FIELD: transportation.
SUBSTANCE: method of controlling the wing placed in the fluid medium at its interaction with the said medium consists in that the wing is arranged at an angle of attack, sufficient for the said interaction. The wing part is isolated by the stabiliser, given its not hinged mounting relative to an axis of rotation of the wing with the angle of attack outrunning the angle of attack in motion, and the wing is turned till stalling on the said wing part. The device intended for using this method has a fixed support connected to the beam via a movable linkage, a carriage hinged on to the latter, at least one wing and a drive. The device is provided with a plate pivoted on to the carriage and provided with a kinematics linkage with the wing, also pivoted on to the carriage. The drive is made so that to be supplied from an appropriate source. At least one wing part is isolated by the stabiliser, given its not hinged mounting relative to an axis of rotation of the wing with the angle of attack outrunning the angle of attack in motion, and the wing is turned till stalling on the said wing part. The wing and its part are provided with a dynamic force pickup connected in the drive electric circuitry via an amplifier. The drive can be controlled by programmed signals of the programming device connected in the drive electric circuit. Apart the wing part isolated by the stabiliser, one more wing part is isolated by the stabiliser and is turned relative to the axis of rotation the other side.
EFFECT: increase in wing speed and in aerohydrodynamic lift on it.
4 cl, 4 dwg
