FIELD: aircraft engineering.
SUBSTANCE: invention relates to aircraft engineering and can be used to create highly efficient and manoeuvrable unmanned aerial vehicles or individual use vehicles. Electric motor, the rotation speed of which is controlled by the control unit, creates a circular motion of the carrier. Circular motion is transmitted to wing axes via ball-shaped ends. Since the axes are fixed on the bearings of the vertical axes of the cardan cross-pieces, the cross-section of the plane of the wings on the entire cone-circular motion of the wing will be in the position created by the position of the vertical axis of the cross-piece. Position of the vertical axis of the cross-piece is adjusted by the position of its horizontal axis fixed through bearings to the bushing. Position of the bushing is adjusted by linear movement of the motor shaft. To increase the efficiency of lift generation, the wing has an aerodynamic profile with a convexity towards the top of the upper surface of the wing and a concavity towards the top of the lower surface of the wing.
EFFECT: higher efficiency of aircraft lift.
1 cl, 5 dwg
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Authors
Dates
2024-12-16—Published
2024-05-20—Filed