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The influence of stator design on the performance of fault tolerant machines

Lookup NU author(s): Professor Barrie MecrowORCiD, Professor Alan Jack, Dr Dave Atkinson, Brian Green

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Abstract

This paper discusses the design of fault tolerant electric fuel pumps for aircraft. A range of prototype machines in the range 10-20 kW have been built and successfully tested, but fuel pump drives of 100 kW or more will be required for large aircraft. This paper discusses the problems, which arise in extending designs up to this power level, particularly focusing on the problem of induced rotor losses. Changes to the design, in particular the stator, are introduced to improve the performance of these future generations of fault tolerant machine. (12 References).

Publication metadata

Author(s): Green B; Mecrow BC; Atkinson DJ; Jack AG; Atkinson GJ

Publication type: Conference Proceedings (inc. Abstract)

Publication status: Published

Conference Name: 16th International Conference on Electrical Machines

Year of Conference: 2004

Pages: 6 pp

Publisher: Institute of Mechatronics and Information Systems

Notes: WiakS DemsM KomezaK . Lodz, Poland. 16th International Conference on Electrical Machines. Conference Proceedings. Cracow, Poland. 5-8 Sept. 2004.

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