An assembly is provided for an aircraft propulsion system. The assembly includes a fixed structure, an inner cowl door and an outer cowl door. The inner cowl door is pivotally connected to the fixed structure. The outer cowl door is pivotally connected to the fixed structure. The outer cowl door is radially outboard of and overlaps the inner cowl door. The linkage extends between and is movably connected to the inner cowl door and the outer cowl door.
Linkage(s) between inner and outer cowl doors
2022-11-29
Patent
Electronic Resource
English
AIRCRAFT NACELLE COMPRISING A COWL WITH TWO ARTICULATED DOORS
European Patent Office | 2020
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