2020
DOI: 10.3390/ma14010008
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The Number of Subgrain Boundaries in the Airfoils of Heat-Treated Single-Crystalline Turbine Blades

Abstract: In the present study, the dendrites deflection mechanism from the mold walls were subjected to verification regarding its heat-treated turbine rotor blades. The number of macroscopic low-angle boundaries created on the cross-section of the blades’ airfoil near the tip was experimentally determined and compared to the number of low-angle boundaries calculated from a model based on the dendrites deflection mechanism. Based on the Laue patterns and geometrical parameters of airfoils, the number of low-angle bound… Show more

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Cited by 5 publications
(5 citation statements)
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“…They observed decreasing primary dendrite arm spacings in increasingly thinner casting geometries. Similar observations were made by Krawczyk and Bogdanowicz [ 11 ] in single‐crystal cored turbine blades in the vicinity of the cooling bores. These areas with smaller primary dendrite arm spacings around the cooling bores are about 3–4 mm wide and already clearly indicate a dependence of the primary dendrite arm spacing on the wall thickness.…”
Section: Introductionsupporting
confidence: 87%
“…They observed decreasing primary dendrite arm spacings in increasingly thinner casting geometries. Similar observations were made by Krawczyk and Bogdanowicz [ 11 ] in single‐crystal cored turbine blades in the vicinity of the cooling bores. These areas with smaller primary dendrite arm spacings around the cooling bores are about 3–4 mm wide and already clearly indicate a dependence of the primary dendrite arm spacing on the wall thickness.…”
Section: Introductionsupporting
confidence: 87%
“…The topograms were recorded with the use of 113-type reflections. The method is described in detail in [ 32 , 33 , 34 ].…”
Section: Methodsmentioning
confidence: 99%
“…In the airfoil of the blades, dendritic segregation has a very complex nature, as the set of parallel dendrites crystallises in a reasonably narrow area between the suction and pressure surfaces of the airfoil. The changes in the chemical composition and a γ heterogeneity around the LABs, in this case, can have complex mechanisms related to the crystallisation of the dendrites near the surface of the casting mould [18]. However, in the bulk root, the side surfaces are mostly parallel to the direction of crystallisation.…”
Section: Of 13mentioning
confidence: 99%