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Inventor(s): |
Benesh;
Alvin H. , Pierre, SD 57501
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Applicant(s): |
none
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Issued/Filed
Dates: |
Feb.
27, 1996 / Dec. 16, 1994
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Application
Number: |
US1994000357701
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IPC
Class: |
F03D
3/06;
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Class: |
Current:416/197.A;416/DIG.002;
416/DIG.009;
Original:416/197.A;416/DIG.2;
416/DIG.9;
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Field
of Search: |
416/197
A,243,DIG. 2,DIG. 9 415/2.1,4.1-4.5,905,907
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Legal
Status: |
Show
legal status actions
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Abstract: |
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 substantially an arc of a circle tangent to the linear portion
and tangent to the circle defining the rotor diameter. A second curved
portion is substantially coincident to the circle defining the rotor diameter.
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Attorney,
Agent, or Firm: |
Merchant,
Gould, Smith, Edell, Welter & Schmidt;
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Primary/Assistant
Examiners: |
Look;
Edward K.; Verdier; Christopher
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U.S.
References: |
(No patents reference this one)
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CLAIMS:
[Hide
claims]: |
What
is claimed is:
1. A Savonius rotor
assembly driven by a moving fluid, said assembly comprising:
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a support;
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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:
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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;
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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;
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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
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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.
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Background/Summary: |
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background/summary
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Drawing
Descriptions: |
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drawing descriptions
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Description
of Preferred Embodiments: |
Show
description of preferred embodiments
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Foreign
References: |

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Other
References:
Article info links
by
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Augmentation of Power
in Slow-Running Vertical-Axis Wind Rotors Using Multiple Vanes, Sivasegaram
et al., Wind Engineering, vol. 7, No. 1, 1983, pp. 12-19.
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Design of a Prototype
Improved Savonius Rotor: "As A System Totality", Rao, pp. 967-973 (no date).
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Article entitled "Vertical
Axis Wind Rotors-Status and Potential", from Wind Energy Conservation,
pp. 28-29 (no date, but published prior to date of application).
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"The Savonius Super Rotor!"
by Michael Hackleman reprinted from the Mother Earth News, No. 193 (no
date, but published prior to date of application).
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Mechanical Engineering,
Vo. 53, May 1931, No. 5, "The S-Rotor and Its Applications" by Savonius.
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The Wind Power Book by
Jack Park, 1981, pp. 93-95.
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Newsletter 1, A Supplement
to Wind and Wind Spinners, Jul. 1975, pp. 1-26.
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"Wind Tunnel Performance
Data for Two-and Three-Bucket Savonius Rotors", Report No. SAND 76-0131,
Jul., 1977 authored by Blackwell, et al.
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Paper Presented at the
Second International Symposium on Wind Energy Systems, held in Amsterdam,
Netherlands, Oct. 3rd-6th, 1978, vol. 2, pp. F3-30 to F3-34.
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