The present invention refers to a tail cone of an aircraft, more specifically to a tail cone made of composite materials comprising: - an internal skin (3), - an external skin (4) which surrounds the internal skin (3), - longitudinal structural members (1) located on the inner face of the internal skin (3) in the longitudinal direction of the tail cone, and - transversal structural members (2) located between the external skin (4) and the internal skin (3) in the transverse direction of the tail cone.
Tail cone of an aircraft
Heckkonus eines Flugzeugs
Cône de queue d'un aéronef
2017-12-20
Patent
Electronic Resource
English
Tail cone with speed reduction assembly and aircraft with tail cone
European Patent Office | 2022
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