Aircraft structure with integrated reinforcing elements

The invention provides an integrated aircraft structure (10), such as a fuselage, with reinforcing elements (51, 53) in areas of the structure that need them because they have openings or are subjected to high loads. The structure (10) comprises a skin (13), a plurality of stringers (15) and a plura...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	BALIGAND, ESTELLE, ARÉVALO RODRIGUEZ, ELENA
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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