An aircraft system for handling cryogenic liquid. The aircraft system comprises a vessel configured to store cryogenic liquid, a vacuum ejector operable to cause at least some of the cryogenic liquid to be moved from the vessel, and a pump downstream of the vacuum ejector, wherein the vacuum ejector is fluidically connected to the pump.
AIRCRAFT SYSTEM, AIRCRAFT FUEL SYSTEM AND METHOD
14.12.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft, aircraft fuel supply system and control method of aircraft fuel supply system
Europäisches Patentamt | 2024
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