A tank for an aircraft, the tank comprising two pressure bulkheads which are connected to each other by a tank wall which is at least partially formed by a portion of a skin of the aircraft's fuselage. The tank further comprises at least one anti-sloshing wall at least partially enclosing one or several openings and at least partially formed by a belonging frame stabilizing the skin. Also a fuselage with such tank, and an aircraft with such fuselage.
FUEL TANK FOR AN AIRCRAFT, FUSELAGE OF AN AIRCRAFT, AND AIRCRAFT
2024-10-31
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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