An aircraft fuselage is configured to receive two tanks designed to contain liquid hydrogen. The fuselage includes a first section for a cockpit, a second section for a passenger cabin and a third section (T3) distinct from the first section (T1) and from the second section (T2). The third section (T3) includes two housings each to house a tank. The two housings are arranged symmetrically with respect to a vertical plane of symmetry (P1). This arrangement of the tanks in a section distinct from the other sections allows them to be located as close as possible to the motors that they have to supply.
Aircraft Fuselage Intended to Receive Two Tanks Designed to Contain Liquid Hydrogen
2023-10-26
Patent
Electronic Resource
English
Aircraft fuselage intended to receive two storage tanks designed to contain liquid hydrogen
European Patent Office | 2023
|European Patent Office | 2023
|European Patent Office | 2023
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