DC pole | Wartość | Język |
dc.contributor.author | Krawczyk, Jacek | - |
dc.contributor.author | Bogdanowicz, Włodzimierz | - |
dc.contributor.author | Sieniawski, Jan | - |
dc.date.accessioned | 2021-01-13T09:57:32Z | - |
dc.date.available | 2021-01-13T09:57:32Z | - |
dc.date.issued | 2021 | - |
dc.identifier.citation | "Materials" 2021, iss. 1, art. no. 8 | pl_PL |
dc.identifier.issn | 1996-1944 | - |
dc.identifier.uri | http://hdl.handle.net/20.500.12128/18314 | - |
dc.description.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 boundaries occurring at the upper part of the blades airfoil after heat treatment was calculated. This number for the analyzed group of blades ranged from 5 to 9. | pl_PL |
dc.language.iso | en | pl_PL |
dc.rights | Uznanie autorstwa 3.0 Polska | * |
dc.rights.uri | http://creativecommons.org/licenses/by/3.0/pl/ | * |
dc.subject | superalloys | pl_PL |
dc.subject | low-angle boundaries | pl_PL |
dc.subject | X-ray topography | pl_PL |
dc.subject | turbine blades | pl_PL |
dc.subject | crystal growth | pl_PL |
dc.title | The Number of Subgrain Boundaries in the Airfoils of Heat-Treated Single-Crystalline Turbine Blades | pl_PL |
dc.type | info:eu-repo/semantics/article | pl_PL |
dc.identifier.doi | 10.3390/ma14010008 | - |
Pojawia się w kolekcji: | Artykuły (WNŚiT)
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