ELECTRIC PROPULSION SYSTEM

An electric propulsion system includes a first stator segment including first teeth and first coils wound around the first teeth and a second stator segment including second teeth and second coils wound around the second teeth. A gap exists in an azimuthal direction between the first stator segment...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	Cottrell, Daniel B, Lovelace, Edward C, Li, Kang, Ouyang, Wen
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DYNAMO-ELECTRIC MACHINES ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION PARACHUTES PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	An electric propulsion system includes a first stator segment including first teeth and first coils wound around the first teeth and a second stator segment including second teeth and second coils wound around the second teeth. A gap exists in an azimuthal direction between the first stator segment and the second stator segment. The electric propulsion system also includes a rotor frame and rotor magnets. The rotor magnets are attached to the rotor frame and configured to rotate the rotor frame in the azimuthal direction in response to the first coils or the second coils being provided current. The electric propulsion system also includes a propeller including a first blade attached to the rotor frame at a first distal end of the first blade and a second blade attached to the rotor frame at a second distal end of the second blade.