Flugzeugstruktur mit integrierten Verstärkungselementen

Details

Veröffentlichungs-Nr.

EP2749491

Aktenzeichen

EP12382547

Anmeldetag

28. Dezember 2012

Veröffentlichung

23. Dezember 2015

Erteilung

23. Dezember 2015

Rechtsraum

EP

IPC

B64C1/12B64C1/06// B64C1/00

Abstract

The invention provides an integrated aircraft structure (10), such as a fuselage, with reinforcing elements (51, 53) in areas of the structure that need them because they have openings or are subjected to high loads. The structure (10) comprises a skin (13), a plurality of stringers (15) and a plurality of frames (17) with mouseholes for the passage of stringers (15) at their crossing zones. The reinforcing elements (51, 53) are configured with a suitable shape to be superimposed to the stringers (15) in said areas. The invention also provides manufacturing processes of said integrated aircraft structure (10).

Anmelder

Firma

Airbus Operations, S.L.

Land

🇪🇸 Spanien

Fachgebiete