Wing assemblies (100) comprise an inboard flight control surface (102), an outboard flight control surface (104) positioned directly adjacent to and outboard of the inboard flight control surface (102), and a dual actuation assembly (106) coupled directly to and forming a linkage between the inboard flight control surface (102) and the outboard flight control surface (104). The dual actuation assembly (106) is configured to selectively transition the inboard flight control surface (102) and the outboard flight control surface (104), in tandem, amongst a retracted configuration (108) and a range of extended configurations (110).
Wing assemblies with tandemly actuated flight control surfaces, aircraft, and related methods
2024-01-30
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
WING ASSEMBLIES WITH TANDEMLY ACTUATED FLIGHT CONTROL SURFACES, AIRCRAFT, AND RELATED METHODS
European Patent Office | 2024
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