Structural component with rib and cross member element

The present invention provides a structural element (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 ad cross member element (204). Here the rib element is bent in the shape of an arc to correspond...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: DOLZINSKI WOLF-DIETRICH, KOHLGRUEBER DIETER, ROMING THORSTEN, SCHROEER THORSTEN, WESTPHAL PHILIPP, LUETZENBURGER MARIUS
Format: Patent
Sprache:chi ; eng
Schlagworte:
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