CONSTRUCTION AND OPERATION OF ELECTRIC OR HYBRID AIRCRAFT

This disclosure describes at least embodiments of a power management system for a vehicle. The vehicle can include a first transducer and a second transducer supported by a housing of the vehicle. The first transducer can be powered by a first battery, and the second transducer can be powered by a s...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	Demont, Sébastien
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTINGELECTRIC POWER CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORSOR DYNAMO-ELECTRIC CONVERTERS CONTROLLING TRANSFORMERS, REACTORS OR CHOKE COILS CONVERSION OR DISTRIBUTION OF ELECTRIC POWER COSMONAUTICS ELECTRICITY EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERATION PARACHUTES PERFORMING OPERATIONS SYSTEMS FOR STORING ELECTRIC ENERGY TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	This disclosure describes at least embodiments of a power management system for a vehicle. The vehicle can include a first transducer and a second transducer supported by a housing of the vehicle. The first transducer can be powered by a first battery, and the second transducer can be powered by a second battery different from the first battery. The first transducer and the second transducer can propel the housing, and the second transducer can charge the second battery. Electronic circuitry can cause the first battery to power the first transducer while the second transducer charges the second battery.