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Novel coupled model for power loss prediction in a record-breaking electric aircraft motor

Robert Goraj (Siemens Electric Aircraft, Erlangen, Germany)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 27 September 2018

Issue publication date: 19 March 2020

215

Abstract

Purpose

The purpose of this paper is to devise an analytical approach to calculate conductor winding losses, considering multiple contributing aspects simultaneously. These include the geometric configuration of coil windings, frequency of the electric current and the dependency on the coil temperature, derived studying a coupled fluid–solid model considering the cooling system characteristics. The obtained results allow identifying power loss trends according to such system variables as coolant inlet temperature or overall flow rate of the motor.

Design/methodology/approach

An easy-to-use coupled analytical approach is applied, which is suitable for rapid estimations of the impact of parameter variation on the resulting conductor winding power losses that facilitates decision-making in the design process of electric aircraft engines.

Findings

In the considered cooling parameters, the overall conductor winding power losses vary approximately between 6 kW and 7.2 kW. More than 95 per cent of this loss is because of direct current losses. These losses cause the variation in maximal coil temperature ranging between 115°C and 170°C.

Practical implications

The SP260D motor is set and was currently tested in Extra 330. It recently broke two world records.

Social implications

One of the current trends in aircraft engineering is electric aircraft. Advantages of electric aircraft include improved manoeuvrability because of greater torque from electric motors, increased safety because of decreased chance of mechanical failure, less risk of explosion or fire in the event of a collision and less noise. There will be environmental and cost benefits associated with the elimination of dependency on fossil fuels and resultant emissions.

Originality/value

The use of a novel fluid–solid interaction model for predicting conductor winding power loss of the SP260D electric aircraft motor has not been done earlier. A novel alternative derivation of the widely applied Dowell’s formula (Dowell, 1966) is presented for the estimation of proximity losses in square winding conductors.

Keywords

Acknowledgements

The author is grateful to his teammates Dr Thomas Gleixner and Dr Izabela Kuder for helpful support during the writing of this paper.

Citation

Goraj, R. (2018), "Novel coupled model for power loss prediction in a record-breaking electric aircraft motor", Aircraft Engineering and Aerospace Technology, Vol. 92 No. 3, pp. 345-354. https://doi.org/10.1108/AEAT-12-2017-0278

Publisher

:

Emerald Publishing Limited

Copyright © 2018, Emerald Publishing Limited

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