B - Operations – Transporting – 64 – C
Patent
B - Operations, Transporting
64
C
B64C 1/18 (2006.01) B64C 1/06 (2006.01)
Patent
CA 2690590
The present invention provides a structural component (200) for an aircraft or spacecraft with an outer skin (100). The structural component comprises a rib element (202) for stiffening the outer skin and a cross member element (204). Here the rib element is bent in the shape of an arc to correspond to an inner contour of the outer skin (100). The cross member element connects two arc sections (206, 206') of the rib element transversely to each other. The cross member element has a higher stiffness than the rib element. From another point of view the invention provides an aircraft with such a structural component.
La présente invention concerne un élément structurel pour un avion ou un aéronef muni d'un revêtement externe. Le composant structurel comprend un élément de nervure pour rigidifier le revêtement externe et un élément de traverse. Ici, l'élément de nervure est courbé en forme d'arc pour correspondre au contour interne du revêtement externe. L'élément de traverse relie deux sections d'arc de l'élément de nervure transversalement l'une à l'autre. L'élément de traverse présente une résistance supérieure à celle de l'élément de nervure. Selon un autre aspect, l'invention porte sur un avion muni d'un tel composant structurel.
Dolzinski Wolf-Dietrich
Kohlgrueber Dieter
Luetzenburger Marius
Roming Thorsten
Schroeer Thorsten
Airbus Operations Gmbh
Dlr - Deutsches Zentrum Fur Luft- Und Raumfahrt E.v.
Oyen Wiggs Green & Mutala Llp
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