An aircraft interior fitting component system (10) comprises an aircraft interior fitting component (12), a support element (20) attached to the aircraft interior fitting component (12) and an aircraft primary structure component (16). The support element (20) is dimensioned in such a way and is attached to the aircraft interior fitting component (12) in such a position that, in an assembled state of the aircraft interior fitting component (12) in an aircraft, it is supported on the aircraft primary structure component (16) at least when a predetermined load acts on the aircraft interior fitting component (12) along the x-axis of the aircraft in flight direction.
AIRCRAFT INTERIOR FITTING COMPONENT SYSTEM AND METHOD FOR MANUFACTURING AN AIRCRAFT INTERIOR FITTING COMPONENT SYSTEM
FLUGZEUGINNENAUSBAUKOMPONENTENSYSTEM UND VERFAHREN ZUR HERSTELLUNG EINES FLUGZEUGINNENAUSBAUKOMPONENTENSYSTEMS
SYSTÈME DE COMPOSANTS D'ÉQUIPEMENT INTÉRIEUR D'AVION ET PROCÉDÉ DE FABRICATION D'UN SYSTÈME DE COMPOSANTS D'ÉQUIPEMENT INTÉRIEUR D'AVION
2017-05-31
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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