Aircraft Turbine Engine Labyrinth Seal CFD Sensitivity Analysis
This article presents the labyrinth seal radial clearance influence. A generic labyrinth seal of a turbine aircraft engine was modeled. The target is to compare and analyze the influence of the radial clearance and location of teeth. The results can be useful for designing the location of teeth and...
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| Published in: | Applied sciences Vol. 10; no. 19; p. 6830 |
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| Abstract | This article presents the labyrinth seal radial clearance influence. A generic labyrinth seal of a turbine aircraft engine was modeled. The target is to compare and analyze the influence of the radial clearance and location of teeth. The results can be useful for designing the location of teeth and their appropriate setting, especially for materials engineering and engineering technology in general. |
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| AbstractList | This article presents the labyrinth seal radial clearance influence. A generic labyrinth seal of a turbine aircraft engine was modeled. The target is to compare and analyze the influence of the radial clearance and location of teeth. The results can be useful for designing the location of teeth and their appropriate setting, especially for materials engineering and engineering technology in general. Keywords: labyrinth seal; aircraft turbine engine; radial clearance This article presents the labyrinth seal radial clearance influence. A generic labyrinth seal of a turbine aircraft engine was modeled. The target is to compare and analyze the influence of the radial clearance and location of teeth. The results can be useful for designing the location of teeth and their appropriate setting, especially for materials engineering and engineering technology in general. |
| Audience | Academic |
| Author | Pátek, Zdeněk Čížek, Michal Vampola, Tomáš |
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| Cites_doi | 10.1016/B978-0-12-410461-7.00005-5 10.1017/9781316755686.006 10.1201/b13616 10.1016/0020-7225(95)00072-6 10.1515/tjj-2016-0041 10.21496/ams.2020.011 10.14311/AP.2020.60.0038 10.1115/HT2007-32275 10.1007/978-3-319-75979-1 |
| ContentType | Journal Article |
| Copyright | COPYRIGHT 2020 MDPI AG 2020 by the authors. Licensee MDPI, Basel, Switzerland. This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http://creativecommons.org/licenses/by/4.0/). Notwithstanding the ProQuest Terms and Conditions, you may use this content in accordance with the terms of the License. |
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| References | (ref_12) 2020; 60 ref_14 Ilieva (ref_9) 2019; 50 Vampola (ref_13) 2019; 23 Furst (ref_10) 2015; 826 ref_1 Subramanian (ref_11) 2018; 35 ref_3 ref_15 ref_8 ref_5 ref_4 Eser (ref_2) 1995; 33 ref_7 ref_6 |
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| Snippet | This article presents the labyrinth seal radial clearance influence. A generic labyrinth seal of a turbine aircraft engine was modeled. The target is to... |
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| SubjectTerms | Air flow Aircraft Aircraft engines aircraft turbine engine Analysis Boundary conditions Clearances Computer simulation Computer-generated environments Energy Equipment and supplies Fluid dynamics Geometry Influence labyrinth seal Labyrinth seals Materials engineering Mechanical properties radial clearance Seals (Closures) Sensitivity analysis Simulation Turbine engines Turbines Velocity |
| Title | Aircraft Turbine Engine Labyrinth Seal CFD Sensitivity Analysis |
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