A cryogenic fuel system (32) for an aircraft (20) includes a fuel tank assembly (34) that is configured to store a cryogenic fuel in a liquid phase during aircraft operation, and a cooling system (36) that is associated with the fuel tank assembly (34). The cooling system (36) is configured to maintain the fuel tank assembly (34) within a predefined temperature range during non-flight operation.
COOLING OF AIRCRAFT CRYOGENIC FUEL TANK ASSEMBLY
KÜHLUNG EINER KRYOGENEN KRAFTSTOFFTANKANORDNUNG EINES FLUGZEUGS
REFROIDISSEMENT D'UN ENSEMBLE RÉSERVOIR DE CARBURANT CRYOGÉNIQUE D'AÉRONEF
16.10.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
Cryogenic tank and aircraft comprising such cryogenic tank
Europäisches Patentamt | 2024
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