Nacelle for turbojet engine of aircraft, has median section surrounding blower and connected to air inlet, where section comprises external panel constituted by monoblock wall that forms external panel for air inlet

摘要

The nacelle (100) has an air inlet for canalizing an air flow towards a blower of a turbojet engine. A median section (5) surrounds the blower and connected to the air inlet. The median section has an external panel constituted by a monoblock wall (60) that forms an external panel for the air inlet. The monoblock wall is mounted movable in translation along a longitudinal axis of the nacelle. The air inlet is divided into an inlet lip (4a) and a downstream structure.