Print Email Facebook Twitter The implications of aerospace requirements on the design-space of a permanent magnet starter/generator system Title The implications of aerospace requirements on the design-space of a permanent magnet starter/generator system Author Brink, E. Gerber, M. De Boer, A. Van der Geest, M. Zeilstra, D. Faculty Electrical Engineering, Mathematics and Computer Science Department Electrical Sustainable Energy Date 2015-04-13 Abstract Starter/generator units based on PM machines are generally not considered due to their inherent safety risks. This technology can, however, prove advantageous for aerospace applications where mass, volume, efficiency and low maintenance costs play a significant role. A safety analysis is performed in order to identify the safety and mitigation measures required to realise such a system which conforms to aerospace requirements. These measures define the design-space and boundary conditions within which a design may be realised. It is found that not all the measures are unique to PM based SGUs and that their degree of influence on the mass and volume is highly dependent on the starting and generating specifications. To reference this document use: http://resolver.tudelft.nl/uuid:73005fd1-6612-46f4-a511-87b5b93136cf Source Proceedings of the 3rd CEAS Specialist Conference on Guidance, Navigation and Control, Toulouse, France, 13-15 April 2015 Part of collection Institutional Repository Document type conference paper Rights © 2015 The Author(s)This work is licensed under the Creative Commons Attribution International License (CC BY) Files PDF 329847.pdf 682.7 KB Close viewer /islandora/object/uuid:73005fd1-6612-46f4-a511-87b5b93136cf/datastream/OBJ/view