A fuselage assembly is provided. The fuselage assembly includes a first barrel section (210) including a body that extends from a first end (211) to a second end (213) and a second barrel section (220) coupled to said first barrel section (210). The second barrel section (220) includes a body that extends from a first end (221) to a second end (223), and the second end (213) of the first barrel section (210) is coupled to the second end (223) of the second barrel section (220). At least one member (130, 132) induces a compressive force to at least one of the first barrel section (210) and the second barrel section (220).
Method of assembling a fuselage and aircraft fuselage
Verfahren zur Montage eines Rumpfs und Flugzeugrumpf
Procédé d'assemblage d'un fuselage et fuselage d'aéronef
2018-04-11
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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