Details
| Original language | English |
|---|---|
| Title of host publication | Proceedings 2024 International Conference on Electrical Machines, ICEM 2024 |
| Number of pages | 7 |
| ISBN (electronic) | 9798350370607 |
| Publication status | Published - 1 Sept 2024 |
Abstract
Index Terms—electrified aircraft propulsion, direct-liquid- cooled conductor, power density
Keywords
- direct-liquid-cooled conductor, electrified aircraft propulsion, power density
ASJC Scopus subject areas
- Engineering(all)
- Mechanical Engineering
- Energy(all)
- Energy Engineering and Power Technology
- Engineering(all)
- Electrical and Electronic Engineering
- Engineering(all)
- Control and Systems Engineering
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Proceedings 2024 International Conference on Electrical Machines, ICEM 2024. 2024.
Research output: Chapter in book/report/conference proceeding › Conference contribution › Research › peer review
}
TY - GEN
T1 - Stator Slot Design Guidelines for Concentrated Windings with Direct Liquid Cooling Channels for Electrified Aviation
AU - Blanken, Norman
AU - Keuter, Ralf Johannes
AU - Ponick, B.
N1 - Publisher Copyright: © 2024 IEEE.
PY - 2024/9/1
Y1 - 2024/9/1
N2 - High power and torque densities are essential to achieve weight reduction in electric propulsion systems. For the future integration of highly utilised electric machines into aircraft propulsion, these must be evaluated also with a focus on service life and reliability. Typically, the components that limit the lifetime of electric machines are the bearings and the insulation of the stator winding. In addition, high power densities and efficiencies are essential for the realisation of electrified aviation. One method to achieve high power densities is to increase the current density. Direct liquid cooling can regulate the resulting temperature within the slot, thus managing thermal aging and increasing insulation reliability. This paper develops stator slot design guidelines for concentrated hollow conductor windings for direct liquid cooling to achieve higher power densities, highlighting the importance of current displacement and temperature-dependent resistance.Index Terms—electrified aircraft propulsion, direct-liquid- cooled conductor, power density
AB - High power and torque densities are essential to achieve weight reduction in electric propulsion systems. For the future integration of highly utilised electric machines into aircraft propulsion, these must be evaluated also with a focus on service life and reliability. Typically, the components that limit the lifetime of electric machines are the bearings and the insulation of the stator winding. In addition, high power densities and efficiencies are essential for the realisation of electrified aviation. One method to achieve high power densities is to increase the current density. Direct liquid cooling can regulate the resulting temperature within the slot, thus managing thermal aging and increasing insulation reliability. This paper develops stator slot design guidelines for concentrated hollow conductor windings for direct liquid cooling to achieve higher power densities, highlighting the importance of current displacement and temperature-dependent resistance.Index Terms—electrified aircraft propulsion, direct-liquid- cooled conductor, power density
KW - direct-liquid-cooled conductor
KW - electrified aircraft propulsion
KW - power density
UR - http://www.scopus.com/inward/record.url?scp=85207474611&partnerID=8YFLogxK
U2 - 10.1109/ICEM60801.2024.10700410
DO - 10.1109/ICEM60801.2024.10700410
M3 - Conference contribution
SN - 979-8-3503-7061-4
BT - Proceedings 2024 International Conference on Electrical Machines, ICEM 2024
ER -