A system comprising an Unmanned Aerial Vehicle, a first load (24), a second load (26), and a fuel cell stack (20) mounted in the Unmanned Aerial Vehicle, the fuel stack comprising: a first end plate (44), a second end plate (46), and an internal current collecting plate (48) arranged in the fuel cell stack (20) between the first end plate (44) and the second end plate (46), wherein the first load (24) is connected to the first end plate (44) and the second end plate (46), and the second load (26) is connected to the first end plate (44) and the internal current collecting plate (48); wherein the first load (24) and the second load (26) are components of the Unmanned Aerial Vehicle.
UNMANNED AERIAL VEHICLE WITH MULTI-VOLTAGE FUEL CELL
UNBEMANNTES LUFTFAHRZEUG MIT MEHRSPANNUNGSBRENNSTOFFZELLE
VÉHICULE AÉRIEN SANS PILOTE AVEC PILE À COMBUSTIBLE MULTI-TENSION
2021-05-26
Patent
Electronic Resource
English
IPC: | H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY / B60L PROPULSION OF ELECTRICALLY-PROPELLED VEHICLES , Antrieb von elektrisch angetriebenen Fahrzeugen / B63G OFFENSIVE OR DEFENSIVE ARRANGEMENTS ON VESSELS , Angriffs- oder Verteidigungsanordnungen auf Schiffen / B63H Schiffsantrieb oder Steuerung der Schiffe , MARINE PROPULSION OR STEERING / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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