A heat exchanger system for an aircraft comprises nacelle having an inlet and an outlet, a nacelle heat exchanger within the nacelle, and a fan system within the nacelle. Air flows into the nacelle through the inlet and out of the nacelle through the outlet. The nacelle heat exchanger is configured to transfer heat away from a coolant using the air in an airflow to the nacelle heat exchanger. The fan system is configured to increase the airflow to the nacelle heat exchanger.
NACELLE AIR HEAT EXCHANGER INTEGRATION FOR A HYDROGEN FUELED FUEL CELL POWERED AIRCRAFT
INTEGRATION EINES GONDELLUFTWÄRMETAUSCHERS FÜR EIN MIT WASSERSTOFFBETRIEBENER BRENNSTOFFZELLE ANGETRIEBENES FLUGZEUG
INTÉGRATION D'ÉCHANGEUR DE CHALEUR D'AIR DE NACELLE POUR UN AÉRONEF ALIMENTÉ PAR PILE À COMBUSTIBLE À HYDROGÈNE
2025-02-19
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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