HYBRID-ELECTRIC DRIVE SYSTEM FOR MULTI-ENGINE AIRCRAFT

The invention relates to a hybrid-electric drive system (10) for multi-engine aircraft (20). The drive system comprises at least one first and second hybrid-electric drive unit (31, 32), each of which has an internal combustion engine (41, 42), a motor-generator unit (71, 72), and a transmission (51...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	NÜSSELER, Martin, RIEDIGER, Carsten
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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