US20110135460A1 - Fluid turbine with ejector shroud - Google Patents

Fluid turbine with ejector shroud Download PDF

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Publication number
US20110135460A1
US20110135460A1 US12/983,066 US98306610A US2011135460A1 US 20110135460 A1 US20110135460 A1 US 20110135460A1 US 98306610 A US98306610 A US 98306610A US 2011135460 A1 US2011135460 A1 US 2011135460A1
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United States
Prior art keywords
shroud
turbine
ejector
ratio
fluid
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Abandoned
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US12/983,066
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English (en)
Inventor
Walter M. Presz, Jr.
Michael J. Werle
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
FloDesign Wind Turbine Corp
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FloDesign Wind Turbine Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US12/054,050 external-priority patent/US8021100B2/en
Application filed by FloDesign Wind Turbine Corp filed Critical FloDesign Wind Turbine Corp
Priority to US12/983,066 priority Critical patent/US20110135460A1/en
Assigned to FLODESIGN WIND TURBINE CORP. reassignment FLODESIGN WIND TURBINE CORP. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: PRESZ, WALTER M., JR., WERLE, MICHAEL J.
Publication of US20110135460A1 publication Critical patent/US20110135460A1/en
Abandoned legal-status Critical Current

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    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D1/00—Wind motors with rotation axis substantially parallel to the air flow entering the rotor 
    • F03D1/04—Wind motors with rotation axis substantially parallel to the air flow entering the rotor  having stationary wind-guiding means, e.g. with shrouds or channels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/10—Stators
    • F05B2240/13—Stators to collect or cause flow towards or away from turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2240/00—Components
    • F05B2240/10—Stators
    • F05B2240/13—Stators to collect or cause flow towards or away from turbines
    • F05B2240/133—Stators to collect or cause flow towards or away from turbines with a convergent-divergent guiding structure, e.g. a Venturi conduit
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/60—Fluid transfer
    • F05B2260/601—Fluid transfer using an ejector or a jet pump
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/96—Preventing, counteracting or reducing vibration or noise
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/72—Wind turbines with rotation axis in wind direction

Definitions

  • the present disclosure relates to a shrouded fluid turbine having a turbine shroud and an ejector shroud downstream of the turbine shroud and surrounding the rear end of the turbine shroud. It has been discovered that a shorter ejector shroud achieves higher efficiency and lower weight compared to previous shrouded wind turbines.
  • the fluid turbines may be used to extract energy from fluids such as air (i.e. wind) or water.
  • the aerodynamic principles of a mixer ejector wind turbine also apply to hydrodynamic principles of a mixer ejector water turbine.
  • HAWTs horizontal axis wind turbines
  • Conventional horizontal axis wind turbines (HAWTs) used for power generation have two to five open blades arranged like a propeller, the blades being mounted to a horizontal shaft that is engaged with a power generator.
  • HAWTs will not exceed 59.3% efficiency in capturing the potential energy of the wind in the blades swept area. It would be desirable to increase the efficiency of a fluid turbine by collecting additional energy from the fluid.
  • the present disclosure relates to fluid turbines comprising a turbine shroud and an ejector shroud.
  • the turbine shroud has mixing lobes along a trailing edge of the turbine shroud.
  • the turbine shroud has an axial length L M
  • the ejector shroud has an axial length L E
  • the ratio of L M to L E is greater than in prior shrouded wind turbines.
  • a fluid turbine comprising a turbine shroud and an ejector shroud.
  • the turbine shroud has a front end and a rear end.
  • the ejector shroud has an inlet end and an exhaust end.
  • the rear end of the turbine shroud comprises a plurality of mixing lobes along a trailing edge, the mixing lobes extending into the inlet end of the ejector shroud.
  • the turbine shroud has an axial length L M .
  • the ejector shroud has an axial length L E .
  • the ratio of L M to L E is from 0.05 to 2.5
  • the ratio of L M to L E is from 0.16 to 2.1
  • the ejector shroud has an outer diameter D I at the inlet end, and the ratio of L E to D I may be from 0.05 to 3.0
  • the ejector shroud has an outer diameter D E at the exhaust end, and the ratio of L E to D E may be from 0.05 to 3.0
  • the turbine shroud has an outer diameter D F at the front end, and the ratio of L M to D F may be from 0.1 to 2.5
  • the turbine shroud has an outer diameter D RO at the rear end, and the ratio of L M to D RO may be from 0.1 to 1.25
  • the turbine shroud has an inner diameter D RI at the rear end, and the ratio of L M to D RI may be from 0.1 to 3.5
  • the ratio of D RO to D RI may be from 0.7 to 2
  • the wind turbine has a total axial length L T , and the ratio of L M to L T may be from 0.05 to 1.0, including from 0.1 to 0.9
  • the ratio of L E to L T may be from 0.05 to 0.9
  • the ejector shroud has a ring airfoil shape and does not have mixing lobes. In other embodiments, the ejector shroud has mixing lobes.
  • the plurality of mixing lobes on the turbine shroud includes a set of high energy mixing lobes and a set of low energy mixing lobes, the high energy mixing lobes having an angle of about 10° to about 50° relative to a horizontal axis that is parallel to the central axis of the turbine shroud.
  • the fluid turbine may further comprise a nacelle body located within the turbine shroud.
  • the nacelle body, turbine shroud, and ejector shroud are coaxial to each other.
  • the nacelle body includes a central passageway.
  • a fluid turbine comprising a turbine shroud and an ejector shroud.
  • the turbine shroud has a front end and a rear end.
  • the ejector shroud has an inlet end and an exhaust end.
  • the rear end of the turbine shroud comprises a plurality of mixing lobes along a trailing edge, the mixing lobes extending into the inlet end of the ejector shroud.
  • the turbine shroud has an axial length L M .
  • the ejector shroud has an axial length L E , an outer diameter D, at the inlet end, and an outer diameter D E at the exhaust end.
  • the ratio of L M to L E is from 0.05 to 2.5; the ratio of L E to D i is from 0.05 to 3; and the ratio of L E to D E is from 0.05 to 3
  • FIG. 1 is a cross-sectional view of a first exemplary embodiment of a shrouded fluid turbine of the present disclosure, marked with reference numerals.
  • FIG. 2 is a cross-sectional view of the shrouded fluid turbine of FIG. 1 , showing various lengths of the fluid turbine.
  • FIG. 3 is a front left perspective view of the shrouded fluid turbine of FIG. 1 .
  • FIG. 4 is a rear right perspective view of the shrouded fluid turbine of FIG. 1 .
  • FIG. 5 is a front left perspective view of the shrouded fluid turbine of FIG. 1 with the rotor and nacelle removed, so that other aspects of the fluid turbine can be more clearly seen and explained.
  • FIGS. 6A-6C are rear perspective cut-away views of the shrouded fluid turbine of FIG. 1 .
  • the rotor and nacelle are removed so that other aspects of the wind turbine can be more clearly seen and explained.
  • the cross-sectional area at the rotor of the turbine shroud, the exit area of the turbine shroud, and the exit area of the ejector shroud are illustrated here.
  • FIG. 7 is a rear view of the shrouded wind turbine of FIG. 1 .
  • the rotor and nacelle are removed from this figure so that other aspects of the wind turbine can be more clearly seen and explained.
  • FIG. 8 is a smaller view of the fluid turbine of FIG. 1 .
  • FIG. 8A and FIG. 8B are magnified views of the mixing lobes of the wind turbine of FIG. 8 .
  • FIG. 9 is a cross-sectional view of a second exemplary embodiment of a shrouded wind turbine of the present disclosure.
  • FIG. 10 is a cross-sectional view of the shrouded fluid turbine of FIG. 9 , showing various lengths of the fluid turbine.
  • FIG. 11 is a cross-sectional view comparing the first exemplary embodiment of FIG. 1 with the second exemplary embodiment of FIG. 9 .
  • FIG. 12 is a chart showing the power output (kilowatts) versus the wind velocity (mph), comparing a wind turbine with a shorter ejector shroud (i.e. the turbine of FIG. 9 ) to a wind turbine having a longer ejector shroud (i.e. the turbine of FIG. 1 ).
  • a Mixer-Ejector Fluid/Water Turbine provides an improved means of generating power from fluid currents.
  • a primary shroud contains an impeller which extracts power from a primary fluid stream.
  • a mixer-ejector pump is included that ingests flow from the primary fluid stream and secondary flow, and promotes turbulent mixing of the two fluid streams. This enhances the power system by increasing the amount of fluid flow through the system, increasing the velocity at the rotor for more power availability, and reducing back pressure on turbine blades. Additional benefits include, among others, the reduction of noise propagating from the system.
  • impeller is used herein to refer to any assembly in which blades are attached to a shaft and able to rotate, allowing for the generation of power or energy from fluid rotating the blades.
  • exemplary impellers include a propeller or a rotor (which may be part of a rotor/stator assembly). Any type of impeller may be enclosed within the turbine shroud in the fluid turbine of the present disclosure.
  • the leading edge of a turbine shroud may be considered the front of the fluid turbine, and the trailing edge of an ejector shroud may be considered the rear of the fluid turbine.
  • a first component of the fluid turbine located closer to the front of the turbine may be considered “upstream” of a second component located closer to the rear of the turbine. Put another way, the second component is “downstream” of the first component.
  • the present disclosure relates to shrouded fluid turbines having an ejector shroud downstream of a turbine shroud.
  • the axial length of the ejector shroud is much shorter than in prior versions, which provides an unexpected increase in the efficiency of the fluid turbine.
  • FIGS. 1-8 are various views of a first exemplary embodiment of a shrouded fluid turbine of the present disclosure.
  • the shrouded wind turbine 100 comprises an aerodynamically contoured turbine shroud 110 , an aerodynamically contoured nacelle body 150 , an impeller 140 , and an aerodynamically contoured ejector shroud 120 .
  • the turbine shroud 110 includes a front end 112 , also known as an inlet end.
  • the turbine shroud 110 also includes a rear end 114 , also known as an exhaust end.
  • the ejector shroud 120 includes a front end or inlet end 122 , and a rear end or exhaust end 124 . Support members 106 are shown connecting the turbine shroud 110 to the ejector shroud 120 .
  • the rotor 146 surrounds the nacelle body 150 .
  • the impeller 140 is a rotor/stator assembly comprising a stator 142 and a rotor 146 .
  • the rotor 146 is downstream and co-axial with the stator 142 .
  • the rotor 146 comprises a central hub 141 at the proximal end of the rotor blades.
  • the central hub 141 is rotationally engaged with the nacelle body 150 .
  • the nacelle body 150 is connected to the turbine shroud 110 through the stator 142 , or by other aerodynamically neutral support structures.
  • a central passageway 152 extends through the nacelle body 150 .
  • the turbine shroud has the cross-sectional shape of an airfoil with the suction side (i.e. low pressure side) on the interior of the shroud.
  • the rear end 114 of the turbine shroud also has mixing lobes 116 .
  • the mixing lobes extend downstream beyond the rotor blades.
  • the trailing edge 118 of the turbine shroud is formed from a plurality of mixing lobes.
  • the rear or downstream end of the turbine shroud is shaped to form two different sets of mixing lobes.
  • High energy mixing lobes 117 extend inwardly towards the central axis 105 of the mixer shroud.
  • Low energy mixing lobes 119 extend outwardly away from the central axis 105 . These mixing lobes are more easily seen in FIG. 4 and FIGS. 6A-6C .
  • a mixer-ejector pump (indicated by reference numeral 101 , FIG. 5 ) comprises an ejector shroud 120 surrounding the ring of high energy mixing lobes 117 and low energy mixing lobes 119 on the turbine shroud 110 .
  • the mixing lobes extend downstream and into an inlet end 122 (see FIG. 1 ) of the ejector shroud 120 .
  • This mixer-ejector pump provides the means for consistently exceeding the operational efficiency of an open-bladed wind turbine of the same rotor size.
  • the turbine shroud 110 has an axial length L M .
  • the ejector shroud 120 has an axial length L E .
  • the entire turbine itself has an axial length L T .
  • the turbine shroud 110 has a throat diameter D F .
  • This throat diameter D F is measured as the smallest diameter of the turbine shroud, and is generally located near the rotor 146 .
  • the rear end 114 of the turbine shroud has an inner diameter D RI and an outer diameter D RO .
  • the inner diameter D RI is measured as the diameter of a circle formed by the trailing edges of the high energy mixing lobes 117 .
  • the outer diameter D RO is measured as the diameter of a circle formed by the trailing edges of the low energy mixing lobes 119 . It should be recognized that generally D F >D RI , D RO >D RI , and D RO >D F . These diameters are also depicted in FIG. 7 .
  • the ejector shroud 120 also has a throat diameter D I .
  • This throat diameter D I is measured as the smallest diameter of the ejector shroud, and is generally located near the inlet end 122 .
  • the ejector shroud 120 also has an outer diameter D E at the exhaust end 124 . This outer diameter is measured as the diameter of a circle formed by the trailing edge 128 of the ejector shroud 120 .
  • L T >L M +L E .
  • the ratio of L M to L E is from 0.05 to 2.5, including from 0.16 to 2.1
  • the ratio of L M to L T may be from 0.1 to 1.0
  • the ratio or L E to L T may be from 0.05 to 0.9
  • the ratio of the ejector shroud length L E to throat diameter D I may be from 0.05 to 3
  • the ratio of the ejector shroud length L E to outer diameter D E may be from 0.05 to 3
  • the ratio of the turbine shroud length L M to throat diameter D F may be from 0.1 to 2.5
  • the ratio of the turbine shroud length L M to the rear end outer diameter D RO may be from 0.1 to 1.25
  • the ratio of the turbine shroud length L M to the rear end inner diameter D RI may be from 0.1 to 3.5
  • the ratio of D RO to D RI may be from 0.7 to 2
  • the nacelle body 150 plug trailing edge included angle A N ( FIG. 1 ) will be thirty degrees or less.
  • the length to diameter (L/D) of the overall wind turbine, or in other words, the ratio of L T to D E will be from 0.05 to 3.0
  • the turbine shroud's entrance area and exit area will be equal to or greater than that of the annulus occupied by the rotor.
  • the internal flow path cross-sectional area formed by the annulus between the nacelle body and the interior surface of the turbine shroud is aerodynamically shaped to have a minimum cross-sectional area at the plane of the turbine and to otherwise vary smoothly from their respective entrance planes to their exit planes.
  • the ejector shroud entrance area is greater than the exit plane area of the turbine shroud.
  • the cross-sectional area of the throat of the turbine shroud 110 is represented by the grid area 154 .
  • the exit area of the turbine shroud at the trailing edge 114 is represented by the grid area 156 .
  • the exit area of the ejector shroud at the trailing edge 128 of the ejector shroud 120 is represented by grid area 158 .
  • the area ratio of the ejector pump, as defined by the ejector shroud exit area 158 over the turbine shroud exit area 156 will be in the range of 1.25-3.0.
  • the number of each type of mixing lobe can be between 6 and 28.
  • the height-to-width ratio of the lobe channels will be between 0.5 and 5.0.
  • the mixing lobe penetration will be between 30% and 80%.
  • the turbine shroud 110 has a set of high energy mixing lobes 117 that extend inwards toward the central axis 105 of the turbine.
  • the turbine shroud also has a set of low energy mixing lobes 119 that extend outwards away from the central axis.
  • the high energy mixing lobes alternate with the low energy mixing lobes around the trailing edge 118 of the turbine shroud.
  • the impeller 140 , turbine shroud 110 , and ejector shroud 120 are coaxial with each other, i.e. they share a common central axis 105 .
  • the trailing edge 118 of the turbine shroud 110 has a circular crenellated shape.
  • the trailing edge can be described as including several inner circumferentially spaced arcuate portions 182 which each have the same radius of curvature. Those inner arcuate portions 182 are evenly spaced apart from each other. Between portions 182 are several outer arcuate portions 184 , which each have the same radius of curvature. The radius of curvature for the inner arcuate portions 182 is different from the radius of curvature for the outer arcuate portions 184 , but the inner arcuate portions and outer arcuate portions have the same center (i.e. along the central axis 105 ).
  • the inner arcuate portions 182 and the outer arcuate portions 184 are then connected to each other by radially extending portions 186 .
  • the term “crenellated” as used herein does not require the inner arcuate portions, outer arcuate portions, and radially extending portions to be straight lines, but instead refers to the general up-and-down or in-and-out shape of the trailing edge.
  • This crenellated structure forms two sets of mixing lobes, high energy mixing lobes 117 and low energy mixing lobes 119 .
  • free stream fluid (indicated generally by arrow 160 , and which may be, for example, air or water) passing through the stator 142 has its energy extracted by the rotor 146 .
  • High energy fluid indicated by arrow 162 bypasses the turbine shroud 110 and stator 142 , flows over the exterior of the turbine shroud 110 , and is directed inwardly by the high energy mixing lobes 117 .
  • the low energy mixing lobes 119 cause the low energy fluid exiting downstream from the rotor 140 to be mixed with the high energy fluid 162 .
  • the high energy fluid 162 enters the ejector shroud 120 .
  • the ejector shroud camber creates a relatively lower pressure on the inner surface of the ejector, in the proximity of the leading edge 122 , compared to the pressure on the outside of the ejector shroud 120 .
  • the lower pressure on the interior of the forward portion of the ejector shroud serves to draw in additional fluid flow that is further mixed with the high and low energy streams.
  • An increase in pressure occurs on the interior of the ejector shroud as the mixing flow moves from the leading edge to the trailing edge of the ejector shroud.
  • an increase in pressure occurs on the interior of the ejector shroud as the flow moves from the upstream end of the ejector shroud to the downstream end of the ejector shroud.
  • Airflow exiting the ejector shroud returns to ambient pressure.
  • the ejector shroud 120 has a ring airfoil shape and does not have mixing lobes. In some embodiments, mixing lobes may also be formed on the trailing edge 128 of the ejector shroud 120 .
  • a tangent line 171 is drawn along the interior surface at the trailing edge of the high energy mixing lobe 117 .
  • a rear plane 173 of the turbine shroud 110 is present.
  • the point where the tangent line 171 intersects the rear plane 173 is indicated here with reference numeral 172 .
  • a line 174 is formed at point 172 parallel to the central axis 105 .
  • An angle ⁇ 2 is formed by the intersection of tangent line 171 and line 174 . This angle ⁇ 2 is between 5 and 65 degrees.
  • a high energy mixing lobe 117 forms an angle ⁇ 2 between 5 and 65 degrees relative to a longitudinal axis that is parallel to the central axis 105 of the turbine.
  • the angle ⁇ 2 is from about 30° to about 50°.
  • a tangent line 176 is drawn along the interior surface at the trailing edge of the low energy mixing lobe 119 .
  • the point where the tangent line 176 intersects the rear plane 173 is indicated here with reference numeral 179 .
  • a line 175 is formed at point 179 parallel to the central axis 105 .
  • An angle ⁇ is formed by the intersection of tangent line 176 and line 175 . This angle ⁇ is between 5 and 65 degrees.
  • a low energy mixing lobe 119 forms an angle ⁇ between 5 and 65 degrees relative to a longitudinal axis that is parallel to the central axis 105 of the turbine. In particular embodiments, the angle ⁇ is from about 20° to about 45°.
  • Mixing lobes are present on the turbine shroud. As shown in FIG. 3 , the ejector shroud 120 has a ring airfoil shape and does not have mixing lobes. If desired, though, mixing lobes may also be formed on a trailing edge 128 of the ejector shroud.
  • the wind turbine 200 comprises a turbine shroud 210 that has a front end 212 and a rear end 214 .
  • High energy mixing lobes 217 and low energy mixing lobes 219 are present around the rear end 214 .
  • the ejector shroud 220 has an inlet end 222 and an exhaust end 224 .
  • Support members 206 connect the turbine shroud 210 to the ejector shroud 220 .
  • the turbine 200 further comprises, similarly, an impeller 240 , stator 242 , rotor 246 , and a nacelle body 250 .
  • a central passageway 252 extends through the nacelle body 250 .
  • the turbine shroud 210 has an axial length L M .
  • the ejector shroud 220 has an axial length L E2 .
  • the entire turbine itself has an axial length L T2 .
  • the turbine shroud 210 has a throat diameter D F .
  • This throat diameter D F is measured as the smallest diameter of the turbine shroud, and is generally located near the rotor 246 .
  • the rear end 214 of the turbine shroud has an inner diameter D RI and an outer diameter D RO .
  • the inner diameter D RI is measured as the diameter of a circle formed by the high energy mixing lobes 217 .
  • the outer diameter D RO is measured as the diameter of a circle formed by the low energy mixing lobes 219 .
  • the ejector shroud 220 also has a throat diameter D I .
  • This throat diameter D I is measured as the smallest diameter of the ejector shroud, and is generally located near the inlet end 222 .
  • the ejector shroud 220 also has an outer diameter D E at the exhaust end 224 . This outer diameter is measured as the diameter of a circle formed by the trailing edge 228 of the ejector shroud 220 .
  • L E2 and L T2 are used to indicate that the lengths of the ejector shroud 220 and the overall turbine 200 differ from the lengths L E and L T shown in the embodiment depicted in FIG. 1-5 .
  • the values for L M , D F , D RI , D RO , D I , and D E are the same for both the embodiments of FIG. 5 and FIG. 10 . This notation relates to FIG. 11 and FIG. 12 , as explained further below.
  • FIGS. 1-10 Comparative calculations were performed on the two embodiments depicted in FIGS. 1-10 .
  • FIG. 11 and FIG. 12 show and explain the results of the calculations.
  • FIG. 11 is a cross-sectional view comparing the first exemplary embodiment of FIG. 1 with the second exemplary embodiment of FIG. 9 .
  • the upper half is the embodiment shown in FIG. 1
  • the bottom half is the embodiment shown in FIG. 9 . This is indicated by the use of the different reference numerals to refer to the turbine shroud ( 110 , 220 ), the ejector shroud ( 120 , 220 ), and the nacelle body ( 150 , 250 ).
  • the throat diameter D F was kept constant between both embodiments, as was the ejector shroud outer diameter D E .
  • the axial length L M was also kept constant.
  • the length of overlap between the turbine shroud and the ejector shroud L ME was kept constant.
  • L E is greater than L E2 .
  • FIG. 12 is a graph showing power output versus the wind velocity for the two different turbines.
  • the power output is intended to show the relative amount of energy captured from the wind stream passing through the turbine shroud.
  • the relative values in this graph were generated by data gathered in a wind tunnel.
  • the first set of values (squares) were generated from a wind turbine having the relatively longer ejector shroud axial length L E .
  • the ratio of L E /D E was 0.32.
  • the second set of values were generated from a wind turbine having the relatively shorter ejector shroud axial length L E2 .
  • the ratio of L E2 /D E was 0.12. As seen in FIG. 12 , a shorter ejector shroud generated more power at the same wind velocity.
US12/983,066 2007-03-23 2010-12-31 Fluid turbine with ejector shroud Abandoned US20110135460A1 (en)

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US12/983,066 US20110135460A1 (en) 2007-03-23 2010-12-31 Fluid turbine with ejector shroud

Applications Claiming Priority (5)

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US91958807P 2007-03-23 2007-03-23
US12/054,050 US8021100B2 (en) 2007-03-23 2008-03-24 Wind turbine with mixers and ejectors
US33272210P 2010-05-07 2010-05-07
US41559210P 2010-11-19 2010-11-19
US12/983,066 US20110135460A1 (en) 2007-03-23 2010-12-31 Fluid turbine with ejector shroud

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US12/054,050 Continuation-In-Part US8021100B2 (en) 2007-03-23 2008-03-24 Wind turbine with mixers and ejectors

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WO2013155187A1 (fr) 2012-04-10 2013-10-17 Flodesign Wind Turbine Corp. Turbine à fluide carénée ayant des éléments d'excitation de couche limite
EP2994636A4 (fr) * 2013-05-09 2016-12-14 S C Topintel Consult S R L Turbine de type à éjecteur
CN107429656A (zh) * 2015-02-12 2017-12-01 液力能源公司 水电/水力涡轮机及其制造和使用方法

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