Statorkörper und den Statorkörper Tragende Stützstruktur
Anmelder: Archer Aviation Inc., Lilium GmbH 🇺🇸
Details
- Veröffentlichungs-Nr.
- EP4718690
- Anmeldetag
- 27. Mai 2024
- Veröffentlichung
- 1. April 2026
- Rechtsraum
- EP
- IPC
- H02K9/22, H02K1/14, H02K1/18
Abstract
The present invention relates to a stator body (10) for a rotating electric machine, comprising: a ring-shaped outer stator yoke (11); a plurality of stator teeth (13) and a plurality of coil pockets (14). According to the invention, a plurality of receptive cavities (12) is recessed into the stator yoke (11) for receiving a plurality of heat sink means (20) for heat dissipation on an outside of the stator body (10); wherein the heat sink means (20) comprise at least one heat flux material having a higher thermal conductivity than a magnetic flux material of at least the stator yoke (11) of the stator body (10).
Anmelder
- Firmen
- Archer Aviation Inc.
Lilium GmbH - Land
- 🇺🇸 USA
US-amerikanisches Luftfahrtunternehmen aus Kalifornien, das elektrisch angetriebene Senkrechtstarter (eVTOL) für den urbanen Lufttransport entwickelt.
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