Device for intermediate fastening between an aircraft fuselage and an aircraft undercarriage

The structure has support element (S) that is provided with the abutments. The panel elements are formed with the edge portions engaged by the abutments. A channel-shaped element is arranged for retaining the panel elements against the abutments. The channel-shaped element is engaged against the fac...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Bellet, Daniel, Gallant, Guillaume
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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