Aircraft panel 1 for an interior of an aircraft, wherein the aircraft panel 1 has a sandwich structure 2, wherein the sandwich structure 2 comprises a core section 4 and a covering section 3 as sandwich layers, wherein the covering section 3 comprises a prepreg layer 6 and wherein the aircraft panel 1 comprises at least one switching element 8 for activating at least one electrical device of the aircraft, wherein at least one switching element 8 is fixed in the covering section 3 by the prepreg layer 6.
AIRCRAFT PANEL FOR AN INTERIOR OF AN AIRCRAFT AND METHOD FOR MAKING THE AIRCRAFT PANEL
PANNEAU D~AERONEF POUR UN INTERIEUR D~UN AERONEF ET METHODE DE FABRICATION DU PANNEAU D~AERONEF
2015-08-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B32B LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM , Schichtkörper, d.h. aus Ebenen oder gewölbten Schichten, z.B. mit zell- oder wabenförmiger Form, aufgebaute Erzeugnisse / C08J Verarbeitung , WORKING-UP / F16S CONSTRUCTIONAL ELEMENTS IN GENERAL , Konstruktionselemente allgemein |
AIRCRAFT PANEL FOR AN INTERIOR OF AN AIRCRAFT AND METHOD FOR MAKING THE AIRCRAFT PANEL
European Patent Office | 2015
|AIRCRAFT INTERIOR TRIM PANEL AND AIRCRAFT FITTED WITH SUCH PANELS
European Patent Office | 2019
|