In a fuel cell system intended for a pressure-independent operation, in which at least one fuel cell having an open cathode is provided, a first fluid chamber adjoins an inflow cross section and a second fluid chamber adjoins an outflow cross section. In the fluid chambers can be set an overpressure which is adapted to the operation of the at least one fuel cell.
FUEL CELL SYSTEM FOR AN AIRCRAFT
2020-02-20
Patent
Electronic Resource
English