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US 2025/0158458 A1Published application
Stator system for an axial flux machine for an aircraft, as well as drive train and aircraft equipped therewith
AssigneeAirbus SAS
InventorsFlorian KAPAUN, Marek GALEK
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Abstract
A stator system for an axial flux machine for an aircraft, the stator system comprising a plurality of inverters and a stator including a plurality of disks wherein each disk comprises at least one dielectric substrate and at least a one conductive trace included in at least one conductive layer defined by the dielectric substrate, the at least one conductive trace forming at least a part of a winding of a at least one phase of the stator, wherein each disk is associated and connected to its own inverter.
Claims16
A stator system for an axial flux machine for an aircraft, the stator system comprising:
- a plurality of inverters;
- and
- a stator including a plurality of disks,
- wherein each disk comprises at least one dielectric substrate and at least a one conductive trace included in at least one conductive layer defined by the at least one dielectric substrate, the at least one conductive trace forming at least a part of a winding of at least one phase of the stator, wherein each disk is associated and connected to a single inverter, and each inverter connected to a single disk.
1 more element
Dependencies are inferred from the claim text.