An aircraft fuselage section extending along a longitudinal direction including: a fuselage structure comprising a plurality of frames; a floor connected to the fuselage structure; a cushioning element arranged on the floor, and a crash absorption assembly between the fuselage structure and the floor, wherein the crash absorption assembly includes first absorption elements and second absorption elements distributed along the longitudinal direction, wherein the first absorption elements and the second absorption elements are configured to dissipate and distribute energy; and wherein the first absorption elements are each arranged at a position corresponding to a frame of the fuselage structure and the second absorption elements are each arranged at a position between successive frames of the fuselage structure.
AIRCRAFT FUSELAGE SECTION
26.06.2025
Patent
Elektronische Ressource
Englisch
Aircraft fuselage section, aircraft fuselage and aircraft
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