HYBRID PROPULSION SYSTEM AND METHOD FOR CONTROLLING SUCH A SYSTEM

The invention relates to a hybrid propulsion system (100) for a multi-rotor rotary-wing aircraft, comprising: an internal combustion engine (12), an electric machine (14) coupled to the internal combustion engine, a rectifier (16) connected to the electric machine, conversion means (18a, 18b, 18c, 1...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	VIVE, LOIS PIERRE DENIS, SERGHINE, CAMEL, KLONOWSKI, THOMAS
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!