MOTOR AIR FLOW COOLING

In one possible embodiment, an aircraft electric motor cooling system is provided having an airflow path through a spinner which includes a first airflow path between an inner rotor and a stator, a second airflow path between an outer rotor the stator and a third airflow path along an outer surface...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: SHEPPARD, LINDSAY, ASPINWALL, HIBBS, BART
Format: Patent
Sprache:eng
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Beschreibung
Zusammenfassung:In one possible embodiment, an aircraft electric motor cooling system is provided having an airflow path through a spinner which includes a first airflow path between an inner rotor and a stator, a second airflow path between an outer rotor the stator and a third airflow path along an outer surface of the outer rotor.