An unmanned aerial vehicle includes a main body, a propulsion assembly including a rotary blade and a motor to rotate the rotary blade about a rotation axis. The propulsion assembly is attached to the main body and further includes a rechargeable battery to supply electric power to the propulsion assembly, a frame portion surrounding an outside of the rotary blade in a radial direction, and a power receiving coil to provide non-contact power feeding. The power receiving coil is electrically connected to the battery, has a frame shape along the frame portion, and is provided in the frame portion.
UNMANNED AERIAL VEHICLE, UNMANNED AERIAL VEHICLE SYSTEM, AND BATTERY SYSTEM
2020-02-20
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / H01F MAGNETS , Magnete / H02J CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER , Schaltungsanordnungen oder Systeme für die Abgabe oder Verteilung elektrischer Leistung |
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