Rumpfheckende eines Flugzeugs

Details

Veröffentlichungs-Nr.

EP3040264

Aktenzeichen

EP14382584

Anmeldetag

30. Dezember 2014

Veröffentlichung

11. Juli 2018

Erteilung

11. Juli 2018

Rechtsraum

EP

IPC

B64C1/06B64C1/14B64C1/16B64C1/26B64C7/00// B64C5/02B64D29/04B64D29/08B64D41/00

Abstract

Fuselage rear end of an aircraft, comprising: - a structural part (1) comprising a skin and longitudinal (30) and transversal reinforcing members (31, 32), and - a fairing (5). The structural part (1) longitudinally spans over the whole rear end and comprises a first portion (2) in which the transversal reinforcing members (32) occupy the whole perimeter of the corresponding fuselage section and at least a second portion (3) in which the transversal reinforcing members (31) occupy only a portion of the perimeter of the corresponding fuselage section, the fairing (5) being located below the second portion (3) of the structural part (1).

Anmelder

Firma

Airbus Operations S.L.

Land

🇪🇸 Spanien

Fachgebiete