PROPULSION SYSTEM FOR AN AIRCRAFT

A propulsion system for an includes a combustion engine, a propulsor, and an electric machine 300 configured to either be driven by the combustion engine or configured to drive the propulsor. The electric machine 300 defines an axis 302. The electric machine 300 includes a rotor 304 extending along...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Hauptverfasser:	VONDRELL, Randy, GANSLER, Michael Thomas, CRABTREE, Glenn David, WEEBER, Konrad Roman
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS DYNAMO-ELECTRIC MACHINES ELECTRICITY ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	A propulsion system for an includes a combustion engine, a propulsor, and an electric machine 300 configured to either be driven by the combustion engine or configured to drive the propulsor. The electric machine 300 defines an axis 302. The electric machine 300 includes a rotor 304 extending along and rotatable about the axis 302, and a stator 306 having a plurality of winding assemblies 318, the plurality of winding assemblies 318 spaced along the axis 302 of the electric machine 300, each winding assembly 318 operable with the rotor 304 independently of an adjacent winding assembly 318 during operation of the electric machine 300.