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

The present invention provides a stiffening element for stiffening a step-like substructure, in particular in an aircraft or spacecraft, having a foot section which is composed of a fiber composite material and is shaped in the form of a step such that it essentially fills the substructure. A method...

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