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Wind turbine with savonius-type rotor

 Alvin H. Benesh
A Savonius rotor assembly includes two blades. Each of the blades has an outer edge and an inner edge with the outer edges of the blades lying on a circle which define the diameter of the rotor. Each of the blades has a linear portion adjacent to the inner edge and a first curved portion which is...
Inventor: Alvin H. Benesh
Primary Examiner: Christopher Verdier

U.S. Classification
416/197A; 416DIG2; 416DIG9

International Classification
F03D 306

View patent at USPTO

Citations

Patent NumberTitleIssue date
274541(unknown)Mar 1883
1413411(unknown)Apr 1922
1766765(unknown)Jun 1930
2007963(unknown)Jul 1935
4005947Fluid operated rotorFeb 1, 1977
4037983Wind motorJul 26, 1977
4039849Wind powered generating systemsAug 2, 1977
4288200Wind tower turbineSep 8, 1981
4359311Wind turbine rotorNov 16, 1982
4362470Wind turbineDec 7, 1982
4474529WindmillOct 2, 1984
4715776Wind turbine system using a savonius type rotorDec 29, 1987
4784568Wind turbine system using a vertical axis savonius-type rotorNov 15, 1988
4830570Wind turbine system using twin savonius-type rotorsMay 16, 1989
4838757Wind turbine system using a savonius type rotorJun 13, 1989

Claims

What is claimed is:

1. A Savonius rotor assembly driven by a moving fluid, said assembly comprising:

a support;
a rotor mounted on the support for rotation about an axis, the rotor including a first blade and a second blade disposed symmetrically about the axis, the rotor having a cross section defined by a plane perpendicular to the axis, the rotor in the cross section including the first and second blades, each having:
an outer edge and an inner edge with the outer edge moving in a path of a first circle around said axis, said circle defining a diameter of the rotor;
a substantially linear portion extending from the inner edge toward said outer edge and terminating at a first location, said inner edge extending substantially beyond said axis on a side thereof opposite said outer edge and spaced from said first circle by a distance less than about 0.2 times said diameter, said linear portions of said first and second blades being substantially parallel;
a first curved portion which is substantially an arc of a second circle, said first curved portion tangent to the substantially linear portion at said first location, said first curved portion terminating at a second location, said first curved portion tangent to said first circle at said second location; and
a second curved portion tangent to the first curved portion at said second location and substantially coincident with said first circle.

2. A Savonius rotor assembly according to claim 1, wherein the diameter of the second circle is 0.30 of the diameter of the rotor.

3. A Savonius rotor assembly according to claim 1, wherein the substantially linear portions of the first and second blades are spaced apart a distance of 0.15 of the diameter of the rotor.

4. A Savonius rotor assembly according to claim 1, wherein the inner edge is a distance of 0.172 of the diameter of the rotor measured on a line extending from the inner edge to the first circle in a direction parallel to the substantially linear portion.

5. A Savonius assembly according to claim 1, wherein the outer edge of the first blade is a distance of 0.32 of the diameter of the rotor from an extension of the substantially linear portion of the first blade measured on a line extending from the outer edge to the extension of the substantially linear portion in a direction perpendicular to the extension of the substantially linear portion.

6. A Savonius rotor assembly according to claim 1, wherein the inner edge of the linear portion is a distance less than 0.35 of the diameter of the rotor measured on a line extending from the inner edge to the first circle in a direction parallel to the substantially linear portion.

7. A Savonius rotor assembly according to claim 1, wherein the diameter of the first curved portion is less than 0.52 of the diameter of the rotor.

8. A rotor assembly according to claim 1 wherein a distance between said linear portions of said first and second blades is less than 0.20 of said diameter.