This invention relates generally to the electro-hydrodynamic wind energy conversion field, and more specifically to a new and useful system and method in the electro-hydrodynamic wind energy conversion field.
Electro-hydrodynamic (“EHD”) wind energy conversion is a process wherein electrical energy is extracted directly from wind energy. An EHD system is typically a solid-state device that uses wind energy to act against an electrostatic field, separating charged elements from a charged source. In concept, this system can convert wind kinetic energy to electrical potential energy in the form of charges collected at very high voltages.
Past investigations into this field, however, have been fraught with many problems that rendered the energy collection insufficient when compared to the energy input for operating the EHD system. In particular, as an EHD system collects charge from the separation of the charged particles, the system creates an electric field (also called a system field 120) that opposes the motion of the charges. The system field may cancel and even overwhelm the electric field used to charge the particles in the EHD system. As a result, the charge supplied to a charged element (e.g., droplets in a charged liquid spray) is reduced due to the interference of the system field with the charging field. This lowers the working current and power output of the entire system. Additionally, the charged particles that are emitted to the wind stream encounter a very large opposing electrostatic force (also called a space charge 122, shown in
The following description of the preferred embodiments of the invention is not intended to limit the invention to these preferred embodiments, but rather to enable any person skilled in the art to make and use this invention.
1. System for Field Shaping in EHD Applications
As shown in
The injector 200 of the preferred embodiment functions to impart charge on a particle and to introduce the charged particle 202 into the electric field. The charged particle is preferably suitable for entrainment within a fluid stream, more preferably a wind stream, such that energy may be harvested from the work done on the particle by the moving fluid. The particle is preferably a water droplet but may be any suitable particle as described below. The injector preferably injects charged particles into the field. The injector is preferably arranged substantially parallel to the gas stream, but may alternatively be oriented perpendicular to the gas stream (e.g. vertically, horizontally, etc.) at an angle to the gas stream, or in any suitable orientation. The injector 200 is preferably an electrospray injector, but may be a hydrostatic injector, a dry needle (e.g. that injects a substantially dry, charged particle into the wind), a corona charger, or any suitable injector. The injector 200 preferably includes an electrode 220 and a nozzle 240 as shown in
The electrodes 220 of the preferred embodiment function to maintain a high field concentration at a particle entrance (e.g., a nozzle tip or nozzle exit) to charge the particles. The particles are preferably water droplets that are inductively positively charged. The electrode 220 is preferably a rail electrode or a ring electrode (i.e., induction ring) made of conductive material. A ring electrode 220 preferably circumscribes the nozzle, and is preferably aligned with the ring axis concentric with the axis of the nozzle 240, with the planar position variable before, co-planar, or aft of the tip of the nozzle 240. The ring electrode 220 preferably maintains a higher field concentration at a point closer to the nozzle than to the electrode, wherein the high field concentration preferably has a rapid drop-off of field (volts/meter) heading radially outward towards the ring electrode from the central axis of the ring electrode. This preferably facilitates high field strengths for charging of particles (e.g., electrospray) without providing a current path for short-circuiting. Use of a large diameter (e.g., ⅛-¼ inch) cross-section wire or rod to form the ring electrode 220 preferably improves the shape of the electric field lines such that charging occurs, but short circuiting is reduced. The electrode 220 may additionally be aerodynamically shaped. For example, the cross section may have an airfoil shape. A large diameter ring electrode additionally preferably provides sufficient space between a nozzle and the electrode 220, creating a large area for wind to carry away charged particles. However, the electrode 220 may alternatively be any other suitable electrode (e.g. a plate electrode) and have any other suitable form factor.
The nozzle 240 of the preferred embodiment functions to produce particles to be charged and entrained within the wind stream. The nozzle preferably emits liquid droplets. The droplets are preferably water droplets but may alternatively be water plus additives (e.g. surfactant, cesium, etc.), a water solution, or any suitable alternative liquid. Alternatively, the nozzle may emit a substantially dry particle, such as a polymer or fertilizer. The nozzle preferably has a nozzle tip on the distal end of the nozzle 240 through which the particle is emitted. A pump system is preferably attached to the nozzle on the proximal end of the nozzle 240. A wide variety of nozzle types may be used due to the reduction in restrictions in spray/droplet requirements due to the field reversal from the electric field generator 300. The nozzle is preferably one of those disclosed in PCT application number PCT/US09/31682, but may alternatively be any suitable nozzle for particle emission and charging. As an alternative to the nozzle 240, air, particulate matter, or other non-liquid particles may alternatively be introduced for charging.
Additionally or alternatively, a preferred embodiment may have a plurality of injectors 200 within the field of the electric field generator 300. The injectors 200 are preferably arranged in an array, but may alternatively be arranged in one or more rows, columns, rings, or any other suitable configuration. The field of the electric field generator 300 is preferably useable by any suitable number of injectors. The array of injectors 200 are preferably aligned along a plane, preferably within the space within the electric field generator 300, but alternatively in a space upstream or downstream from the electric field generator 300. The number of injectors is preferably dependent on the properties of the electric field generator 300. In one example, 8-12 injectors are co-planarly arranged within the field of the electric field generator.
The electric field generator 300 (field shaper) of the preferred embodiment functions to manage the properties of the electric field (magnitude and direction) in the region substantially near the injector. More specifically, the electric field generator 300 functions to generate a shaping field 320 that reverses the system field 120 in a localized space near the injector. The net electric field at the tip of a nozzle 240 (or at another satisfactory portion of the injector 200) is preferably held at the maximum electric potential of the charging field (e.g. significantly positive or negative). The magnitude of the net electric field preferably precipitously drops from this maximum at the tip of the nozzle 240 to zero at a point downstream from the injector (zero field point 322). This zero field point is preferably 5 to 10 millimeters displaced from the tip of the nozzle 240 in the direction of the wind stream. The zero field point may alternatively be displaced a greater length, such as 20-50 millimeters or any suitable distance. Thus, the net electric field preferably transitions from a charging field at the nozzle tip to pulling the particles at a point downstream from the injector 200. This functions to prevent shorting of the particles. Beyond the zero field point, the net electric field then preferably opposes particle motion along the Z-axis (i.e., in the direction of the wind stream). Energy can then be harvested from the wind stream overcoming the opposing electric field force on the charged particle. The net electric field at the zero field point 322 is preferably approximately zero, but may alternatively be slightly negative or slightly positive. The electric field generator 300 (also known as a field shield or field shaper) is preferably a conductive element (e.g. a guard electrode) charged to create an electrostatic field with constant shape during normal operating conditions. However, the electric field generator 300 may be an electromagnetic generator, such as a magnetic element (e.g. permanent magnet or electromagnet), or any suitable electric field generator. Additionally/alternatively, the generated electric fields may be dynamic and time-variable instead of static. The electric field generator may be positioned substantially co-planar, downwind, or upwind relative to the injector 200.
In a first embodiment, as shown in
The system of the first embodiment may additionally include at least one field leveler 342 that functions to homogenize (i.e., normalize or make uniform) the field of the electric field generator. The field leveler 342 is preferably a conductive component that augments the field of the electric field generator 340. The field leveler 342 is preferably used in combination with an array of injectors 200. For example, a field leveler 342 is preferably positioned within the center of the space defined by the electric field generator 340 as shown in
In a second embodiment, as shown in
Additionally, the electric field generator 300 may be adapted to alter one or more properties of the fluid stream. More preferably, the electric field generator 300 is adapted to have aerodynamic and/or lift-generating properties that focus the wind stream to enhance charged particle radial expansion to further dissipate the space charge. Wind from a wider area, preferably upstream from the injector 200, may be funneled through the electric field generator 300. The electric field generator is preferably formed as an airfoil, but may alternatively be formed as a convergent-divergent nozzle (as shown in
The electric field generator 300 may be made of modular components such that an electric field generator can be easily constructed. A modular design could even be designed for connecting an array of electric field generators. The electric field generator 300 preferably is rounded or has rounded edges. Sharp edged hardware such as nuts and fasteners are preferably protected, and common corona reduction practices are preferably followed. The electric field generator may alternatively come in any suitable shape or form. The electric field generator is preferably electrically insulated to prevent shorting, and is preferably encapsulated by a solid dielectric material, but may alternatively be encapsulated by a liquid dielectric material, glass, ceramic, or a composite polymer.
The electric field generator 300 is preferably powered to generate the electrostatic field of the electric field generator 300. With the addition of the electric field generator, the electrodes 220 of the injector 200 can preferably be operated at a lower voltage, which functions to increase efficiency. Lowering the voltage even further below that of the electrode(s) 220 may further lower the induction charging voltage and enhance the efficiency of the system. Additionally, the electric field generator 300 may be charged by a power source separate from the ring electrode(s) 220. With a separate power supply, the electric field generator 300 preferably draws power during startup and preferably maintains the field with no or little power loss since there is preferably no current flowing in the circuit of the electric field generator 300. This is comparable to charging a capacitor and holding the voltage constant. Small amounts of positive entrained charge may short back to the electric field generator 300. The aerodynamic design of the electric field generator may reduce such occurrences.
In a first preferred embodiment, as shown in
In a second preferred embodiment, the system includes substantially the same components as the first embodiment, except that the electric field generator includes a plurality of shielding and attracting electrode pairs 360, located downstream from the injector, in addition to the circumscribing inductive electrode. The electrode pairs are encapsulated within an airfoil made of dielectric material. Each shielding electrode is held at substantially the same low positive potential, and each attracting electrode at substantially the same high negative potential (relative to the shielding electrodes). The magnitudes of the electric fields created between the shielding electrode and the attracting electrode (shaping field) are preferably substantially smaller than the magnitude of the system field. The shielding and attracting electrode pairs 360 are positioned within the system field (downstream from the injector), substantially near the injector, with the shielding electrode aligned proximal the injector and the attracting electrode distal the injector. Each shielding and attracting electrode pair is substantially aligned along the gas stream, and moves as the gas stream changes direction.
In a third preferred embodiment, the system includes substantially the same components as the second embodiment, except that the electric field generator only includes the plurality of shielding and attracting electrode pairs 360, and does not include a circumscribing inductive electrode.
As a person skilled in the art will recognize from the previous detailed description and from the figures and claims, modifications and changes can be made to the preferred embodiments of the invention without departing from the scope of this invention defined in the following claims.
This application claims the benefit of U.S. Provisional Application No. 61/394,298, filed 18 Oct. 2010, titled “A System And Method For Controlling Electric Fields In Electro-Hydrodynamic Applications” and U.S. Provisional Application No. 61/528,440 filed 29 Aug. 2011, titled “A System And Method For Controlling Electric Fields In Electro-Hydrodynamic Applications,” which are incorporated in their entirety by this reference. This application is related to prior application Ser. No. 12/357,862, filed 22 Jan. 2009, titled “Electro-Hydrodynamic Wind Energy System” and prior PCT application number PCT/US09/31682, filed 22 Jan. 2009, titled “Electro-Hydrodynamic Wind Energy System” which are incorporated in their entirety by this reference.
This invention was made with government support under HR0011-09-C-0144 awarded by the Department of Defense/Defense Advanced Research Projects Agency. The government has certain rights in the invention.
Number | Name | Date | Kind |
---|---|---|---|
414943 | Dewey | Nov 1889 | A |
911260 | Pennock | Feb 1909 | A |
1014719 | Pennock | Jan 1912 | A |
2638555 | Marks | May 1953 | A |
3121196 | Kasemir | Feb 1964 | A |
3138919 | Deutsch | Jun 1964 | A |
3191077 | Marks et al. | Jun 1965 | A |
3309546 | Boll | Mar 1967 | A |
3411025 | Marks | Nov 1968 | A |
3489669 | Ruhnke | Jan 1970 | A |
3518461 | Marks | Jun 1970 | A |
3792293 | Marks | Feb 1974 | A |
3960505 | Marks | Jun 1976 | A |
4073516 | Kling | Feb 1978 | A |
4146371 | Melcher et al. | Mar 1979 | A |
4146800 | Gregory et al. | Mar 1979 | A |
4204844 | Pilat | May 1980 | A |
4206396 | Marks | Jun 1980 | A |
4271357 | Bradshaw et al. | Jun 1981 | A |
4328436 | Biblarz et al. | May 1982 | A |
4395648 | Marks | Jul 1983 | A |
4417293 | Larigaldie | Nov 1983 | A |
4433248 | Marks | Feb 1984 | A |
4450364 | Benoit | May 1984 | A |
4486669 | Pugh | Dec 1984 | A |
4523112 | Marks | Jun 1985 | A |
4581675 | Kelly | Apr 1986 | A |
4667100 | Lagna | May 1987 | A |
5047892 | Sakata et al. | Sep 1991 | A |
5125230 | Leonard | Jun 1992 | A |
5214386 | Singer et al. | May 1993 | A |
5273838 | Draper et al. | Dec 1993 | A |
5912396 | Wong | Jun 1999 | A |
6254034 | Carpenter | Jul 2001 | B1 |
6302331 | Dvorsky et al. | Oct 2001 | B1 |
6440600 | Starzak | Aug 2002 | B1 |
6452499 | Runge et al. | Sep 2002 | B1 |
6462337 | Li et al. | Oct 2002 | B1 |
6504702 | Noll | Jan 2003 | B1 |
6544484 | Kaufman et al. | Apr 2003 | B1 |
7405672 | Taylor et al. | Jul 2008 | B2 |
7478712 | Mccowen | Jan 2009 | B2 |
7855476 | Ogram | Dec 2010 | B2 |
8102082 | Ogram | Jan 2012 | B2 |
8283811 | Ogram | Oct 2012 | B2 |
20020060631 | Runge et al. | May 2002 | A1 |
20020153006 | Zimlich et al. | Oct 2002 | A1 |
20030218855 | Goldenberg | Nov 2003 | A1 |
20040089156 | Gartstein et al. | May 2004 | A1 |
20040129931 | Asryan et al. | Jul 2004 | A1 |
20040134997 | Khain et al. | Jul 2004 | A1 |
20040164241 | Farnsworth et al. | Aug 2004 | A1 |
20040179322 | Pletcher et al. | Sep 2004 | A1 |
20060061107 | Cadaret | Mar 2006 | A1 |
20070114381 | Jackson | May 2007 | A1 |
20070216316 | Hirano et al. | Sep 2007 | A1 |
20080063577 | Crowe et al. | Mar 2008 | A1 |
20080073530 | Jolliffe et al. | Mar 2008 | A1 |
20080199195 | Swift et al. | Aug 2008 | A1 |
20080308095 | Trees et al. | Dec 2008 | A1 |
20080309087 | Evulet et al. | Dec 2008 | A1 |
20090218910 | Carmein et al. | Sep 2009 | A1 |
20090314850 | Kampmeyer | Dec 2009 | A1 |
20100018850 | Adhvaryu et al. | Jan 2010 | A1 |
20100127624 | Roy | May 2010 | A1 |
20100156444 | Ponjee et al. | Jun 2010 | A1 |
20110050080 | Suzuki et al. | Mar 2011 | A1 |
20120000627 | Jewell-Larsen et al. | Jan 2012 | A1 |
20120304637 | Allen et al. | Dec 2012 | A1 |
20130008315 | White et al. | Jan 2013 | A1 |
20130015257 | Kalra et al. | Jan 2013 | A1 |
20130285379 | Seeley et al. | Oct 2013 | A1 |
20130313942 | White et al. | Nov 2013 | A1 |
Number | Date | Country |
---|---|---|
639000 | Nov 1936 | DE |
19629417 | Feb 1998 | DE |
10360876 | Sep 2005 | DE |
0909232 | Jul 2009 | GB |
2009094441 | Jul 2009 | WO |
2010127178 | Nov 2010 | WO |
Entry |
---|
D. Djairam “The Electrostatic Wind Energy Converter, Electrical Performance of a High Voltage Prototype”, pp. 1-173. Doctoral Dissertation, Dec. 10, 2008. http:/ /repository.tudelft.nl/view/ir/uuid:e1cfdada-85ea-45c4-b6e4-b798abf5917 e/. |
D. Djairam et al. “The Development of an Electrostatic Wind Energy Converter (EWICON)” 2005 International Conference on Future Power Systems High Voltage Technol. & Manage. Group, Delft Univ. of Technol. Dec. 2005; DOI: 10.1109/FPS.2005.204208 ISBN: 90-78205-02-4. |
Number | Date | Country | |
---|---|---|---|
20120211989 A1 | Aug 2012 | US |
Number | Date | Country | |
---|---|---|---|
61528440 | Aug 2011 | US | |
61394298 | Oct 2010 | US |