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).
Fuselage rear end of an aircraft
Rumpfheckende eines Flugzeugs
Extrémité arrière du fuselage d'un aéronef
2018-07-11
Patent
Electronic Resource
English
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