公开(公告)号：US20240253799A1

公开(公告)日：2024-08-01

申请号：US18405325

申请日：2024-01-05

Applicant: Airbus Operations SAS

Inventor： Anne-Laure LAFLY ,  Wolfgang BROCHARD

IPC: B64D29/08 ,  F01D25/00

CPC classification number: B64D29/08 ,  F01D25/00 ,  F05D2230/239

Abstract: 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.