The invention discloses an aircraft fuel system. The fuel system used for the aircraft includes a fuel storage system, a heat exchanger, a fuel cooling loop and a pump, wherein the fuel storage system includes a fuel tank, the fuel cooling loop is configured to convey fuel from the storage system through the heat exchanger and returns to the storage system, and the pump is configured to pump the fuel through the cooling loop. The aircraft fuel system that the invention relates to is used for improving aircraft safety and reducing aircraft vulnerability caused by flammability of the fuel tank.
Aircraft fuel system
2015-06-03
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Double-walled tube for aircraft fuel system, aircraft fuel system and aircraft
European Patent Office | 2025
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