Plattenstruktur und zugehöriges Verfahren

Details

Veröffentlichungs-Nr.

EP3009344

Aktenzeichen

EP14189185

Anmeldetag

16. Oktober 2014

Veröffentlichung

29. Mai 2019

Erteilung

29. Mai 2019

Rechtsraum

EP

IPC

B64C1/12B64C1/10B64C3/22

Abstract

The invention relates to a panel structure (1) for a vehicle, and especially for an aircraft (A) or spacecraft, comprising: an area member (2), especially a skin member, that defines an areal expanse with a first surface (3) and an opposite second surface (4) and having a thickness (5) between the first and second surfaces (3, 4); and a plurality of elongate stiffener members (6) which are attached to the area member (2) and extend over at least one of the first and second surfaces (3, 4); wherein at least one of the stiffener members (6) is bifurcated at a bifurcation point (P) into two or more branch stiffener members (6'). The invention also provides a method of producing such a panel structure (1).

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete