An aircraft engine nacelle spoiler assembly including a number of spoilers and actuators. Each spoiler has a drag surface and a nacelle connection point. The spoilers are shiftable via the actuators between a stowed position and a deployed position such that the drag surfaces are substantially parallel with the direction of relative wind when the spoilers are stowed and exposed to the relative wind when the spoilers are deployed.
Nacelle aerodynamic spoiler
2021-07-27
Patent
Electronic Resource
English
European Patent Office | 2021
|Self-adaptive nacelle spoiler device with folding mechanism and control method
European Patent Office | 2021
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