Airbus Operations Sl

Cesar Bautista De La Llave

Elena Arévalo Rodríguez

Jose Sanchez Gomez

Angel Postigo Rodriguez

Bernardo Lopez Romano

Cristina Ortega Juaristi

José Ignacio Lopez-Reina Torrijos

The present invention relates to an aircraft load frame () made of a composite material, characterized in that it comprises two side elements () and a base element (), the side elements () being joined at the inner part of the frame () by means of the base element () and each of the side elements () comprising a leg () joining the frame () to the aircraft fuselage skin, a web () and a lower flange () joining the web () and the base element ().

Aircraft load frame made of a composite material

The invention relates to an aircraft with a protection shield for the rear composite material, fuselage) for conducting tail impact tests, in addition to a tail absorber, the shield () being formed by a plurality of pieces () joined to supports () fixed to the rear fuselage () behind the tail absorber (), said pieces () having a laminar structure with an outer steel sheet (), an inner composite sheet () and an intermediate high resistance silicon sheet ().

Aircraft with a rear fuselage protection shield

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Madrid, Spain

Cesar Bautista De La Llave