US2008273977A1PendingUtilityA1
Methods and Devices for Utilizing Flowing Power
Individually held — no corporate assignee on recordPriority: Jan 21, 2004Filed: Jan 21, 2005Published: Nov 6, 2008
Est. expiryJan 21, 2024(expired)· nominal 20-yr term from priority
Inventors:Jeffrey Beard
Y02E10/74F05B 2240/122F03D 3/061F05B 2250/25F03D 3/062F05B 2240/213Y02B10/30F03D 3/06F03D 3/00F05B 2240/3062
33
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Claims
Abstract
A method and apparatus related to the utilization of flowing medium is provided including a turbine blade comprising at least one protrusion along at least a portion of a surface of said blade and a twisted portion.
Claims
exact text as granted — not AI-modified1 . An turbine blade comprising:
at least one protrusion along at least a portion of a surface of said blade; and a twisted portion.
2 . The turbine blade of claim 1 wherein the at least one protrusion comprises at least one outward protrusion.
3 . The turbine blade of claim 2 wherein the at least one outward protrusion comprises at least one ridge.
4 . The turbine blade of claim 1 wherein said ridges are at least partially recessed on a surface of the blade.
5 . The turbine blade of claim 1 wherein said at least one protrusion and said twisted portion at least partially overlap.
6 . The turbine blade of claim 1 wherein said at least one protrusion is on an inside surface of the blade.
7 . The turbine blade of claim 1 wherein said ridges are on an outside surface of the blade.
8 . The turbine blade of claim 1 wherein said twisted portion is evenly distributed along the entire length of said blade.
9 . The turbine blade of claim 1 wherein said twisted portion is evenly distributed along a portion of said blade that is less than the entire length of the blade.
10 . The turbine blade of claim 1 wherein said twisted portion is unevenly distributed along the entire length of said blade.
11 . The turbine blade of claim 1 wherein said twisted portion is unevenly distributed along a portion of said blade that is less than the entire length of the blade.
12 . The turbine blade of claim 1 wherein said blade is substantially flat.
13 . The turbine blade of claim 1 wherein said blade is curved.
14 . The turbine blade of claim 1 wherein said blade is concaved on an inside surface of said blade.
15 . The turbine blade of claim 1 wherein said blade is made from a simple piece of material.
16 . The turbine blade of claim 1 wherein said blade is assembled from a plurality of pieces.
17 . The turbine blade of claim 1 wherein the at least one protrusion comprises at least one inward protrusion.
18 . The turbine blade of claim 17 wherein the at least one outward protrusion comprises at least one dimple.
19 . The turbine blade of claim 18 wherein said at least one dimple is shaped to improve wind flow over the outside surface of said blade.
20 . The turbine blade of claim 18 wherein said blade comprises a plurality of approximately uniform size dimples.
21 . The turbine blade of claim 18 wherein said blade comprises asymmetrically shaped dimples.
22 . The turbine blade of claim 18 wherein said blade comprises dimples having a plurality of sizes.
23 . The turbine blade of claim 18 wherein said dimples are at least partially recessed on a surface of the blade.
24 . The turbine blade of claim 18 , wherein said dimples have a plurality of shapes.
25 . A turbine comprising:
at least one blade including: at least one protrusion along at least a portion of said at least one blade, and a twisted portion; and at least one rotor, wherein said rotor is in communication with said at least one blade.
26 . The turbine of claim 25 wherein said at least one protrusion and said twisted portion of said blade at least partially overlap.
27 . The turbine of claim 25 wherein said at least one blade is attached on at least one end to at least one end piece.
28 . The turbine of claim 27 wherein said at least one end piece is in communication with said at least one rotor.
29 . The turbine of claim 25 wherein said turbine further comprises a shaft in communication with at the at least one blade.
30 . The turbine of claim 29 , wherein said shaft is in communication with a magnetic or flexible coupler between said blade and said rotor.
31 . The turbine of claim 29 , wherein said shaft is in communication with at least one rotor.
32 . The turbine of claim 25 wherein said at least one blade is made of materials selected from a group consisting of carbon fiber, fiber reinforced thermoplast, fiberglass, plastic, metal and epoxy.
33 . The turbine of claim 25 wherein said at least one blade comprises a plurality of blades and wherein said blades are symmetrically opposed.
34 . The turbine of claim 25 wherein said at least one blade comprises a plurality of blades and said blades are arranged in said turbine directing energy transfer from one blade to another blade.
35 . The turbine of claim 34 wherein said energy is wind energy.
36 . The turbine of claim 34 wherein said energy is hydrodynamic energy.
37 . The turbine of claim 25 wherein said at least one blade comprises a plurality of blades and said blades are arranged in said turbine directing energy transfer from one blade to another blade having unobstructed air flow through at least a portion of an approximately central axis of rotation of said turbine.
38 . The turbine of claim 37 , wherein said portion of an approximately central axis of rotation of the turbine is approximately as long as the twisted portion of the blades.
39 . The turbine of claim 25 wherein said turbine is mounted on a surface to provide an angle within a range of approximately horizontal to approximately vertical with respect to the surface upon which the turbine is mounted and an approximately central axis of rotation of said turbine.
40 . The turbine of claim 25 further comprising a wind augmentation device.
41 . The turbine of claim 25 wherein said protrusion is an outward protrusion.
42 . The turbine of claim 41 wherein said outward protrusion includes a ridge.
43 . The turbine of claim 26 wherein said ridge is shaped to resist wind flow in one direction.
44 . The turbine of claim 26 wherein said blade comprises a plurality of said ridges.
45 . The turbine of claim 26 wherein said ridges are at least partially recessed on a surface of the blade.
46 . The turbine of claim 25 wherein said protrusion is an inward protrusion.
47 . The turbine of claim 25 wherein said inward protrusion includes a dimple.
48 . The turbine of claim 25 wherein said twisted portion is evenly distributed along a portion of said blade that is less than the entire length of the blade.
49 . The turbine of claim 25 wherein said at least one blade is curved.
50 . The turbine of claim 49 , wherein said curve is concave on an inside surface of said blade.
51 . A turbine blade, wherein said blade comprises:
at least one flared portion; and a twisted portion.
52 . The turbine blade of claim 51 , wherein said flared portion and said twisted portion at least partially overlap.
53 . The turbine blade of claim 51 wherein said flared portion is widest at approximately the middle of the blade's length.
54 . The turbine blade of claim 51 wherein said blade comprises two or more flared portions.
55 . The turbine blade of claim 51 wherein said twisted portion is evenly distributed along the entire length of said blade.
56 . The turbine blade of claim 51 wherein said twisted portion is unevenly distributed along a portion of said blade that is less than the entire length of the blade.
57 . The turbine blade of claim 51 wherein said blade is curved.
58 . The turbine blade of claim 51 wherein said blade is concave on an inside surface of said blade.
59 . The turbine blade of claim 51 wherein said blade is made from a plurality of pieces.
60 . A turbine comprising:
one or more blades wherein at least one of said blades comprises a flared portion and a twisted portion; and at least one rotor, wherein said rotor is in communication with at least one of said blades.
61 . The turbine of claim 60 wherein said flared portion and said twisted portion of said blade at least partially overlap.
62 . The turbine of claim 60 wherein at least one of said blades is attached on at least one end to at least one end piece.
63 . The turbine of claim 62 wherein said end piece is in communication with at least one rotor.
64 . The turbine of claim 60 wherein said rotor is in communication with at least one actuator.
65 . The turbine of claim 60 wherein said turbine further comprises a shaft in communication with at least one of said one or more blades.
66 . The turbine of claim 65 wherein said shaft is in communication with a magnetic or flexible coupler between at least one of said one or more blades and said rotor.
67 . The turbine of claim 65 wherein said one or more blades comprises a plurality of blades which are symmetrically opposed.
68 . The turbine of claim 65 wherein said one or more blades comprises a plurality of blades and said plurality of blades are arranged in said turbine directing energy transfer from a first blade to a second blade.
69 . The turbine of claim 68 wherein said energy is wind energy.
70 . The turbine of claim 68 wherein said energy is hydrodynamic energy.
71 . The turbine of claim 68 wherein said one or more blades comprises a plurality of blades and said plurality of blades are arranged in said turbine directing energy transfer from a first blade to a second blade having unobstructed flow through at least a portion of an approximately central axis of rotation of said turbine.
72 . The turbine of claim 71 wherein said portion of an approximately central axis of rotation of the turbine is approximately as long as the twisted portion of the blades.
73 . The turbine of claim 72 wherein said portion of an approximately central axis of rotation of the turbine is approximately as long as said blades.
74 . The turbine of claim 60 wherein said turbine is mounted on a surface to provide an angle within a range of approximately horizontal to approximately vertical with respect to the surface upon which the turbine is mounted and an approximately central axis of rotation of said turbine.
75 . The turbine of claim 60 further comprising a wind augmentation device.
76 . The turbine of claim 60 wherein said flared portion is widest at approximately the middle of the blade's length.
77 . The turbine of claim 60 wherein at least one of said one or more blades comprises two or more flared portions.
78 . The turbine of claim 60 wherein said twisted portion is evenly distributed along a portion of said blade that is less than the entire length of the blade.
79 . The turbine of claim 60 wherein said twisted portion is unevenly distributed along the entire length of said blade.
80 . The turbine of claim 60 wherein said blade is curved.
81 . The turbine of claim 80 wherein said curve is concaved on an inside surface of said blade.
82 . The turbine of claim 60 wherein said at least one or more blades includes a plurality of blades wherein said blades comprise a flared portion and a twisted portion and further comprising at least one end piece attached to each end of at least two of said plurality of blades wherein said blades overlap each other at an approximately central axis of rotation having a space between said blades where the blades overlap.
83 . The turbine of claim 82 wherein said flared portion and said twisted portion of said blade are at least partially coincidental.
84 . The turbine of claim 82 wherein end pieces comprise at least one channel to accept an end edge of at least one of said blades.
85 . A method for capturing energy comprising:
providing a plurality of blades wherein at least one of said blades comprise at least one protrusion along at least a portion of the blade surface and wherein a portion of at least one of said blades is twisted; and exposing said blades to a flow stream.
86 . The method of claim 85 wherein said at least one protrusion is an outward protrusion.
87 . The method of claim 85 wherein said at least one protrusion is an inward protrusion.
88 . The method of claim 86 wherein said outward protrusion is a ridge.
89 . The method of claim 86 wherein said outward protrusion is a raised dimple.
90 . The method of claim 87 wherein said inward protrusion is a dimple.
91 . The method of claim 85 wherein a portion of at least one of said blades is flared.
92 . The method of claim 85 further comprising providing at least one rotor in communication with at least one of said blades.
93 . The method of claim 92 further comprising providing at least one actuator.
94 . The method of claim 85 wherein said providing step further comprises providing a plurality of dimples along at least a portion of said plurality of blades.
95 . The method of claim 85 wherein each blade includes a flared portion.
96 . The method of claim 85 wherein said flow stream is selected from the group consisting of airflow and water flow.
97 . The method of claim 85 wherein said blades are in connection with a central shaft.
98 . A method of translating energy comprising:
providing a plurality of blades in connection with a rotor; placing said rotor and blades in connection with an end plate; placing said rotor in communication with an actuator; and exposing said blades to a flow stream.
99 . The method of claim 98 wherein said flow stream is selected from the group consisting of airflow and water flow.
100 . The method of claim 98 wherein said providing step further comprises providing s plurality of blades wherein said blades comprise at least one ridge along at least a portion of the blade surface and wherein a portion of said blades are twisted.
101 . The method of claim 98 wherein said providing step further comprises providing s plurality of blades wherein a portion of said blades are flared.
102 . The method of claim 98 wherein said actuator is selected from a group consisting or a generator, a mill, a pump, a speed control device, and a brake.
103 . The method of claim 98 wherein said providing step further comprises providing a plurality of dimples along at least a portion of said plurality of blades.
104 . The method of claim 98 wherein said blades are in connection with a central shaft.Join the waitlist — get patent alerts
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