An assembly is provided for an aircraft propulsion system (10). The assembly includes a fixed structure (27), an inner cowl door (32) and an outer cowl door (40). The inner cowl door (32) is pivotally connected to the fixed structure (27). The outer cowl door (40) is pivotally connected to the fixed structure (27). The outer cowl door (40) is radially outboard of and overlaps the inner cowl door (32). A linkage (46) extends between and is movably connected to the inner cowl door (32) and the outer cowl door (40).
LINKAGE(S) BETWEEN INNER AND OUTER COWL DOORS
VERBINDUNG(EN) ZWISCHEN INNERER UND ÄUSSERER TRIEBWERKSVERKLEIDUNG
LIAISON(S) ENTRE DES PORTES DE CAPOT INTERNES ET EXTERNES
2024-05-29
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
AIRCRAFT NACELLE COMPRISING A COWL WITH TWO ARTICULATED DOORS
European Patent Office | 2020
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