Structural component with rib and cross member element

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:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung: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 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 strength than the rib element. From another point of view the invention provides an aircraft with such a structural component.