AIRCRAFT AIR INLET COMPRISING AT LEAST TWO WALLS CONNECTED END TO END BY WELDING, METHOD FOR THE ASSEMBLY OF SUCH AN AIR INLET, AND AIRCRAFT COMPRISING AT LEAST ONE SUCH AIR INLET

An air inlet of a nacelle of an aircraft including a lip having a leading edge configured to split an air flow into interior and exterior air flows, the interior air flow entering the air inlet, an exterior panel, an intermediate panel, interposed between the lip and the exterior panel, having a fir...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	LAFLY, Anne-Laure, BROCHARD, Wolfgang
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINE PLANTS IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS STEAM ENGINES TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An air inlet of a nacelle of an aircraft including a lip having a leading edge configured to split an air flow into interior and exterior air flows, the interior air flow entering the air inlet, an exterior panel, an intermediate panel, interposed between the lip and the exterior panel, having a first edge connected to the lip by at least a first connection and a second edge connected to the exterior panel by at least a second connection, the first connection connecting the first edge of the intermediate panel and the lip comprising at least one butt weld bead having an outer face in the extension of the outer faces of the lip and of the intermediate panel.