Stiffening element for an aircraft or spacecraft, and method for its production

The invention provides a stiffening element, in particular for a shell component of an aircraft or spacecraft, which has a stiffening profile part and a foot part. The stiffening profile part is in this case composed of a lightweight metal material, and the foot part is composed of a material which...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: ROMING THORSTEN, SCHROEER THORSTEN
Format: Patent
Sprache:eng
Schlagworte:
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