Landing flap kinematics driven by way of a pinion drive

Details Landing flap kinematics driven by way of a pinion drive Landing flap kinematics driven by way of a pinion drive

B - Operations, Transporting

64

C

B64C 9/16 (2006.01) B64C 9/20 (2006.01) B64C 13/34 (2006.01) B64C 13/38 (2006.01)

Patent

CA 2706413

The invention relates to a device for moving a trailing edge flap (10) on an aircraft wing (2), wherein the trailing edge flap comprises one or more flap segments (4, 6, 8), a first flap segment (4) being movably mounted on the wing (2) and connected to a first toothed moving element (22) driven by a first pinion (16).

L'invention concerne un dispositif de mise en mouvement d'un volet de bord de fuite (10) d'une aile d'avion (2), lequel volet de bord de fuite présente un ou plusieurs segments de volet (4, 6, 8), un premier segment de volet (4) étant monté mobile sur l'aile (2) et relié à un premier élément mobile denté (22) mû par un premier pignon (16).

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