FEM-based optimal design and testing of synchronous magnetic coupling for aerospace Starter/Generator applications
Improvements in high energy density rare-earth permanent magnets make it innovative to develop magnetic couplings for Starter/Generator applications in the light of more electric aircraft to ensure magnetically insulated contactless power transmission between decoupled shafts for safe operation. Alt...
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Format: | Article |
Language: | English |
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Elsevier
2023-05-01
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Series: | Engineering Science and Technology, an International Journal |
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Online Access: | http://www.sciencedirect.com/science/article/pii/S2215098623000800 |
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author | Sami Arslan Ires Iskender Tuğba Selcen Navruz |
author_facet | Sami Arslan Ires Iskender Tuğba Selcen Navruz |
author_sort | Sami Arslan |
collection | DOAJ |
description | Improvements in high energy density rare-earth permanent magnets make it innovative to develop magnetic couplings for Starter/Generator applications in the light of more electric aircraft to ensure magnetically insulated contactless power transmission between decoupled shafts for safe operation. Although there are essential studies on magnetic couplings in the literature, especially those for aerospace Starter/Generator structures are rarely encountered. However, methodologies considering system constraints and examining design parameters of couplings are in demand. In response to such a need, this paper proposes the novel design of highly reliable synchronous radial magnetic couplings with torque requirements of 6 and 12 N·m to isolate Starter/Generator and piston engine shafts in model aircraft. The preliminary volume is obtained analytically. Simulations are executed by optimetric approaches in Ansys Maxwell 2D. Optimisation techniques are compared in Maxwell 3D to get the final shape. The retaining sleeve of 0.5 mm is suggested. Loss of synchronisation in the event of the piston shaft failure or exceeding the maximum torque of the coupling is also examined. The torque fluctuation at load changes is 0.1%. Performance tests are conducted on the direct dynamic test bench. Absolute error margin is 37% for the Virtual Work method, 13% for 2D FEM and 6% for 3D FEM. The coupling efficiency is 93.8% at the maximum operating speed and the critical angle, and 96.9% at the minimum torque angle and the minimum operating speed. |
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format | Article |
id | doaj.art-bb9ef1cbc68a4bfdafda9c3b7fbe51da |
institution | Directory Open Access Journal |
issn | 2215-0986 |
language | English |
last_indexed | 2024-04-09T13:22:20Z |
publishDate | 2023-05-01 |
publisher | Elsevier |
record_format | Article |
series | Engineering Science and Technology, an International Journal |
spelling | doaj.art-bb9ef1cbc68a4bfdafda9c3b7fbe51da2023-05-11T04:24:06ZengElsevierEngineering Science and Technology, an International Journal2215-09862023-05-0141101403FEM-based optimal design and testing of synchronous magnetic coupling for aerospace Starter/Generator applicationsSami Arslan0Ires Iskender1Tuğba Selcen Navruz2Electrical and Electronics Engineering Department, Gazi University, Graduate School of Natural and Applied Sciences, Ankara 06500, Turkey; Corresponding author.Electrical Electronics Engineering, Çankaya University, Ankara 06790, TurkeyElectrical and Electronics Engineering, Gazi University, Ankara 06560, TurkeyImprovements in high energy density rare-earth permanent magnets make it innovative to develop magnetic couplings for Starter/Generator applications in the light of more electric aircraft to ensure magnetically insulated contactless power transmission between decoupled shafts for safe operation. Although there are essential studies on magnetic couplings in the literature, especially those for aerospace Starter/Generator structures are rarely encountered. However, methodologies considering system constraints and examining design parameters of couplings are in demand. In response to such a need, this paper proposes the novel design of highly reliable synchronous radial magnetic couplings with torque requirements of 6 and 12 N·m to isolate Starter/Generator and piston engine shafts in model aircraft. The preliminary volume is obtained analytically. Simulations are executed by optimetric approaches in Ansys Maxwell 2D. Optimisation techniques are compared in Maxwell 3D to get the final shape. The retaining sleeve of 0.5 mm is suggested. Loss of synchronisation in the event of the piston shaft failure or exceeding the maximum torque of the coupling is also examined. The torque fluctuation at load changes is 0.1%. Performance tests are conducted on the direct dynamic test bench. Absolute error margin is 37% for the Virtual Work method, 13% for 2D FEM and 6% for 3D FEM. The coupling efficiency is 93.8% at the maximum operating speed and the critical angle, and 96.9% at the minimum torque angle and the minimum operating speed.http://www.sciencedirect.com/science/article/pii/S2215098623000800Contactless power transmissionOptimisationParametric solutionRadial magnetic couplersSynchronous couplings |
spellingShingle | Sami Arslan Ires Iskender Tuğba Selcen Navruz FEM-based optimal design and testing of synchronous magnetic coupling for aerospace Starter/Generator applications Engineering Science and Technology, an International Journal Contactless power transmission Optimisation Parametric solution Radial magnetic couplers Synchronous couplings |
title | FEM-based optimal design and testing of synchronous magnetic coupling for aerospace Starter/Generator applications |
title_full | FEM-based optimal design and testing of synchronous magnetic coupling for aerospace Starter/Generator applications |
title_fullStr | FEM-based optimal design and testing of synchronous magnetic coupling for aerospace Starter/Generator applications |
title_full_unstemmed | FEM-based optimal design and testing of synchronous magnetic coupling for aerospace Starter/Generator applications |
title_short | FEM-based optimal design and testing of synchronous magnetic coupling for aerospace Starter/Generator applications |
title_sort | fem based optimal design and testing of synchronous magnetic coupling for aerospace starter generator applications |
topic | Contactless power transmission Optimisation Parametric solution Radial magnetic couplers Synchronous couplings |
url | http://www.sciencedirect.com/science/article/pii/S2215098623000800 |
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