An aircraft includes a wing and a leading-edge aerodynamic surface coupled to the wing. An actuator is disposed within the wing and coupled to the leading-edge aerodynamic surface via a linkage system. Two or more hinge systems are coupled to the leading-edge aerodynamic surface and configured to rotate about a fixed axis internal to the wing to move the leading-edge aerodynamic surface between a retracted position and a drooped position.
LEADING-EDGE DROOP ACTUATION SYSTEM
VORDERKANTENBETÄTIGUNGSSYSTEM
SYSTÈME D'ACTIONNEMENT DE BORD D'ATTAQUE
2025-06-11
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Tailoring Stall Characteristics Using Leading-Edge Droop Modifications
Online Contents | 1994
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