In order to improve liquid hydrogen storage on an aircraft (10), the invention proposes a liquid hydrogen tank (36) integrated into a fuselage (12) of an aircraft (10). At least a portion of the tank wall (38) is formed from particularly suitable tank skin panels (42) and/or pressure bulkheads (48). The portion forming the tank wall (38) is reinforced to accommodate a tank pressure (PLH2) of about 3 bar.
为了改善飞行器(10)上的液氢储存,本发明提出了一种集成到飞行器(10)的机身(12)中的液氢罐(36)。罐壁(38)的至少一部分由特别适合的罐蒙皮面板(42)和/或压力隔板(48)形成。形成罐壁(38)的部分被加强,以容纳大约3bar的罐压力(PLH2)。
Aircraft fuselage section, aircraft fuselage and aircraft
飞行器的机身部段、飞行器机身以及飞行器
2023-01-13
Patent
Electronic Resource
Chinese
FUSELAGE SECTION OF AN AIRCRAFT, AIRCRAFT FUSELAGE, AND AIRCRAFT
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