Stator Slot Design Guidelines for Concentrated Windings with Direct Liquid Cooling Channels for Electrified Aviation

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Autoren

  • Norman Blanken
  • Ralf Johannes Keuter
  • B. Ponick
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Details

OriginalspracheEnglisch
Titel des Sammelwerks2024 International Conference on Electrical Machines, ICEM 2024
ISBN (elektronisch)9798350370607
PublikationsstatusVeröffentlicht - 1 Sept. 2024

Abstract

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

Zitieren

Stator Slot Design Guidelines for Concentrated Windings with Direct Liquid Cooling Channels for Electrified Aviation. / Blanken, Norman; Keuter, Ralf Johannes; Ponick, B.
2024 International Conference on Electrical Machines, ICEM 2024. 2024.

Publikation: Beitrag in Buch/Bericht/Sammelwerk/KonferenzbandAufsatz in KonferenzbandForschungPeer-Review

Blanken, N, Keuter, RJ & Ponick, B 2024, Stator Slot Design Guidelines for Concentrated Windings with Direct Liquid Cooling Channels for Electrified Aviation. in 2024 International Conference on Electrical Machines, ICEM 2024. https://doi.org/10.1109/ICEM60801.2024.10700410
Blanken, N., Keuter, R. J., & Ponick, B. (2024). Stator Slot Design Guidelines for Concentrated Windings with Direct Liquid Cooling Channels for Electrified Aviation. In 2024 International Conference on Electrical Machines, ICEM 2024 https://doi.org/10.1109/ICEM60801.2024.10700410
Blanken N, Keuter RJ, Ponick B. Stator Slot Design Guidelines for Concentrated Windings with Direct Liquid Cooling Channels for Electrified Aviation. in 2024 International Conference on Electrical Machines, ICEM 2024. 2024 doi: 10.1109/ICEM60801.2024.10700410
Blanken, Norman ; Keuter, Ralf Johannes ; Ponick, B. / Stator Slot Design Guidelines for Concentrated Windings with Direct Liquid Cooling Channels for Electrified Aviation. 2024 International Conference on Electrical Machines, ICEM 2024. 2024.
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title = "Stator Slot Design Guidelines for Concentrated Windings with Direct Liquid Cooling Channels for Electrified Aviation",
abstract = "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",
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AU - Blanken, Norman

AU - Keuter, Ralf Johannes

AU - Ponick, B.

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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

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