The present disclosure pertains to an unmanned aerial vehicle system. Some exemplary implementations may include: a mounting frame (110) onto which at least a payload (30) is affixed; a plurality of fuel cell stacks (50) operable in a predefined configuration, each of the plurality of stacks (50) being in a separate package; one or more tanks (60) configured to supply hydrogen tot the plurality of stacks; a propulsion system (70, 80) configured to receive an out put power generated from the plurality of stacks (50); and a power controller (40) configured to couple the plurality of stacks in the predefined configuration.
UAV HAVING CONFIGURABLE FUEL CELL POWER SYSTEM
UAV MIT KONFIGURIERBAREM BRENNSTOFFZELLENSTROMSYSTEM
UAV À SYSTÈME D'ALIMENTATION DE PILE À COMBUSTIBLE CONFIGURABLE
2025-01-22
Patent
Electronic Resource
English
IPC: | B64U / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / 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 |
CONFIGURABLE ELECTRIC VEHICLE CHARGING SYSTEM HAVING CENTRALLY LOCATED POWER MODULES
European Patent Office | 2024
|