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 DE FUSELAGE POUR AÉRONEF
2024-01-24
Patent
Electronic Resource
English
Assembly method for assembling aircraft fuselage panel, fuselage part and aircraft
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