In order to improve liquid hydrogen storage on aircraft (10), the invention proposes a liquid hydrogen tank (36) that is integrated into the fuselage (12) of the aircraft (10). At least one portion of the tank wall (38) is formed by specially adapted tank skin panels (42) and/or a pressure bulkhead (48). The parts forming the tank wall (38) are strengthened so as to contain a tank pressure (PLH2) of about 3 bar.
FUSELAGE SECTION OF AN AIRCRAFT, AIRCRAFT FUSELAGE, AND AIRCRAFT
FLUGZEUGRUMPFABSCHNITT, FLUGZEUGRUMPF UND FLUGZEUG
SECTION DE FUSELAGE D'UN AÉRONEF, FUSELAGE D'AÉRONEF ET AÉRONEF
2023-01-04
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Aircraft fuselage section, aircraft fuselage and aircraft
European Patent Office | 2023
|FUSELAGE SECTION OF AN AIRCRAFT, AIRCRAFT FUSELAGE, AND AIRCRAFT
European Patent Office | 2022
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