L. Papini
Design and testing of electromechanical actuator for aerospace applications
Papini, L.; Connor, P.; Patel, C.; Empringham, L.; Gerada, C.; Wheeler, P.
Authors
PETER CONNOR Peter.Connor@nottingham.ac.uk
Senior Application Engineers in Industrialisation of Electrical Machines and Drives
C. Patel
LEE EMPRINGHAM LEE.EMPRINGHAM@NOTTINGHAM.AC.UK
Professor of Power Conversion Technologies
CHRISTOPHER GERADA CHRIS.GERADA@NOTTINGHAM.AC.UK
Professor of Electrical Machines
PATRICK WHEELER pat.wheeler@nottingham.ac.uk
Professor of Power Electronic Systems
Abstract
Electromechanical actuators are gaining interest in the aerospace industry within the More Electrical Aircraft (MEA) architecture. The end-goal of fully electric aircraft includes Electromechanical actuation for flight control systems. The design and testing of a flight control system for helicopter swash-plate is presented in this work. The mechanical system is driven by electrical machines and controlled by dedicated power electronics, both of which fit challenging space requirements and environmental conditions. The predicted performances are validated by experimental testing of prototypes.
Citation
Papini, L., Connor, P., Patel, C., Empringham, L., Gerada, C., & Wheeler, P. (2018). Design and testing of electromechanical actuator for aerospace applications. In 2018 25th International Workshop on Electric Drives: Optimization in Control of Electric Drives (IWED2018) - Proceedings (1-6). https://doi.org/10.1109/IWED.2018.8321392
Conference Name | 2018 25th International Workshop on Electric Drives: Optimization in Control of Electric Drives (IWED) |
---|---|
Conference Location | Moscow, Russia |
Start Date | Jan 31, 2018 |
End Date | Feb 2, 2018 |
Acceptance Date | Dec 6, 2017 |
Online Publication Date | Mar 22, 2018 |
Publication Date | 2018 |
Deposit Date | Aug 16, 2018 |
Publicly Available Date | Mar 29, 2024 |
Publisher | Institute of Electrical and Electronics Engineers |
Pages | 1-6 |
Book Title | 2018 25th International Workshop on Electric Drives: Optimization in Control of Electric Drives (IWED2018) - Proceedings |
Chapter Number | 42 |
ISBN | 978-1-5386-1201-9 |
DOI | https://doi.org/10.1109/IWED.2018.8321392 |
Keywords | More electric aircraft; Fault tolerant; Permanent magnet machine; Electro-mechanical actuator |
Public URL | https://nottingham-repository.worktribe.com/output/1036053 |
Publisher URL | https://ieeexplore.ieee.org/document/8321392/ |
Additional Information | © 2018 IEEE. Personal use of this material is permitted. Permission from IEEE must be obtained for all other uses, in any current or future media, including reprinting/republishing this material for advertising or promotional purposes, creating new collective works, for resale or redistribution to servers or lists, or reuse of any copyrighted component of this work in other works. |
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