An air intake for a nacelle of an aircraft propulsion assembly includes an upstream section that defines an air intake flow path, a central section surrounding a fan of an engine, and a downstream section surrounding a combustion chamber of the engine. The air intake includes a disassembly mechanism which has a panel able to move between a flush closed position in which the panel provides aerodynamic continuity of the air intake in the air intake flow path, and an open maintenance position in which the panel is radially and outwardly retracted in relation to its flush closed position in order to free up a space which allows removal of a blade of the fan at its distal end.
NACELLE POUR AÉRONEF ET ENTRÉE D'AIR ASSOCIÉE
AIRCRAFT NACELLE AND ASSOCIATED AIR INLET
FLUGZEUGGONDEL UND ZUGEHÖRIGER LUFTEINLASS
2023-05-17
Patent
Electronic Resource
French
ENTRÉE D'AIR DE NACELLE ET NACELLE COMPORTANT UNE TELLE ENTRÉE D'AIR
European Patent Office | 2025
|ENTRÉE D'AIR DE NACELLE ET NACELLE COMPORTANT UNE TELLE ENTRÉE D'AIR
European Patent Office | 2020
|Entrée d’air de nacelle et nacelle comportant une telle entrée d’air
European Patent Office | 2021
|