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Mild hybridisation of turboprop engine with high-power-density integrated electric drives

Cossart, Gregory; Chen, Yuzheng; Yang, Tao; Khowja, Muhammad; La Rocca, Antonino; Nasir, Usman; Chowdhury, Shajjad; Evans, Dean; Kember, Dafydd; Klonowski, Thomas; Arnaud, Yohan; Apostin, Lucie; Liger, Thierry; Cossart, Grégory; Vakil, Gaurang; Gerada, Chris; Bozhko, Serhiy; Detry, Sebastien; Diette, Christophe; Wheeler, Patrick

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Authors

Gregory Cossart

Yuzheng Chen

TAO YANG TAO.YANG@NOTTINGHAM.AC.UK
Associate Professor

ANTONINO LA ROCCA ANTONINO.LAROCCA@NOTTINGHAM.AC.UK
Professor of Applied Thermofluids and Propulsion Systems

Usman Nasir

Shajjad Chowdhury

Dean Evans

Dafydd Kember

Thomas Klonowski

Yohan Arnaud

Lucie Apostin

Thierry Liger

Grégory Cossart

SERHIY BOZHKO serhiy.bozhko@nottingham.ac.uk
Professor of Aircraft Electric Power Systems

Sebastien Detry

Christophe Diette

Profile Image

PATRICK WHEELER pat.wheeler@nottingham.ac.uk
Professor of Power Electronic Systems



Abstract

This paper shares with the aerospace community a case study of turboprop mild hybridisation using a recently developed integrated drive system in the University of Nottingham, UK, within the ACHIEVE project under EU H2020 CleanSky 2 program (project No. 737814). The developed drive system enables green taxiing of a turboprop aircraft while on the ground with its engine off, and as an electrical generator when the turboprop is in the air. The entire system is designed to be able to integrate within the power auxiliary gear box (PAGB) of a turboprop aircraft. Some of the key features of the developed system include a high-speed permanent magnet machine (up to 14,200rpm) with dual three-phase design, SiC-based high power density (11.8kW/L for the power converter, 35.3kW/L and 7.2kW/kg for the machine active parts), integrated cooling design for high-temperature operation (>130ºC ambient temperature), fault tolerance consideration with dual channel operation capabilities and sensorless control for entire operational conditions. This paper is giving an overview of the design process of the electrical machine, power converters, and its cooling of the entire drive. Numerical analysis (FEM and CFD) and some experimental results are presented to demonstrate the effectiveness and the desired performance of the developed integrated drive system.

Citation

Cossart, G., Chen, Y., Yang, T., Khowja, M., La Rocca, A., Nasir, U., …Wheeler, P. (2022). Mild hybridisation of turboprop engine with high-power-density integrated electric drives. IEEE Transactions on Transportation Electrification, 8(4), 4148-4162. https://doi.org/10.1109/TTE.2022.3160153

Journal Article Type Article
Acceptance Date Mar 7, 2022
Online Publication Date Mar 16, 2022
Publication Date 2022-12
Deposit Date Mar 21, 2022
Publicly Available Date Mar 21, 2022
Journal IEEE Transactions on Transportation Electrification
Electronic ISSN 2332-7782
Publisher Institute of Electrical and Electronics Engineers (IEEE)
Peer Reviewed Peer Reviewed
Volume 8
Issue 4
Pages 4148-4162
DOI https://doi.org/10.1109/TTE.2022.3160153
Keywords Electrical and Electronic Engineering; Energy Engineering and Power Technology; Transportation; Automotive Engineering
Public URL https://nottingham-repository.worktribe.com/output/7642230
Publisher URL https://ieeexplore.ieee.org/document/9736987

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