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
2022-03-02
Patent
Electronic Resource
English