The present application relates to a fuselage assembly for an aircraft. The fuselage assembly has a stringer extending longitudinally along the fuselage. The stringer defines a fluid channel. The fluid channel is configured to form at least part of a distribution duct of a cabin air distribution system. The present application also relates to a cabin air distribution system, a frame for an aircraft fuselage, and an aircraft. The frame can also comprise a fluid duct and a skin mounting section configured to mount to a skin of the aircraft fuselage, wherein the fluid duct is spaced from the skin mounting section.
FUSELAGE ASSEMBLY FOR AN AIRCRAFT
RUMPFANORDNUNG FÜR EIN FLUGZEUG
ENSEMBLE FUSELAGE POUR AÉRONEF
2024-05-01
Patent
Electronic Resource
English
Assembly method for assembling aircraft fuselage panel, fuselage part and aircraft
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