HYBRID PROPULSION SYSTEM AND METHOD FOR CONTROLLING SUCH A SYSTEM

A hybrid propulsion system for a multi-rotor rotary-wing aircraft, including: an internal combustion engine, an electric machine coupled to the internal combustion engine, a rectifier connected to the electric machine, a converter, an electric network connecting the rectifier to the converter, elect...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KLONOWSKI, Thomas, VIVE, Lois Pierre Denis, SERGHINE, Camel
Format:	Patent
Sprache:	eng
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
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