VERTICAL TAKEOFF AND LANDING AIRCRAFT USING HYBRID ELECTRIC PROPULSION SYSTEM AND CONTROL METHOD THEREFOR

VERTICAL TAKEOFF AND LANDING AIRCRAFT USING HYBRID ELECTRIC PROPULSION SYSTEM AND CONTROL METHOD THEREFOR

A vertical takeoff and landing aircraft using a hybrid electric propulsion system and a control method therefor according to an embodiment of the present invention can: perform control such that, during vertical takeoff and landing of an aircraft (1), a generator (20), a power management device (4),...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: MOON, Chang Mo, MOON, Ji Ho
Format: Patent
Sprache:eng ; fre ; ger
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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Beschreibung
Zusammenfassung:A vertical takeoff and landing aircraft using a hybrid electric propulsion system and a control method therefor according to an embodiment of the present invention can: perform control such that, during vertical takeoff and landing of an aircraft (1), a generator (20), a power management device (4), and a battery management system (60) simultaneously provide power to a motor (80); and perform control such that, during a cruise flight or transition flight of the aircraft (1), the thrust of a second propeller (82) is increased and a battery (62) of the battery management system (60) is charged with redundant power generated by the generator (20).