IP Library Granted Patent US 12662987
Granted Patent B2
US 12662987 · App. 18/664,302 · Granted Jun 23, 2026

Mechanical-only, multi-use, automatically retractable vertical wind turbine, using wing drag

Inventor: Guy P. Gadola, III (Sharpsville, PA)
F03D3/066F03D3/005F05B2240/2022F05B2240/218
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Quick Facts
Patent No.
US 12662987
App. No.
18/664,302
Granted
Jun 23, 2026
Kind
B2
Abstract

What is disclosed is a vertical-axis wind turbine that looks somewhat similar to a vertical pole during no-wind or relatively low-wind conditions, i.e., when the turbine is waiting for relatively windy conditions, and that transitions between its “waiting state” and “wind harnessing state” automatically. Yet, to automatically transition between states, the turbine uses relatively few moving mechanical assemblies and uses no electric parts. The turbine has levers attached radially to a vertical mast and one or more wings attached to each lever. Each wing's mounting angle causes the wing to move the lever to which it is attached to deploy the wing(s) attached to that lever to rotate the mast. At an approximate rotation point of the mast, to avoid the deployed wing(s) from unduly opposing the mast's rotation, the wing's angle facilitates the retraction of the wing(s). The net drag of the wing(s) serves to rotate the mast.

Claims (13)

1 . A vertical-axis wind-energy-conversion system (VAWECS) comprising:

a central vertical mast;

a plurality of axles, hinges, or pivots connected radially to the central vertical mast so that each axle's, hinge's, or pivot's axis of rotation is perpendicular to the central vertical mast's axis of rotation;

a plurality of lever arms where each lever arm is connected to a said axle, hinge, or pivot,

a plurality of wings where each wing is mounted on a said lever arm so that the majority of the wing or the entire wing is on one side of one or more lever arm axle, hinge, or pivot to form an assembly of the wing and lever arm and where

the wing has a camber and

when the assembly of the wing and lever arm is oriented so that the lever arm is generally perpendicular to the vertical mast

the wing's positive-camber side generally faces toward a rotational direction of the central vertical mast and

the wing's edge furthest from the central vertical mast is tilted, about the longitudinal axis of the lever arm, toward the rotational direction of the central vertical mast.

2 . The VAWECS of claim 1 further comprising a plurality of opening angle limiters where each lever arm has a said limiter connecting the lever arm to the central vertical mast.

3 . The VAWECS of claim 1 further comprising a plurality of backstops where a said backstop for each lever arm is mounted on the central vertical mast generally on or near the longitudinal line of the vertical mast passing through the point at which the lever arm's axle, hinge, or pivot meets the central vertical mast so that the lever arm is rotationally in front of the backstop with respect to the rotation of the lever arm about the lever arm's axle, hinge, or pivot in the same general direction to which the convex side of the lever arm's wing is facing.

4 . The VAWECS of claim 1 further comprising a plurality of backstops where a backstop for each lever arm is integrated into the said lever arm's axle or hinge.

5 . The VAWECS of claim 1 further comprising a plurality of opening angle stops where an opening angle stop for each lever arm is integrated into the said lever arm's axle, hinge, or pivot.