A cryogenic fuel system for an aircraft, the cryogenic fuel system includes a fuel tank assembly that is configured to store a cryogenic fuel in a liquid phase during aircraft operation, and a cooling system that is associated with the fuel tank assembly. The cooling system is configured to maintain the fuel tank assembly within a predefined temperature range during non-flight operation.
COOLING OF AIRCRAFT CRYOGENIC FUEL TANK ASSEMBLY
17.10.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Cryogenic tank and aircraft comprising such cryogenic tank
Europäisches Patentamt | 2024
|