Airbus Operations Sl

Ana Reyes Moneo Peñacoba

Elena Arévalo Rodríguez

Diego Folch Cortés

Francisco José Cruz Domínguez

Pablo Timoteo Sanz Martínez

Eduardo Vinué Santolalla

César Bautista De La Llave

Esteban Martino Gonzáles

A fuselage rear end of an aircraft, comprising a structural part comprising a skin and longitudinal and transversal reinforcing members and a fairing. The structural part longitudinally spans over the whole rear end and comprises a first portion in which the transversal reinforcing members occupy the whole perimeter of the corresponding fuselage section and at least a second portion in which the transversal reinforcing members occupy only a portion of the perimeter of the corresponding fuselage section. The fairing is located below the second portion of the structural part.

Fuselage rear end of an aircraft

An aircraft fuselage part () located in a section of an aircraft () having a propulsion system () attached by upstream pylons (), the fuselage part includes a skin (); a plurality of frames () arranged perpendicularly to a longitudinal axis (); a single or internally divided upper longitudinal box () and a single or internally divided lower longitudinal box () which are configured to form with the skin () a multi-cell structure, belonging in each cell the external side to the skin () and the internal sides to the longitudinal boxes (); a plurality of lateral beams () that are interconnected with the frames () to form together with the skin () a structural unity. The fuselage components () are dimensioned so that the aircraft can withstand the effect of pre-defined failure events keeping a sufficient number of closed cells.

Impact resistant and damage tolerant aircraft fuselage

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Getafe, Spain

Ana Reyes Moneo Peñacoba