FIELD: aviation.
SUBSTANCE: present invention relates to aeronautical equipment. Segment shock flap consists of several flat wing-shaped segments attached to the rear of the airfoil of aircraft plane b ball and shock joints. The segments are attached independently from each other to the rear of the airfoil by elbowed ball joints and shock absorbers disposed inside the wing, with addressable configured amortization rigidity, connected to the flat wing-shaped segments by moveable rods or other joint, allowing to provide a movable, spring-loaded condition of wing-shaped segments during their vibratory operation.
EFFECT: invention allows to stabilise the wing pressure.
6 dwg
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