Tail cone of an aircraft
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 s...
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| Format: | Patent |
| Sprache: | eng ; fre ; ger |
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| Zusammenfassung: | 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. |
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