FIELD: aviation.
SUBSTANCE: elastomer control surface based on the continuous bypassing processing technology comprises the first control surface (712) connected to the hydrogasdynamic housing (704); and the first elastomeric coupling means (702) connected to the first control surface (712) and the hydrogasdynamic housing (704) such that the first butt gap (716) formed while the first control surface (712) moving relative to the hydrogasdynamic housing (704) is filled. The hydrogasdynamic housing (704) comprises a wing. The first control surface (712) comprises a movable trailing edge (706) with the possibility to move in the rear direction to increase the wing area on one side, and thus creating an additional lifting force and initiating a corresponding roll-off. The method characterizes the creation of an elastomer control surface.
EFFECT: improved aerodynamic characteristics.
14 cl, 9 dwg
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