The invention relates to a composite panel assembly comprising a first panel (1) with a first skin (3), a second skin (5), a core (7), an assembly flange (17 ; a second panel (2) with a first skin (4), a second skin (6), a core (8), an assembly flange (18), at least a fastening device (22, 30, 31) adapted to fasten the assembly flange (17) of the first panel to the assembly flange (18) of the second panel, characterized in that the core (7, 8) of one of the first panel (1) or the second panel (2) comprises reinforcing pins (9, 10) and a high-density portion (29, 28) placed along the assembly flange.
COMPOSITE PANELS ASSEMBLY, FURNITURE COMPRISING SUCH ASSEMBLY AND AIRCRAFT COMPRISING SUCH ASSEMBLY
VERBUNDPLATTENANORDNUNG, MÖBEL MIT SOLCH EINER ANORDNUNG UND FLUGZEUG MIT SOLCH EINER ANORDNUNG
ENSEMBLE DE PANNEAUX COMPOSITES, MEUBLE COMPRENANT UN TEL ENSEMBLE ET AÉRONEF COMPRENANT UN TEL ENSEMBLE
2020-12-09
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / 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 |
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