The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System
This paper concerns fatigue testing of the rotor of the propulsion system for the MOSUPS – an unmanned aircraft designed in a joint wing configuration, and equipped with a ducted propeller. The work presents the analysis of the stresses and deformations of the rotor structure as well as the form of...
| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Sciendo
2016-06-01
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| Series: | Fatigue of Aircraft Structures |
| Subjects: | |
| Online Access: | https://doi.org/10.1515/fas-2016-0008 |
| _version_ | 1797967535715385344 |
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| author | Głowacki Dominik Rodzewicz Mirosław |
| author_facet | Głowacki Dominik Rodzewicz Mirosław |
| author_sort | Głowacki Dominik |
| collection | DOAJ |
| description | This paper concerns fatigue testing of the rotor of the propulsion system for the MOSUPS – an unmanned aircraft designed in a joint wing configuration, and equipped with a ducted propeller. The work presents the analysis of the stresses and deformations of the rotor structure as well as the form of the loading cycle. The aim of the paper is to introduce the concept of a simplified method of fatigue testing of multi-blade rotors. With the sophisticated geometry of the rotor in mind – the authors applied the FEM tools and implemented the ANSYS and nCode programs. The prototype of the fatigue stand built by the authors is also presented in the paper. |
| first_indexed | 2024-04-11T02:32:43Z |
| format | Article |
| id | doaj.art-c539ef01802e4723a3cd50f0829c0143 |
| institution | Directory Open Access Journal |
| issn | 2300-7591 |
| language | English |
| last_indexed | 2024-04-11T02:32:43Z |
| publishDate | 2016-06-01 |
| publisher | Sciendo |
| record_format | Article |
| series | Fatigue of Aircraft Structures |
| spelling | doaj.art-c539ef01802e4723a3cd50f0829c01432023-01-02T21:02:48ZengSciendoFatigue of Aircraft Structures2300-75912016-06-01201689710310.1515/fas-2016-0008fas-2016-0008The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion SystemGłowacki Dominik0Rodzewicz Mirosław1Warsaw University of Technology, Institute of Aeronautics and Applied Mechanics, Nowowiejska 24, 00-665WarsawWarsaw University of Technology, Institute of Aeronautics and Applied Mechanics, Nowowiejska 24, 00-665WarsawThis paper concerns fatigue testing of the rotor of the propulsion system for the MOSUPS – an unmanned aircraft designed in a joint wing configuration, and equipped with a ducted propeller. The work presents the analysis of the stresses and deformations of the rotor structure as well as the form of the loading cycle. The aim of the paper is to introduce the concept of a simplified method of fatigue testing of multi-blade rotors. With the sophisticated geometry of the rotor in mind – the authors applied the FEM tools and implemented the ANSYS and nCode programs. The prototype of the fatigue stand built by the authors is also presented in the paper.https://doi.org/10.1515/fas-2016-0008uavpropulsion systemstress analysisfatigue tests |
| spellingShingle | Głowacki Dominik Rodzewicz Mirosław The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System Fatigue of Aircraft Structures uav propulsion system stress analysis fatigue tests |
| title | The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System |
| title_full | The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System |
| title_fullStr | The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System |
| title_full_unstemmed | The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System |
| title_short | The Elaboration of the Method of Fatigue Testing of the Rotor of the Mosups Plane Propulsion System |
| title_sort | elaboration of the method of fatigue testing of the rotor of the mosups plane propulsion system |
| topic | uav propulsion system stress analysis fatigue tests |
| url | https://doi.org/10.1515/fas-2016-0008 |
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