Fuel cell system for an aircraft, method for operating a fuel cell system in an aircraft and aircraft with such a fuel cell system
A fuel cell system (2) comprises a first fuel cell unit (4) having a first fuel cell (8) and a second fuel cell (10), a second fuel cell unit (6) having a third fuel cell (54) and a fourth fuel cell (56), a hydrogen tank (36), an oxygen supply unit (38) and at least one air inlet (25). The first fue...
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Format: | Patent |
Sprache: | eng ; fre ; ger |
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