STRUCTURAL ELEMENT FOR AN AIRCRAFT FUSELAGE THAT PREVENTS LATERAL-TORSIONAL BUCKLING

The invention relates to a structural element for an aircraft fuselage, generally shaped in the form of a longitudinally elongate section. The element comprises two wings, each wing including: a portion that extends uninterrupted along the entire length of the section, and legs spaced apart from one...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GIUSEPPIN LAURENT, MUELLER MARKUS, ALBY SEBASTIEN
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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