot end parts. Film cooling has been widely used in turbine blades because of its inherent high efficiency cooling characteristics, and has become one of the main cooling measures for high temperature components of aero-gas turbine engines [1][2][3]. Coolant flow is introduced from the hole on the cooling wall to the primary stream.…”
Section: Introductionmentioning
confidence: 99%
“…In the context of aviation manufacturing, a large number of microscopic cooling holes are present in films on the surfaces of the turbine blades of aero-engines [1][2][3], and these micro-holes are distributed on the blades at different angles [4][5][6]. Such a structure can be used to form a film of cooling gas on the surface of the blade to ensure its reliable operation in the ultra-high-temperature environment of the combustion chamber [7][8][9].…”
Section: Introductionmentioning
confidence: 99%