AIRCRAFT PROVIDED WITH A CENTRAL FAIRING THAT ADJUSTS THE PRESSURE OVER THE WING STRUCTURE BY LOCAL GEOMETRIC DEFORMATIONS

The invention relates to an aircraft (10) comprising: - a fuselage (12), - two wings (14, 16) to which engine nacelles are attached and which are each connected laterally to the fuselage, one on each side thereof, by a central fairing, the central fairing (18, 20) comprising, facing each wing, two o...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	JIMENEZ, PHILIPPE, NAMER, ARNAUD, FOL, THIERRY
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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