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
30.01.2024
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
WING ASSEMBLIES WITH TANDEMLY ACTUATED FLIGHT CONTROL SURFACES, AIRCRAFT, AND RELATED METHODS
Europäisches Patentamt | 2024
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