Fluid Turbine Rotor Blade

Abstract

A fluid turbine has semi-spherical, hollow blades arrayed about a vertical axis. The turbine's blade shape reduces drag on a convex side and increases drag on a concave side. Part of the center of the array of rotor blades is open, allowing flow through the center of the array. The spherical form enhances fluid flow through the center of the array and results in rotational force on a downwind blade, and directs fresh air into bypass flow. A combination of holes and a deflector surface generates vortices as updraft flow passes through holes, creating a pressure differential between the area surrounding the holes and the upper portions of the blade. Fluid passing from relatively higher pressure to relatively lower pressure passes the deflector surface, forming vortices that result in rotational force on the blades of the fluid turbine.

Claims

1. A rotor blade for a vertical axis fluid turbine comprising: A horizontal surface, having a first end proximal to the top of the rotor blade, and a second end proximal to the bottom of the rotor blade; and a curved surface extending between said first end and said second end, having a concave side, a convex side, a vertical edge; and a vertical central axis, parallel to the vertical edge; and an empty space extending between said first end and said second end, and proximal to said vertical central axis and proximal to said vertical edge of said curved surface; and an array of holes in said horizontal surface second end, proximal to the bottom of the rotor blade; wherein in a fluid stream, the concave side of said curved surface exhibits more drag than the convex side, resulting in rotation about said vertical central axis and fluid moves through said array of holes, forming vortices that exert a force on the concave side of said curved surface.

2. The rotor blade of claim 1 further comprising: a deflector surface offset from, and joined to, said horizontal surface surface second end, and proximal to said array of holes; wherein fluid that moves through said array of holes is deflected by said deflector surface, resulting in a relatively higher pressure proximal to the holes and a relatively lower pressure in the area of the blade above said deflector surface, drawing fluid flow from said relatively higher pressure to said relatively lower pressure forming a vortex which results in a force on said concave side of said curved surface of said rotor blade.

3. The rotor blade of claim 2 wherein the deflector surface is offset from said horizontal surface second end by a ratio that is between 1/14 and 1/36 of the overall height of the rotor blade.

4. The rotor blade of claim 2, the deflector surface further comprising: a root proximal to said vertical central axis, and a tip relatively further from said vertical central axis; wherein the offset distance between the tip and said segment of a spherical surface second end is smaller than the offset distance between the root and said horizontal surface second end.

5. A vertical axis fluid turbine comprising: a rotor assembly having at least two rotor blades, each rotor blade in said rotor assembly comprising: a segment of a spherical surface residing on a datum sphere, having a first end proximal to the top of the rotor blade, and a second end proximal to the bottom of the rotor blade; and a curved surface extending between said first end and said second end, having a concave side and a convex side, a vertical edge; and a vertical central axis parallel to the vertical edge, extending through a center of said datum sphere, and through the center of said rotor assembly; and an empty space extending between said first end and said second end and proximal to said vertical central axis and proximal to said vertical edge of said curved surface; and an array of holes in said segment of a spherical surface, second end, proximal to the bottom of the rotor blade; wherein fluid flowing over one of said at least two rotor blades exerts a force on said curved surface concave side, flows without obstruction through said empty space between said first end and said second end and proximal to said vertical central axis and then flows over, and exerts a force on, a second of said at least two rotor blades, curved surface concave side, as the fluid exits the rotor assembly; while updraft fluid flow passes through said array of holes, causing a vortex that in turn exerts a force on said curved surface concave side of each of said at least two rotor blades.

6. The vertical axis fluid turbine of claim 5 wherein: each rotor blade in said rotor assembly further comprises: a deflector surface offset from, and joined to, said segment of a spherical surface second end, and proximal to said array of holes; wherein fluid moves through said array of holes, is deflected by said deflector surface, resulting in a relatively higher pressure proximal to the holes and a relatively lower pressure in the area of the blade above said deflector surface, drawing fluid flow from said relatively higher pressure to said relatively lower pressure forming a vortex which results in a force on said concave side of said curved surface of each said rotor blade in said rotor assembly.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0014] FIG. 1 is a front perspective view of an example embodiment;

[0015] FIG. 2 is a bottom, perspective view of the embodiment thereof;

[0016] FIG. 3 is a perspective view of a rotor blade thereof;

[0017] FIG. 4 is a top, cross section flow diagram of the embodiment thereof;

[0018] FIG. 5 is a color diagram of the flow diagram of FIG. 4;

[0019] FIG. 6 is a cutaway perspective view thereof;

[0020] FIG. 7 is a side, cross section, flow diagram thereof;

[0021] FIG. 8 is a computer fluid dynamic image of the embodiment;

[0022] FIG. 9 is a detailed, computer fluid dynamic image thereof;

[0023] FIG. 10 is a detailed, computer fluid dynamic image thereof.

DESCRIPTION

[0024] Referring to FIG. 1 FIG. 2 and FIG. 3, rotor blades 110 are arrayed about a central axis 118. The central axis may be said to reside vertically, in the center of a datum sphere. Each rotor blade's inner, longitudinally oriented surface is concave 113 and each longitudinally oriented, outer surface is convex 111. The concave inner surface 113 experiences increased drag in a fluid stream while the convex side 111 experiences relatively less drag. Latitudinally, each rotor blade has an upper surface 112 and a lower surface 114 which are both substantially perpendicular to the concave/convex surfaces 113/111. The upper surface 112 and lower surface 114 are coincident with a spherical datum surface and may be said to be formed from a segment of the datum sphere having an upper end 112 and a lower end 114. Each rotor blade lower surface 114 has an array of holes 116 proximal to a deflector surface 120. The combination holes 116 and deflector surface 120 divert fluid flow from turbulent updrafts, toward the concave inner surface 113 by creating a pressure differential between the holes and the rest of the blade inlet. The resultant low-pressure zone at the blade tip sucks surrounding flow in to encourage the formation of a vortex.

[0025] One skilled in the art understands that the rotor blades 110 may be connected to a shaft configured to turn a generator. The overall shape of the blades when assembled is that of a sphere. In an example embodiment, rotor blades are constructed of a fiber-reinforced polymer combined with a dye that appears fluorescent to birds and as monochromatic to humans.

[0026] The illustration in FIG. 4 is a top, cross-section view depicting flow through the turbine 100. The example embodiment shows four rotor blades 110, each having a concave side 113 and a convex side 111. One blade is at θ=0°, one at θ=90°, one at θ=180°, and another at θ=270°, One skilled in the art understands that the convex side 111 exhibits less drag when facing the fluid stream than a concave side 113. The rotor blade at θ=180°, while the concave side 113 exhibits greater drag when facing the fluid stream, causing rotation of the blades. In this view the apparatus is rotating in a clockwise rotation. Vortices generated by the combination holes 116 and deflector surface 120 result in a vortex in the outer region of each blade thus increasing the rotational force on each blade. An array of holes 116 is shown on each blade in dashed line, or hidden line, as the holes are beneath deflectors 120 in the view in FIG. 4. Fluid flowing through holes 116 around deflectors 120 result in vortices 131 which result in force vector(s) 148 thus increasing the rotational force on the rotor assembly.

[0027] FIGS. 4 and 5 show a fluid stream meeting the turbine as an impediment, causing some of the stream 132 to flow past the turbine. This is referred to as bypass flow 132. The primary means of energy extraction occurs when a portion of the fluid stream 136 flows into the concave side of a blade 113, at position forming the resultant force vector 140. Some of the fluid stream flowing into the concave side of the blades at positions θ=270°, and θ=0°, are depicted by lines 136. Another portion of the fluid stream flows into the concave side of a blade at position θ=270 is shown as fluid stream 138. In one example, a portion of the fluid stream 136 and another portion of the fluid stream 138 encounters the concave side of a rotor blade at θ=270°, initially interacting with the concave side of the blade at θ=270°, creating the resultant force vector 144. The fluid then flows through the center of the turbine to the concave side of a rotor blade at position θ=90°, creating the resultant force vector 142. Some of the fluid 138 passes through the open center 139 of the turbine and creates a resultant force vector 142. Other portions of the fluid stream 134 flow through the center and out an upstream blade at θ=180°, creating force vector 146 before exiting the turbine to mix with bypass flow 132.

[0028] FIG. 6 is a flow diagram depicting a fluid stream moving through a vertical cross-section of the rotor blades. The spherical form of the rotor assembly guides the portion of the stream 136 through the open center of the rotor assembly. The portion of the fluid stream 136 is compressed as it passes through the turbine. Specifically, as it passes through the rotor assembly, some of the flow 136 becomes compressed, increasing in velocity. This compressed, higher-velocity fluid stream is depicted in dashed-line area 137. The higher velocity flow 137 then mixes with the relatively slower bypass flow 132 in the region of the turbine wake.

[0029] FIG. 7 shows a computer fluid-dynamics image of some of the wake flow 137 traveling at a relatively higher velocity than the wake flow 141.

[0030] FIG. 8 is a cutaway, perspective view showing the open center 139 and an example fluid stream line 136 creating force vectors 144 and 142 as it passes through the turbine, impacting concave surfaces 113. Vortices 131 generated by the combination of holes 116 and deflector surfaces 120 exert a force on the inner, concave surface of each rotor blade. One skilled in the art understands how the flow diagram of FIG. 4 applies to the perspective view of FIG. 8.

[0031] FIG. 9 and FIG. 10 illustrate the vortex created by the combination of holes 116 and deflector 120 that generates a force against the concave blade surface 113. The central axis 118 is shown for reference. A portion of updraft flow 133 (FIG. 10) passes through holes 116, is flows along the deflector surface 120 and enters the interior of the turbine blade as a vortex 131. A relatively higher pressure forms at the holes 116, beneath the deflector 120, than that of the rest of the interior of the blade. The resultant low pressure area at the blade tip sucks the surrounding air into the blade encouraging the formation of a vortex 131 which in turn forces air to the extremities of the blade resulting in additional rotational force on the rotor.

[0032] In some embodiments the ratio of open space in the center of the turbine to the area occupied by the rotor blades is between 1:5 and 1:7 and in one embodiment is approximately 1:6.

[0033] While example embodiments have been described herein, it is expressly noted that these embodiments should not be construed as limiting, but rather that additions and modifications to what is expressly described herein also are included within the scope of the invention. Moreover, it is to be understood that the features of the various embodiments described herein are not mutually exclusive and can exist in various combinations and permutations, even if such combinations or permutations are not made express herein, without departing from the spirit and scope of the invention.