Flugzeugmonumentverbundkonstruktion unter Verwendung von Unidirektionalem Gespreiztem Kohlenstoffflachzuggewebe

Details

Veröffentlichungs-Nr.

EP3733514

Aktenzeichen

EP19212633

Anmeldetag

29. November 2019

Veröffentlichung

6. März 2024

Erteilung

6. März 2024

Rechtsraum

EP

IPC

B64D11/04// B64D11/00

Abstract

A construction of commercial aircraft interior monument employs carbon fiber Spread Tow Fabric (STF) as face sheets (skins) surrounding a paper honeycomb or foam core to produce flat pressed panels of high strength and desirable thickness. Each individual panel is joined with other panels to construct a modular rectangular cubic able to be modularly coupled with additional structures to form the aircraft monument. The use individual STF panels offer a desirable weight and footprint of a fabricated structure as a whole. Also usable in conjunction with other composite reinforcements, the individual STF panels produce hybrid lay-ups for both pressed flat panel and tooled composite moldings offering a high strength to weight ratio of the overall monument.

Anmelder

Firma

B/E Aerospace, Inc.

Land

🇺🇸 USA

Fachgebiete