An aircraft includes a chamber (1), a processor, a memory, and a compressor system (12b) in fluid communication with the chamber. The compressor system (12b) configured to selectively pressurize the chamber (1). The chamber supports a fuel cell (26), a motor, and/ or electrical components that electrically communicate with the fuel cell (26) and the motor to power the aircraft. The memory includes instructions stored thereon, which when executed by the processor, cause the aircraft to receive an altitude value of the aircraft, and selectively pressurize the chamber using the compressor system based on the received altitude value to reduce corona discharge in the chamber.
CORONA DISCHARGE MANAGEMENT FOR HYDROGEN FUEL CELL-POWERED AIRCRAFT
KORONAENTLADUNGSVERWALTUNG FÜR MIT WASSERSTOFFBRENNSTOFFZELLEN BETRIEBENES FLUGZEUG
GESTION DE DÉCHARGE PAR EFFET COURONNE POUR AÉRONEF ALIMENTÉ PAR PILE À COMBUSTIBLE À HYDROGÈNE
2024-07-03
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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