Development of an aircraft wheel actuator for green taxiing

Galea, Michael; Pickering, Stephen J.; Tighe, Chris; XU, ZEYUAN; Hamiti, Tahar; Gerada, Chris

Abstract

In this paper, the design and construction aspects of a wheel actuator to be used for aircraft taxiing on the ground and which will be located in the main landing gear are addressed. The main challenges with the application are the high torque density and fault tolerance requirements. This paper will look at all the different design aspects of the traction motor required for the actuator, including the electro-magnetic design and analysis, thermal management and mechanical analysis. The paper will then conclude with a brief overview of the construction aspects of the motor of the wheel actuator and experimental validation.

Citation

Galea, M., Pickering, S. J., Tighe, C., XU, Z., Hamiti, T., & Gerada, C. (2014, September). Development of an aircraft wheel actuator for green taxiing. Presented at XXI International Conference on Electrical Machines (ICEM '2014), Berlin, Germany

• Presentation Conference Type: Edited Proceedings
• Conference Name: XXI International Conference on Electrical Machines (ICEM '2014)
• Start Date: Sep 2, 2014
• End Date: Sep 5, 2014
• Acceptance Date: Sep 2, 2014
• Online Publication Date: Nov 20, 2014
• Publication Date: Nov 20, 2014
• Deposit Date: Aug 24, 2018
• Publisher: Institute of Electrical and Electronics Engineers
• Pages: 2492-2498
• DOI: https://doi.org/10.1109/ICELMACH.2014.6960537
• Keywords: Torque , Windings , Rotors , Load modeling , Traction motors , Iron , Aircraft
• Public URL: https://nottingham-repository.worktribe.com/output/1102572
• Publisher URL: https://ieeexplore.ieee.org/document/6960537
• Related Public URLs: http://www.scopus.com/inward/record.url?eid=2-s2.0-84916209342&partnerID=40&md5=75ed4865f046eba926d1a8a0e65032db