FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft models. The slat (1) of the wing (2) of the aircraft model is placed in front of the wing (2), pivotally connected to it along the OO1 axis, balanced by a balancer and limited in deviation by stops (4, 5). Each stop (4, 5) is made of metal wire, with one end having vertical and horizontal sections oriented in the direction of flight, the other together with the similar end of the wire of the other stop is formed by a rod (6), which is glued into the body of the slat (1) and oriented in the direction of flight. The balancer is formed by a rod (6) and stops (4, 5). Between the latter, in the continuation of the base plane of the wing (2), there is a spike (7) limiting the angle of deflection of the slat, rigidly connected to the wing (2). At large angles of attack of the model, the stops (4 or 5) contact the spike (7) and thus the angle of deflection of the slat (1) is limited.
EFFECT: invention is aimed at improving the efficiency of the wing slat of the aircraft model.
1 cl, 1 dwg
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