FIELD: aviation.
SUBSTANCE: invention relates to aviation. Aircraft wing flap sliding device comprises beam fixed on wing, on which there is hinged link carrying front, rear bearing link and rocker. With front and rear bearing links hinged link front suspension of flap, which is articulated with rocker by link synchronisation, one arm of which is pivotally connected with link synchronisation, and second arm is with flap rear suspension link. Flap front suspension link is attached to flap beam by means of ball joint. Flap rear suspension link is connected to rocker and to flap beam by means of ball joints.
EFFECT: reduced internal stresses in links.
5 cl, 4 dwg
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