US20170204839A1 - Apparatus for Generating Energy from a Fluid Flow Induced Movement of a Contacting Surface Structure Relative to an Opening to a Cavity in a Frame - Google Patents

Abstract

A generator moving through a medium has a contacting surface structure relative to a frame with a spring coupled between the two. The contacting surface structure also has an electrogenerative portion coupled to the contacting surface structure and the frame, such as a piezoelectric or electromagnetic structure, although other types of structures are known within the art. The movement of the frame through the medium exerts forces upon the contacting surface structure which causes contacting surface structure movement relative to the base structure through the electrogenerative portion. The spring provides a force upon the contacting surface structure in response to the force from the fluid flow.

Description

CROSS-REFERENCE TO RELATED APPLICATIONS
• This application claims the benefit of Provisional Application No. 61/508,694, filed Jul. 18, 2011, in the United States Patent and Trademark Office, and is a divisional of application Ser. No. 13/551,593 filed Jul. 17, 2012.
BACKGROUND
• 1. Field of the Invention
• The preferred embodiments of the invention are directed to the field of power generation.
• 2. Description of the Related Art
• Generators harnessing energy from a fluid flow (such as air) are known within the art, however such generators typically have turbines or propellers which have a large cross-section. The movement of the medium creates a motive force upon the turbine or propeller, which is connected to a device to convert the movement into electricity. But the large cross-sections of these traditional designs increase the amount of wind resistance presented by the generators, limiting the practicality of their application in certain fields.
• For example, the prior art describes a vehicle having a wind tunnel and turbine generator, but the aerodynamic limitations of the turbine are not ideal for vehicular applications. Those disclosures created wind resistances which would substantially decrease fuel efficiency. The energy would also be capped at a theoretical 60% recovery, further impacting the efficiency relative to the burden on the system from the design. Other generator designs have been developed to try to minimize the aerodynamic cost of the generators. For example, designs have sought to take advantage of the aeroelastic or flutter effect in aerodynamics by placing structures into the middle of a fluid flow. These designs have previously suggested using wings that move about one or two points or elastic membranes that are fixed at two ends. These designs cross the fluid flow, creating oscillations perpendicular to the fluid flow in the wing or membrane. The designs introduce drag and a blocking obstacle in the fluid flow and require supporting structures which greatly affect the cross-sectional aerodynamics. They also require a fixed direction of fluid flow that is perpendicular to the orientation of the long axis of the wing or membrane. The prior art describes one such design utilizing a string membrane pulled taut across two rigid structures. Similarly, the prior art describes wing generators have been presented which mount a wing across two support pillars to generate electricity from the pitch and yaw motion of the wing.
• Kite generators have also been presented which transfer kite movement to a fixed base structure through a tether. These kites are typically flown at higher altitudes to harness the stronger wind forces. Similarly, there is currently interest in developing tethered autonomous flight vehicles with generators that are flown at high altitude to take advantage of the greater wind forces at altitude.
• Prior devices typically required large structures and/or large motive forces, which often mean that the devices could only be operated under certain conditions or in certain locations. These devices also typically have many moving parts, which increase the need for maintenance and the potential for breakdown. These devices also face increased stresses as motive forces increased, requiring designs or use that compensated for high speed or shut down to avoid damage. Furthermore, the output from these devices varies substantially with the relative velocity of the medium, often requiring the design to compensate for velocities outside of a tolerance range.
• These devices also often times require a fixed direction of flow. In order to compensate for varying directions of flow, previous devices have been rotatable with guiding panels to orient the device in the correct direction relative to the direction of flow.
• Each of these designs presents its own complications and complexities, at least some of which can be alleviated by an embodiment of the present invention. For example, the aerodynamic cost from the cross-sectional shapes of many of these designs is too high for certain applications, such as in vehicular applications. Additionally, the mechanical complexities of some of the devices have been a noted concern, resulting in high cost, difficult maintenance, and overall complicated manufacturing. Other designs are unidirectional and not able to be accommodating of changing directions of fluid flow without additional rotational structures. Some of the designs are also dependent on the speed of fluid flow, with limited efficiency or effectiveness outside of a narrower range of preferred flow speeds. Some designs may even break down at excessive speeds, as has been shown in test flights of generators at altitude.
• There is a need for a device that can generate electricity from relatively lower levels of motive force and provide smaller cross-sections. There is also a need for scalable, stackable devices to generate electricity in locations where traditional devices are not suitable. The increased use of electric and hybrid engine systems in vehicles has also created an increased need for ways of generating electricity to recharge batteries.
• Also, given a stated desire to design turbine generators that operate at altitude under strong winds and via cables or tall supporting structures, there is a need for a device which minimizes aerodynamic complications associated with turbines and other non-aerodynamic shapes so as to more easily maintain operational altitude and minimize complications from stronger wind speeds.
SUMMARY OF THE INVENTION
• It is therefore an object of an embodiment of the present invention to provide a generator that utilizes relative movements of a particular medium to generate electricity. The generator harnesses the energy of surface structure movements influenced at least by forces due to the flow of fluid of the medium. The energy is converted to electricity via an electrogenerative portion.
• It is also an object of an embodiment of the present invention to provide a generator that operates more independently of the direction of movement of a particular medium. It is also an object of an embodiment of the present invention to provide a generator that is less susceptible to large motive forces and more structurally robust under such extreme circumstances. It is another object of an embodiment of the present invention to provide a generator design more capable of accommodating a number of varied flow speeds. It is another object of an embodiment of the present invention to provide a generator design that is reduced is size, complexity, and cost.
• It is also an object of an embodiment of the present invention to provide a generator with a small form-factor. It is also an object of an embodiment of the present invention to provide an electric generator that utilizes wind power with a relatively limited cross-section. It is also an object of an embodiment of the present invention to provide an electric generator that does not significantly increase drag or alter the aerodynamics and/or wind resistance of the base structure. It is also an object of an embodiment of the present invention to provide a generator which is modular, stackable in series and/or parallel, and scalable, providing multiples of combinations depending on available space and power requirements.
• It is another object of an embodiment of the present invention to provide a generator design that can be incorporated with a number of varied applications, including for example, vehicular movement such as automobiles, rail, marine, and aviation.
BRIEF DESCRIPTION OF DRAWINGS
• In the drawings, wherein like reference numerals denote similar elements throughout the figures:
• FIG. 1adepicts an example of a cell for implementing an embodiment of the present invention with a coil in which a magnet is only secured on one end.
• FIG. 1bdepicts another example of a cell for implementing an embodiment of the present invention with a coil in which a magnet is secured on two ends.
• FIG. 1cdepicts another example of a cell for implementing an embodiment of the present invention in which two coils are located within the same cavity.
• FIG. 1ddepicts another example of a cell for implementing an embodiment of the present invention with a coil in which a magnet is positioned so that the coil is on the cover instead of the substrate.
• FIG. 1edepicts an example of a coil placed on the cover.
• FIG. 1fdepicts another example of a cell for implementing an embodiment of the present invention with a film material in or on the cover made of piezoelectric materials.
• FIG. 1gdepicts the cross section of a wing structure for implementing an embodiment of the present invention with a leading edge and a flexible surface.
• FIG. 1hdepicts a coupled structure where the two paired surface structures are placed and joined opposite one another by a connecting rod.
• FIG. 1idepicts a coupled structure where the two paired surface structures are placed and joined adjacent one another.
• FIG. 1jdepicts placement of cells on a base structure having oscillating protrusions on the leading edge.
• FIG. 1kdepicts a coupled structure where the curved surface structure is rigid so as to join the two opposite curved surfaces around the pivot point.
• FIG. 2adepicts a block diagram of various components for implementing an embodiment of the present invention where the cells are connected to individual multiplier/rectifier circuits.
• FIG. 2bdepicts a block diagram of various components for implementing an embodiment of the present invention where the cells are connected to a single multiplier/rectifier circuit.
• FIG. 3adepicts an example of an array of cells for implementing an embodiment of the present invention where the array is located along a bottom surface of a structure.
• FIG. 3bdepicts an example of an array of cells for implementing an embodiment of the present invention where the array is located along a top surface of a structure.
• FIG. 3cdepicts an example of an array of cells for implementing an embodiment of the present invention where the array is located along both the top and bottom surfaces of a structure.
• FIG. 4 depicts an example of a wing structure for implementing an embodiment of the present invention where the structure contains cavities and a thin, rigid plate extending partially over the opening to each cavity.
• FIG. 5 depicts an example of a wing structure for implementing an embodiment of the present invention where the structure contains a large, shared cavity and thin, rigid plates extending partially over the opening or openings to the cavity.
• FIG. 6 depicts an example of a design for a tear shaped covering as part of an embodiment of the present invention.
• FIG. 7adepicts an example of a pipe structure for implementing an embodiment of the present invention with fluid flow in pipes where the pipe structure shares a cavity across each opening.
• FIG. 7bdepicts an example of a pipe structure for implementing an embodiment of the present invention with fluid flow in pipes where the pipe structure has a separate cavity for each opening.
• FIG. 8 depicts an example of a tube structure with cells distributed along the surface of the tube where the tube may be internally pressurized if desired.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
• Some embodiments of the invention are described below in further detail with respect to the Figures.
• According to an aspect of an embodiment of the invention, a generator has a surface structure or contacting portion relative to a base structure or frame and is positionable within a field of flow. Preferably, the surface structure is connected to the base structure along the leading edge of the surface structure relative to the direction of flow such that the field of flow is directed substantially over the surface structure. The surface structure can be shaped in a number of ways when taking into account aerodynamics, including curvilinear, faceted, and angular shapes. Many structural shapes are known within the art and can be incorporated here to provide a desired level of aerodynamics for the particular application, such as aerofoils, wing shapes, spoilers, riblets, curved leading edges, etc. The surface structure design also helps to generate a motive force from the field of flow, depending on the orientation of the surface structure and/or the angle of the surface structure relative to the field of flow.
• In another aspect of an embodiment of the invention, the generator has an electrogenerative portion or energy converting portion positioned relative to the surface structure and the base structure. The electrogenerative portion is preferably a piezoelectric or an electromagnetic structure, although other types of structures are known within the art. The field of flow exerts forces upon the surface structure which causes surface structure movement relative to the base structure and generates electricity through the electrogenerative portion. The electricity generated can be directed to one or more systems requiring electrical input. The electricity generated can also be directed to a charging circuit for a storage device (such as a battery or capacitor) for later use. Circuits for rectifying, multiplying and otherwise modifying the energy output of the generator can also be employed to match the requirements of the load(s).
• In another aspect of an embodiment of the invention, the system can be designed so as to present counteracting forces from a biasing member apart from the forces from the field of flow. For example, springs or elastics can be used to add forces present when the system is outside a field of flow. If the generator is designed to have an enclosed area from the field of flow, then the relative pressure differential from the field of flow and within the enclosed area will also contribute additional forces. If the generator is designed to have a pairing of surface structures where movement of one surface structure induces movement in the other surface structure, then the movement forces of the first surface structure can be viewed also as an additional force for the second surface structure. Depending on the orientation of the surface structure, gravity may also contribute an additional force on the system. And depending on the position of the surface structure in the field of flow, these additional forces will aide and/or oppose the forces from the field of flow.
• The forces present on the surface structure act like an impulse or input force on the generator, which can be viewed as an oscillating spring system. Continued flow contributes energy to the oscillating spring system, generating a prolonged oscillation pattern as the system seeks to return to equilibrium. By design, the generator system can preferably be built to have damping characteristics that are modeled as critically damped or even underdamped, resulting in oscillations that do not decay so long as the system continues to have input energy. The oscillating motion directs the motive energy in the surface structure to the electrogenerative portion which converts it to electrical energy.
• Referring toFIGS. 1a, 1b, and 1cagenerator cell200 has a covering202 over acavity400 having an initial pressure. This initial pressure is preferably at or around the pressure of the surrounding medium when the surrounding medium is static.Cavity400 is preferably sealed to be airtight or watertight. In such arrangements,cavity400 can be pressurized to bias the initial force on covering202. When the surrounding medium is moving relative to the enclosed medium within the cavity, a pressure difference is created across the covering202. This pressure difference will exert force upon covering202 as the medium attempts to equilibrate the difference. The elasticity of the overall system creates oscillations from this change to the steady state pressures. System elasticity can be achieved from at least the following sources: the cover, a spring, the internal medium, the connective portion between the substrate and the cover.
• In other embodiments,cavity400 can be partially enclosed but not sealed. For example,cavity400 may have one or more additional uncovered openings in the enclosure so long as the pressure incavity400 is relatively different than that resulting from movement in the medium on the outside of thecover202. For example, this relationship can be maintained by having a long separation between the medium immediately on either sides of covering202 where the separation extends in the direction of the flow of the surrounding medium. In another embodiment of the present invention,cavity400 could have an opening to the enclosure facing the direction of flow of the medium where the enclosure is shaped to alter the pressure inside the enclosure and under covering202 relative to the surrounding medium outside covering202. For example, the enclosure could be shaped to have a relatively large opening that tapers to a smaller opening or vis a versa. Each enclosure shape would alter the pressure withincavity400 and under covering202, relative to the surrounding medium. In a preferred embodiment of the present invention,cavity400 would have an enclosure that does not have an opening facing the direction of flow of the medium.
• Covering202 is preferably flexible or elastic and made of materials that are expandable in surface area. The pressure difference across covering202 that results from relative movement of the surrounding medium would create a force on covering202 and induce movement. The combination of elastic forces in the covering, reactionary forces from pressure changes under covering202, applied forces from the surrounding medium onto changes in the shape of covering202, and/or any additional spring devices in the embodiments as described below, create counter-movement. The combination of forces can be tuned and balanced so as to generate resonance in thecovering202.
• An example material for covering202 could be rubber. Covering202 could also comprise multiple parts, optionally made of different materials or having different characteristics such as different rigidity, weight, or thickness. For example, inFIG. 1a, covering202 is shown having twoparts203 andpart201.Part203 can be made of a relatively rigid material to whichmagnet300 is mounted. For example, a styrofoam material preferably can be used as therigid structure203, providing light weight but rigid material. Plastics could also be used to formstructure203.Part201 can be made of a relatively flexible material, preferably extending fromPart203 to cover the uncovered remainder ofcavity400. In a preferred embodiment of the present invention, the covering202 has a relativelyrigid part203 with riblets to reduce drag. The relativelyrigid part203 can be angled in the neutral state of the cell such that downwards pressure is generated at the onset from the moving medium. In a preferred embodiment, the riblets can be spaced at around twice the height of the riblets in order to further decrease drag. Alternatively, the spacing of the riblets and their height can be designed so as to create a cross-section in the surface that optimizes the reduction in drag. Various shapes of riblets, along with their size and spacings have been studied within the art for years.
• In another embodiment of the present invention, the covering202 has riblets spaced along a relatively flexible surface. The riblets can be relatively rigid by comparison, a characteristic that can be achieved for example by having a certain thickness to the riblet which relatively reduces stretching or forming the riblets out of a different material. As the covering202 expands, the spacing between the riblets changes. In a preferred embodiment, at about an expected pressure differential between the interior of the cell and the outside medium which is moving relatively at an expected speed, the riblets will be spaced at a distance different from the neutral state because the covering has expanded or stretched. The particular spacing can be designed in accordance to the height of the riblet to be twice the riblet height, or alternatively to take into consideration the cross-sections formed by the spacing and the riblet height. Preferably, this increased spacing will decrease relatively the amount of drag of the covering as a result of the bulging of the cover. The height of the riblets preferably remains substantially the same throughout the stretching range of the covering202, although the riblets can be designed to also flatten out during stretching if the design parameters contemplate it.
• In another embodiment, as shown inFIG. 1j, thecells200 are positioned along asurface100 at intervals corresponding to thepeaks102 orvalleys103 of an oscillating edge shape. The benefits of such an oscillating edge shape are disclosed in U.S. Pat. No. 6,431,498. The oscillating edge shape provides leadingprotrusions102 which act to separate fluid flow into streams along the direction of the valleys, reducing drag. Preferably, thecells200 are aligned along thevalleys103 to take advantage of the separated fluid streams. In another preferred embodiment, thecells200 can be positioned after the leading edge but still within thephysical valleys103. In another embodiment, the cells can be incorporated into theprotrusions102 themselves, such as a design where the surface structure is positioned in a c-shape across the top105 andbottom104 of the leading edge with a pivot around the leading point of theprotrusion102. A similar cross-sectional view of one such protrusion can be seen inFIG. 1kwhere, in one embodiment, the protrusion comprises acurved structure207 pivoting along theoutermost point210. In a fluid flow, thecurved surface structure207 oscillates along thepivot point210 to alternately increase and decrease the relative height of the protruding structure along the length of the protrusions inFIG. 1j,104 and105. Thecurved structure207 can also be connected to thebase structure100 via a flexible cover extending from the end point of thecurved structure208 to a location along thebase structure surface100.
• InFIGS. 1a, 1b, 1cand 1d, movements inmagnet300 provide a changing magnetic field to acoil500, inducing an electric current. First, when the surroundingmedium401 has a pressure difference relative to the initial pressure in the cavity, the covering202 flexes to try to equalize the pressure difference. The equalization may also overshoot, causing a differential in the other direction. Second, in some embodiments when the surrounding medium401 changes pressure due to relative movement, the velocity also provides a force on the covering202 when part of the covering202 flexes into the surrounding medium. This force will in turn relatively increase the pressure within thecavity400. In other embodiments, the covering202 may not flex above the surface of thesubstrate100, so the movement would be attributable to the relative changes in pressure both outside and inside thecavity400. Additionally, the material used in covering202 may provide elasticity which would provide forces to return themagnet300 to the initial position. InFIG. 1b, a spring600 (or other elastic retaining mechanism) can also be attached between the magnet and thecoil500 or thestructure100. Thisspring600 provides additional force on themagnet300, and can be designed so that themagnet300 is pushed out, pulled in, or neutrally positioned in the initial state of thegenerator cell200. Other connective devices other thansprings600 can be used to provide tension or recoil, such as an elastic structure.
• Cell200 can be designed to includemultiple magnets300 and coils500 within thesame cavity400. Such an arrangement would function similarly toFIGS. 1aand 1b, but provide added output for the same displacement forces. One such possible arrangement is depicted inFIG. 1c, showing twomagnets300 and twocoils500 within thesame cavity400. Themagnets300 also have twosprings600 connecting them to thestructure100. In another embodiment,FIG. 1ccan be implemented with only onemagnet300 oncover202. Two ormore coils500 are grouped with themagnet300 such that movement by thesingle magnet300 generates electricity in the plurality of thecoils500. Preferably, thesingle magnet300 is sufficiently large in size so as to cover the combined cross-section of the group ofcoils500.
• Coil500 can be wound in a number of different ways which are well known, such as a bifilar coil, a Barker coil, a flat coil, a planar spiral coil, a Helmholtz coil, a Maxwell coil, or a Tesla coil. One such example is provided inFIG. 1e. Themagnet300 is moved relative to thecoil500 by a number of factors. Thecoil500 and themagnet300 can also be interchangeably positioned, as shown inFIG. 1dwhere the coils are fixed to thecover202 as opposed to thesubstrate100. In another embodiment of the present invention,multiple coils500 can be fixed to thesame cover202.Coil500 inFIGS. 1a-1dcan also be designed so as to decrease the vertical space required forcell200, such as with a flat coil or a planar spiral coil. Various coil designs will provide different tradeoffs between the amount of power generated, manufacturing cost, and coil size, and the particular selections will depend on the requirements of the application or preferences of the designer. In another embodiment of the present invention, a plurality ofcoils500 is arranged within eachcell200 where the plurality ofcoils500 contains two or more different coil designs. Preferably, the different coil designs are chosen to complement one another.
• InFIG. 1f, covering202 is shown having at least twoparts204 and205 wherepart204 contains a piezoelectric material or film andpart205 does not. In another preferred embodiment,parts204 straddle the edge ofcell200 so that movement in covering202 results in a bending ofparts204, along with the piezoelectric material. In an alternative embodiment, the piezoelectric material or film could be throughout covering202 such that covering202 consists of only one part. In an alternative embodiment, the piezoelectric material or film could be layered on top of apart204 of covering202 or the entirety of covering202. In addition to piezoelectric materials, generators using nanowires as known in the state of the art can also be used to generate electricity when the nanowires are flexed. Another alternative embodiment utilizes a piezoelectric skin as known in the state of the art which has a particularly optimized design to efficiently generate electricity from vibrations. It will be obvious to persons of ordinary skill in the art to use similar types of electrogenerative films in place of a piezoelectric material. Movement in covering202 would directly result in bending of thepiezoelectric material204 or film in covering202.
• By spacing the generator cells at particular intervals and designing them to have a particular depth or departure from the smooth surface state, drag can even be reduced by the alternating structure resulting from movement. Alternatively, the neutral state of the coverings for each cell can be designed such that they sag inward. By spacing the cells, a dimple effect like with a golf ball can be created. Dimple effects are well known to persons of ordinary skill in the art.
• In another embodiment, multiple surface structures can be grouped together so that a force on one structure results in forces on the other structures. InFIG. 1h, this is depicted where thesurface structures203 are paired with another surface structure233 opposite the overall shape of the generator housing orsubstrate100. Similarly inFIG. 1k, the two halves of acurved surface structure207 are positioned opposite each other relative to a field of flow. The pairing can be accomplished through rigidity in the material joining the twosurface structures207 along a pivot point or pivotaxis210, or can be accomplished through a physical connector such as arod206. In a preferred embodiment, as one surface structure is displaced in one direction, the other surface structure is displaced in the opposite direction. Thus, forces from a field of flow which depress one surface structure will elevate the other surface structure, resulting in a greater depressing force on the latter surface structure. This same relationship can also be accomplished withsurface structures212 in twogenerator cells200 that are adjacent to one another by having a connecting joint211 which pivots between the two surface structures about a pivot point oraxis210, as shown inFIG. 1i. As joint211 rotates aboutpoint210, the pairedsurface structures212 will alternately be elevated or depressed. Joint211 can be joined tostructures212 via a rotational coupling, sliding contact, or an elastic or flexible connection. In another embodiment, the remaining covering over thecells200 can also be elastic to maintain contact as desired between joint211 andstructures212.
• Referring toFIGS. 2aand 2b, various embodiments are provided for connecting one ormore cells200 to one or more multiplier/rectifier circuits700. The multiplier/rectifier circuit700 can be connected to one ormore cells200. Thecells200 may also be connected in series or in parallel or both, depending on the desired type and magnitude of output. In a preferred embodiment of the invention, a grouping of cells is connected in series and groups of cells are then connected in parallel in order to increase the output voltage and maintain a minimum level of power output.
• Various voltage multiplication or rectification circuits known in the industry can be implemented as the voltage multiplier/rectifier blocks700 inFIGS. 2aand 2b. These types of circuitry can convert AC to DC and/or shift the output to reduce negative voltages. Some known circuit designs include Greinacher voltage multiplier circuitry, Villard voltage multiplier circuitry, Cockcroft-Walton voltage multiplier circuitry, and fullwave rectifier circuitry. While these are circuit designs provided in the present embodiments, any other type of voltage multiplier or voltage rectifier can be used to accomplish the same purpose of rectification or voltage shifting. The particular design selected will vary depending on the cost restrictions and the requirements of the application. For example, some applications may be designed to provide rectified outputs that have a small ripple. Other applications may tolerate significant variability in the output or even a sinusoidal AC type output.
• For the multiplier/rectifier circuits700 used, various types of diodes may also be selected for the circuitry, depending on cost and performance requirements. Certain diodes may provide larger reverse bias voltages or relatively reduce the voltage consumption of circuitry. In a preferred embodiment of the invention, Schottky diodes are utilized in the multiplier/rectifier circuit700 in order to minimize the required forward voltage bias of the diode relative to other design options.
• The outputs from the multiplier/rectifier circuits700 can be directed to charging circuitry of various designs known within the art. Some examples of known charging circuits include constant voltage, constant current, taper current, pulsed charge, burp charge, IUI charge, float charge, or trickle charge circuitry. These various designs are known within the art and the particular selection depends on the needs of the system being designed, as well as cost and the amount of electricity generated. Some designs may also be constrained by the type of storage device for the system. For example, the storage device can be a lithium-ion, lead acid, NiMH, or nickel-cadmium battery, each of which may preferably be incorporated with particular charging circuits. Also, the storage device could be a supercapacitor, which is known within the art as an alternative to batteries. Alternatively, the outputs can be directly fed into electronic circuitry utilizing the generated power. In one preferred embodiment of the invention, the output is connected to lithium-ion batteries or supercapacitors already used in vehicles as a power source. In another embodiment of the present invention, the multiplier/amplifier circuit may be incorporated into the charging circuit.
• FIG. 4 depicts an embodiment of the present invention in an aerofoil shape. Thecell cavities400 may be formed as cylinders although any shape can be utilized. The particular selection can be designed according to the anticipated pressure differential across the covering of thecell200. For example, to achieve a certain neutral air pressure within thecell200, the volume of thecavity400 must be taken into account along with the elasticity or rigidity of the covering. At atmospheric pressure, this will be less important. But for a pressure biased cell, whether negative or positive relative to atmospheric pressure, the cell contents will exert a force on the covering, displacing it by an amount relative to the elasticity forces. The covering will achieve an equilibrium state where the pressure force within thecavity400 is balanced by the force from the covering resisting further deformation. The cell can also be filled with a gas or liquid having a different density than air. This will change the compressibility of the contents of the cell, changing the amount of deflection of the cover and the forces needed to move the covering.
• In another embodiment, the covering can also be designed so that arigid plate203 as shown inFIG. 4 is incorporated into the covering. The rigid plate can be formed in connection with the substrate so as to be elastically movable. In a preferred embodiment, therigid plate203 can be formed so that the neutral position is at an angle relative to thesurface substrate100 such that therigid plate203 protrudes away from thecell cavity400.
• In another embodiment, depicted inFIG. 6 the cell opening in the substrate over which the covering201 can be shaped so as to provide about the same elastic forces across the dimensions of therigid plate203. A preferred embodiment has a tear shaped opening such that the rigid plate's203pivot axis210 is fixed at or near the narrow point of the tear shape. The point of greatest deflection for the rigid plate is fixed around the radial point for the generally spherically curved portion of the tear shape. This allows the covering201 to stretch proportionally to the deflection amount along therigid plate203.
• In another embodiment, the cell cavity in the substrate can be a larger structure as shown inFIG. 5. Larger structures allow for multiplerigid plates203 to be associated with thesame cavity400 and thus the same cell pressure. In another embodiment, this larger structure can preferably incorporate a rigid covering over the entire opening which in turn has smaller openings shaped for individual rigid plates and coverings, similar toFIG. 6. This allows the design to simultaneously control the covering displacements with the elasticity of the covering and maintain approximately the same pressure applied to all of the individual coverings.
• FIG. 1gdepicts the cross-section of the types of structures depicted inFIGS. 4 and 5 with a covering, as described above. Thecurved front area102 of thesubstrate100 is followed by thecell200, which comprises a covering202 with preferably apiezoelectric material204 incorporated into parts of the covering205 so as to straddle the edges ofcavity400. Alternatively, embodiments containing magnets and coils can also be employed, as described above. InFIGS. 4 and 5, thecavity400 is depicted some distance from the leading edge of the structure. However, it is understood that thecavity400 can be positioned anywhere along thestructure100. For example, the cavity can be formed at the leading edge itself such that the covering is adjacent to or overlapping the leading edge of the structure. Such a design may be preferred in certain circumstances where the movement of the surrounding medium creates the greatest forces at the leading edge.
• In another embodiment, multiple layers of substrates can be oriented so as to funnel wind into smaller pathways which are adjacent to the openings to the cavities in the substrates. This can be visualized by stacking the embodiments depicted inFIGS. 1g,4 and5 to create a tiered structure with gaps between each tier. The gaps form the smaller pathways, funneling fluid flow along a path adjacent to thecover202 ofFIG. 1g. Alternatively, only one additional layer need be added to the embodiments depicted inFIGS. 1a-d, creating a single smaller pathway adjacent to thecover202. For example, a spoiler on a vehicle located over the top of an array of generator cells will serve to shrink the fluid flow pathway adjacent to thecovers202 of the generator cells.
• Similarly, as depicted inFIGS. 3a-c, thesubstrate100 comprises an aerofoil or wing structure such as a spoiler on a vehicle. The cells can be mounted on the top602 or the bottom601 surfaces or both. Alternatively, thestructure100 can also be hollowed out for a single cavity or comprise a plurality of larger cavities that contain multiple generator cells. These various designs are depicted inFIGS. 3-5. In a further embodiment, the substrate is incorporated into the body of the moving object. For example the substrate can be a panel on the body of a vehicle, such as the hood, truck, roof, or door panels. In another embodiment, the substrate can be incorporated into paneling underneath the vehicle. Additionally, the substrate can be incorporated into wall or roof panels of cargo trucks. This same paneling can also be incorporated into the sides or the roof of trains or rail transportation. The designs would be similar to those employed in vehicles and cargo trucks. The openings to the cavities in the substrate can also be coupled with a control mechanism that either clamps the elastic covering and/or rigid plate or slides over the covering. This allows the generator to be shut down during certain operating circumstances. For example, if the energy storage system is completely charged, the generator can be shut down instead of rerouting the energy. Alternatively, if the movement speed of the medium is outside an ideal range, the generator can be shut down until a better environment exists.
• In a preferred embodiment, the paneling is incorporated into the trunk of the vehicle such that the trunk itself serves also as the cavity for the embodiment. The cells are aligned along the back edge of the trunk. The covering over each of the cells comprises a rigid plate and an elastic membrane such that the rigid plate is elastically oriented in the neutral state up at an angle relative to the trunk surface to form a small spoiler shape. Magnets are attached to the rigid plates. A coil for each magnet is positioned underneath the rigid plate at a particular separation to allow for the anticipated downward deflection of the rigid plate. The coils are sized approximately equal to the cross-sectional area of the magnet. Alternatively, piezoelectric material or another electrogenerative film as previously described and known within the state of the art can be incorporated into the covering in lieu of or in addition to the magnet and coil design.
• The substrate could also be a panel on a boat. The paneling could be fixed to the top surface or upper siding of the boat to make use of the movement of air as the boat moves. Alternatively, the panel can be incorporated into the base of the boat which is underwater to make use of the relative movement of water.
• In another preferred embodiment of the present invention, the substrate can be incorporated with a dam, waterbed, or pipe so as to harness the flow of water or some other liquid as the medium. For example, as depicted inFIG. 7a, a hollowed ring structure can be formed for the substrate having acentral cavity250, aninner wall111, and anouter wall110. Optionally, the ring structure may have an internally supportingbeam112, although if the ring structure's depth is not too great, such a support structure would not be necessary because the structure would be supported from caps that would radially connectinner wall111 toouter wall110. Each coveredopening202 in the ring structure shares thesame cavity250. Alternatively, as shown inFIG. 7b, multipleseparate cavities252 can be formed within the ring structure betweeninner wall111 andouter wall110. The area betweenouter wall110 andcavity252 can either be hollow as well or filled in. Ifcavity252 is filled in, then functionally, it would be as ifouter wall110 was adjacent tocavity252. Each coveredopening202 has itsown cavity252. Various other combinations could also be easily implemented, for example, where pairs of covered openings could share the same cavity and multiple cavities would be incorporated into the ring structure. The ring structure can be incorporated into a piping system such that the inner surface of thering structure111 shares surfaces with the inner wall of the pipes. The connections can either be welded, glued, or screwed together. The inner ring surface has openings formed to the cavity or cavities and the openings are covered according to the various embodiments of the present invention previously described. In a preferred embodiment, the coverings are designed so that rigid plates in each of thecoverings202 are angled in the neutral state to protrude towards the central axis of the ring structure and into the fluid flow. The rigid plates are oriented so that the pivot axis or point for the rigid plates is the first part to be in contact with any fluid flow, thus accommodating rather than opposing the expected flow of fluid through the pipes.
• In another embodiment of the present invention, the substrate can be incorporated into the surface structure of a plane. In a preferred embodiment, the substrate is shaped as a ring along the outside of the body of a passenger plane. The ring has separate cavities equally and symmetrically positioned along the circumference. The coverings maintain a generally flat surface with the rest of the plane's body so as to minimize additional structures on the surface of the plane. The functionality of such an embodiment would be similar to the embodiments previously described above, especially the vehicular embodiments. In another embodiment similar to being incorporated into a plane, the substrate can be incorporated into an airborne generator design that is tethered to a cable. The airborne generator comprises a gliding or flying structure with generator cells incorporated into the surface. The airborne generator is then flown at high altitude to take advantage of greater and more consistent wind speeds. Because embodiments of the present invention minimize aerodynamic impact from the generator itself, the airborne generator would be able to better maintain altitude and would require less complex control systems to stay in flight.
• FIG. 8 depicts another embodiment of the present invention where the substrate comprises along tube120 which is sealed to provide a pressurized internal cavity. Thetube structure120 has openings, which are optionally but preferably symmetrically oriented along the length of thetube120, withcoverings202 that maintain the integrity of the internal cavity and provide a flexible surface structure so as to incorporate an electrogenerative device. The covered openings preferably create a dimpled arrangement along thecircular tube120.
• The embodiments described above are intended to provide illustrations of particular aspects of the present invention. It is evident to persons of ordinary skill in the art that various modifications and changes may be made thereto without departing from the broader understanding and scope of the present invention disclosed herein. The particular embodiments and figures are provided to illustrate aspects of the present invention and are not the only embodiments contemplated by that broader disclosure of the present invention herein.

Claims (15)

1. A fluid flow generator comprising:

a frame comprising a cavity and an opening in a surface of said frame connecting to said cavity;

a contacting surface for contacting a fluid flow over said surface of said frame and positioned relative to said opening in said surface to at least partially enclose said cavity, wherein said fluid flow results from movement of said frame through a medium comprising a gas;

a spring positioned to contact both said frame and said contacting surface; and

an energy converting portion interposed between said frame and said contacting surface for converting energy from movement of said contacting surface relative to said frame due to said fluid flow.

2. The fluid flow generator ofclaim 1, wherein said frame is a rigid material.

3. The fluid flow generator ofclaim 1 further comprising an elastic membrane connected to said contacting surface and said frame and positioned relative to said contacting surface and said opening in said frame surface to enclose said cavity.

4. The fluid flow generator ofclaim 1, wherein said contacting surface of said covering further comprises a shaped structure that extends beyond said frame and into said fluid flow.

5. The fluid flow generator ofclaim 1, wherein said contacting surface further comprises at least one of a curvilinear surface shape, a faceted surface shape and an angular shape.

6. The fluid flow generator ofclaim 1, wherein said opening comprises a plurality of edges on said frame surface and

said contacting surface is directly connected to one of said plurality of edges and not directly connected to at least another of said plurality of edges.

7. The fluid flow generator ofclaim 1, wherein said energy converting portion is made of at least one of a piezoelectric material, a magnet, a wire coil, and a nanowire.

8. The fluid flow generator ofclaim 1 further comprising an energy storing device.

9. The fluid flow generator ofclaim 8, wherein said energy storing device is made of at least one of a battery, a capacitor, a super capacitor, a flywheel, and a pressure tank.

10. A fluid flow generator comprising:

a frame comprising a cavity and an opening in a surface of said frame connecting to said cavity;

a covering positioned within said opening to cover at least a portion of said opening in said frame surface and to at least partially enclose said cavity;

said covering comprising a rigid composition having a curvilinear shape for contacting a fluid flow, wherein said fluid flow results from movement of said frame through a medium comprising a gas;

a spring coupled between said frame and said covering; and

an energy converting portion interposed between said frame and said covering for converting energy from movement of said covering relative to said frame due to said fluid flow.

11. The fluid flow generator ofclaim 10 further comprising an elastic membrane connected to said contacting surface and said frame and positioned relative to said contacting surface and said opening in said frame surface to enclose said cavity.

12. The fluid flow generator ofclaim 10, wherein said energy converting portion is made of at least one of a piezoelectric material, a magnet, a wire coil, and a nanowire.

13. The fluid flow generator ofclaim 10, further comprising an energy storing device.

14. A fluid flow generator comprising:

a frame comprising a cavity and an opening in a surface of said frame connecting to said cavity;

a fluid contacting means for contacting a fluid flow and at least partially enclosing said cavity, wherein said fluid contacting means is movable relative to said frame due to a fluid flow force resulting from movement of said frame through a medium comprising a gas;

a spring means for providing a restorative force on said fluid contacting means in opposition to said fluid flow force, wherein said spring means is coupled to said frame and said fluid contacting means;

an energy converting means interposed between said frame and said fluid contacting means for converting energy from movement of said fluid contacting means relative to said frame due to said fluid flow force.

15. The fluid flow generator ofclaim 14 further comprising an elastic means for fully enclosing said cavity.

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