An actuator system (100) is described herein for actuating movement of a control surface (3) of an aircraft wing (1), said system (100) comprising: a common input rail (160) connectable to a means for providing movement to said input rail (160); a plurality of rotary geared actuators "RGAs" (110); a common output rail (130) connectable to said control surface (3); wherein each of said plurality of RGAs (110) is connected to said input rail (160) by an individual input clutch (170) and also connected to said output rail (130) by an individual output clutch (171), and wherein the input clutch (170) functions independently of the output clutch (171). A method for manufacturing such an actuator system (100) is also disclosed.
ROTARY ACTUATION FOR THIN WING APPLICATIONS
ACTIONNEMENT ROTATIF POUR DES APPLICATIONS D'AILE MINCE
21.10.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Beam-penetrating spline rotary actuation folding wing and aircraft
Europäisches Patentamt | 2024
|