CONTROL DEVICE FOR ELECTRIC FLIGHT VEHICLE

A control device is configured to control an electric flight vehicle. The electric flight vehicle includes an electric drive device configured to drive and rotate a rotor blade and a cooling unit configured to cool the drive device. The control device includes a temperature acquisition unit and a co...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	SUGITA, Shun, NAKATA, Shingo, TAKEMURA, Yuichi
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 MEASURING MEASURING QUANTITY OF HEAT MEASURING TEMPERATURE PARACHUTES PERFORMING OPERATIONS PHYSICS TESTING THERMALLY-SENSITIVE ELEMENTS NOT OTHERWISE PROVIDED FOR TRANSPORTING
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Beschreibung
Zusammenfassung:	A control device is configured to control an electric flight vehicle. The electric flight vehicle includes an electric drive device configured to drive and rotate a rotor blade and a cooling unit configured to cool the drive device. The control device includes a temperature acquisition unit and a cooling determination unit. The temperature acquisition unit is configured to acquire temperature of the drive device as a device temperature. The cooling determination unit is configured to determine, according to the device temperature, whether a cooling-related abnormality has occurred as an abnormality related to cooling of the drive device by the cooling unit.