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WO2018186896A1 - Système de conversion d'accélération en énergie de rotation - Google Patents

Système de conversion d'accélération en énergie de rotation Download PDF

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Publication number
WO2018186896A1
WO2018186896A1 PCT/US2017/029783 US2017029783W WO2018186896A1 WO 2018186896 A1 WO2018186896 A1 WO 2018186896A1 US 2017029783 W US2017029783 W US 2017029783W WO 2018186896 A1 WO2018186896 A1 WO 2018186896A1
Authority
WO
WIPO (PCT)
Prior art keywords
ballast
assembly
silo
sensor
compressed air
Prior art date
Legal status (The legal status 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 status listed.)
Ceased
Application number
PCT/US2017/029783
Other languages
English (en)
Inventor
Jorge Pablo FERNANDEZ
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.)
Jpf Holdings And Trusts LLC
Original Assignee
Jpf Holdings And Trusts LLC
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 US15/479,115 external-priority patent/US9926905B2/en
Application filed by Jpf Holdings And Trusts LLC filed Critical Jpf Holdings And Trusts LLC
Publication of WO2018186896A1 publication Critical patent/WO2018186896A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • F03B—MACHINES OR ENGINES FOR LIQUIDS
    • F03B17/00—Other machines or engines
    • F03B17/02—Other machines or engines using hydrostatic thrust
    • F03B17/025—Other machines or engines using hydrostatic thrust and reciprocating motion
    • 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
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G3/00—Other motors, e.g. gravity or inertia motors
    • 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
    • F03G—SPRING, WEIGHT, INERTIA OR LIKE MOTORS; MECHANICAL-POWER PRODUCING DEVICES OR MECHANISMS, NOT OTHERWISE PROVIDED FOR OR USING ENERGY SOURCES NOT OTHERWISE PROVIDED FOR
    • F03G3/00—Other motors, e.g. gravity or inertia motors
    • F03G3/02—Other motors, e.g. gravity or inertia motors using wheels with circumferentially-arranged compartments co-operating with solid falling bodies
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
    • F16D63/00—Brakes not otherwise provided for; Brakes combining more than one of the types of groups F16D49/00 - F16D61/00
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D13/00—Pumping installations or systems
    • F04D13/02—Units comprising pumps and their driving means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D25/00—Pumping installations or systems
    • F04D25/02—Units comprising pumps and their driving means
    • 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
    • Y02E10/20—Hydro energy

Definitions

  • the present invention relates to a system for converting acceleration to rotational energy to actuate various devices or assemblies.
  • Applicant is able to achieve the desired result with one ballast instead of two.
  • the Tung reference further requires a larger tank than the present invention, which creates additional complexity leading to added material costs and potential breakdowns.
  • FIG. 1 represents front elevational view of the present system in its operating environment after the initial phase.
  • ballast assembly 20 is filled with compressed air since that is how it is manufactured.
  • ballast assembly 20 can be seen filled with water since valves 24; 24a were opened upon ballast assembly 20 reaching the top of the silo to allow water in to sink the ballast back to the bottom in preparation for the next cycle.
  • FIG. 2 shows the beginning of the next cycle as ballast member 22 is still partially filled with water but compressed air from intermediary tank assembly 60 is being delivered to ballast assembly 20.
  • J-pipe 66 is seen allowing water into intermediary tank assembly 60 as compressed air has left its inner space.
  • FIG. 3 is a front elevational view showing ballast member 22 completely refilled with compressed air and intermediary tank 62 filled with water.
  • Figure 4 shows a front elevational view wherein ballast member 22 is permitted by brake 23 to begin rising bringing rack assembly 100 up with it.
  • Compressor 1003 is stationary but as rack 1001 moves upwards and against compressor 1003 via transmission 1002 it actuates the compressor releasing compressed air into intermediary tank to refill it. Water can be seen displaced through J-pipe 66 back into silo 42.
  • FIG. 5 shows rack assembly 100 at its uppermost point. At this point, latches 27; 27a are about to be released from anchoring members 104; 104a of rack assembly 100. Intermediary tank 62 is now fully filled with compressed air again.
  • Figure 6 shows latches 27; 27a now disengaged from anchoring members 104; 104a allowing rack assembly to drop to its bottommost position.
  • Ballast member 22 is now rising to the top of silo 42.
  • FIG. 7 represents a partial view of the present invention wherein ballast member 22 has risen to the top of silo 42 and valves 24; 24a are now opened allowing water, or any liquid that is used, to flood ballast member 22 and begin sinking it back down to the bottom of silo 42.
  • Figure 8 shows the continued descent of ballast member 22 within silo 42 and latches 27; 27a ready to reengage anchoring members 104; 104a.
  • Figure 9 shows a view of the present invention with the proportions that can be used.
  • Figure 10 illustrates an embodiment of the present invention wherein shaft 1000 is used to actuate an alternator.
  • Figure 11 illustrates an embodiment of the present invention wherein shaft 1000 is used to actuate a centrifugal pump.
  • Figure 12 illustrates an embodiment of the present invention wherein shaft 1000 is used to actuate a centrifugal blower.
  • FIG 13 Shows the phase in which the air filled ballast is released from the latching assembly and rises, transferring power from the Ballast's positive buoyancy to the power output shaft, for use in whatever system the output shaft is connected to.
  • This phase can go on for as long as is required the per the requirements of the system to which it is connected.
  • the system's output can be modulated by modifying the speed at which the Ballast rises through the partial engagement of the brake. It can operate in slow cycles for use in electrical generation, or in fast cycles for use in high demand situations. However, the output speed of the rising ballast is limited by the water resistance around the ballast when it rises, promoting it's use for more torque intensive procedures.
  • valves on it's topmost position are opened. This lets out any air contained within it's chamber allowing it to descend to the bottom of the tank.
  • FIG. 14 Shows the ballast refilling phase having three distinct stages labeled A, B, and C respectively.
  • ballast has just reached the bottom of the tank and has latched onto the assembly, also the brake is fully engaged, thus preventing the ballast from moving.
  • C Illustrates the finished exchange, specifically, the air filled ballast and the water filled intermediary tank.
  • Figure 15 Shows the intermediary refilling phase that is powered by the positive buoyancy of the ballast, 9946 Kg of buoyance respectively.
  • the bottommost point of the tank is 100 meters, specifically, 99 meters for the height of the tank, and 1 meter for the height of the intermediary tank.
  • the total pressure equals 9.672 atmospheres or 142.121 psi.
  • the speed at which the ballast rises is manipulated. This is done through the use of a brake which slows the rise of the ballast to a predetermined speed, and also thorough the use of a gear train to convert the buoyancy force into the proper format to be received for use by the compressor.
  • Figure 4 and Figure 5 show the process by which the intermediary tank is refilled.
  • Figure 16 Shows a side view of an embodiment for a gear train wherein through partial engagement of the brake, the ballast is permitted to rise at a rate of 2 inches per second, which rotates a gear with a radius of 5 inches.
  • the 5" radius gear has a sheave/gear attached to it which has a radius of 6.8", this uses either a chain or a v-belt to rotate the attached sheave/gear that has a radius of 5".
  • This sheave/gear is attached to the inner portion of a larger gear, which has a radius of 10".
  • This 10" gear is meshed with a smaller 4" gear.
  • the 4" gear is attached to a gear of 10" that uses a v-belt to run the compressors sheave of 5.9375".
  • Figure 17 Shows an alternate view of Figure 16.
  • Figure 18 shows a power output conversion table
  • ballast assembly 20 that can be a square or rectangular shape and its bottom end is open. Ballast assembly 20 can begin in its initial position already filled with compressed air. It can be manufactured that way. Ballast assembly 20 includes ballast member 22, upper valves 24; 24a and latch members 27; 27a, which are powered using motors 124; 124a. In one embodiment, motors 124; 124a can be powered by alternating current. In yet another the motors can be powered using direct current. The ballast assembly 20 is positioned inside a silo assembly 40 that is filled with liquid.
  • a cable 50 runs down the height of the silo assembly 40 and its first end 52 is mounted at the top of ballast assembly 20 and winds around rotational assembly 300 what includes wire drum 302.
  • the rotation of wire drum 302 can be used to rotate shaft 1000 that in turn can be used to actuate various instruments and/or equipment such as an alternator, a fan, or a pump.
  • the present invention can be understood to act as an educational device for the purposed of teaching how the acceleration from gravity as the ballast member 22 drops, or its buoyancy as it rises, can be converted to rotational energy. This can be practical when harnessing wasted energy from outside processes. The wasted energy can be transferred to acceleration which can then be transferred to rotational energy using the present invention.
  • Ballast assembly 20 includes sensors 25 that detect when ballast assembly 20 is at the top and bottom of the silo assembly 40. When sensor 25 detects sensor 25b the system knows that ballast member 22 has reached the top of the silo 42. The system will open valves 24; 24a allowing water to enter ballast assembly 20 and sink it to the bottom of silo assembly 40.
  • Cable 50 includes second end 54 that is mounted within ballast member 20 at its top wall opposite first end 52 after the cable 50 was wrapped around wire drum 302 and passed through a plurality of pulleys 28. In one embodiment, first end 52 does not meet with second end 54.
  • Anchoring members 104; 104a are mounted at the distal ends of rods 102; 102a of rack assembly 100. The bottom of rack assembly 100
  • air compressor 1003 includes a rack 1001 that cooperates with transmission member 1002 that in turn is fixed to the air compressor 1003.
  • air compressor 1003 can be stationary and rack 1001 moves up against transmission 1002 that in turn actuates the compressor to deliver compressed air into pipe 1004.
  • the system also includes intermediary tank assembly 60 that includes upper valve 65, connecting pipe 63 that allows compressed air to travel between intermediary tank assembly 60 and ballast assembly 20.
  • Intermediary tank assembly 60 can be manufactured with compressed air, ambient air, or liquid.
  • Upper valve 65 can be a one-way valve and is opened to allow compressed air inside of ballast assembly 20 when ballast assembly 20 is locked at the bottom of silo assembly 40. Latches 27; 27a engage anchoring members 104; 104a upon sensor 25 reaching the level of sensor 25a.
  • brake 23 prior to upper one-way valve 65 opening, brake 23 must be locking cable 50 thereby preventing any movement of cable 50 and in turn ballast member 22.
  • Intermediary tank 60 includes upper valve 65, connecting pipe 63 that allows compressed air to travel between intermediary tank assembly 60 and ballast assembly 20.
  • Intermediary tank assembly 60 can be manufactured with compressed air, ambient air, or liquid.
  • Upper valve 65 can be a one-way valve and is opened to allow compressed air inside of ballast assembly 20 when ballast assembly 20 is
  • Intermediary tank 60 also includes bottom valve 64 that can be a oneway valve that when opened allows compressed air to enter from air compressor 1003 via pipe 1004.
  • Intermediary tank assembly 60 also includes upper and lower float sensor 68a; 68b, respectively, housed therein. In its initial cycle the ballast assembly 20 begins at the bottom of silo 60 filled with compressed air. Brake 23 is released a predetermined amount allowing ballast assembly 20 to rise.
  • Lower float sensor 68b detects when the liquid has been replaced by the compressed air. At this point, latches 27; 27a are disengaged from anchoring members 104; 104a thereby preventing any further compressed air from exiting compressor 1003.
  • Rack assembly 100 is now permitted to drop into its initial position again.
  • top sensor 25b detects sensor 25 indicating that ballast assembly 20 has reached the top of the silo 42
  • valves 24; 24a will open allowing water in and the ballast will drop.
  • the intermediary tank 60 is filled with compressed air and rack assembly 100 has been lowered.
  • intermediary tank 60 using transmission 1002 and push the water out of J-Pipe 66.
  • ballast assembly 20 is traveling upwards through silo assembly 40 as brake 23 allows.
  • Brake 23 is controlled by the control unit that synchronizes all the sensors and valves of the system. Alternatively, brake 23 and the sensors and valves can be controlled manually.
  • ballast assembly 20 again reaches the bottom and latches members 24; 24a and brake 23 engage, ballast assembly 20 can be immediately refilled with the compressed air that was stored in intermediary tank 60. The process continues to repeat itself.
  • Latch members 27; 27a can also be hooks or any other means for anchoring the ballast member 22 to the rack assembly 100.
  • ballast member 22 While ballast member 22 is traveling up the silo member 42 cable 50 is rotating around drum 302 thereby converting the acceleration of the ballast member 22 to rotation energy. Also, when ballast member 22 is descending within silo member 42 cable 50 is also causing drum 302 to rotate converting the acceleration of ballast member 22 to rotation energy.
  • the system begins operations with air inside the intermediary tank and ballast tank. This prefilling is done as part of the manufacturing process of the machine, and this initial filling of compressed air occurs once and only the date of the machine manufacture.
  • the machine is manufactured to begin functioning in the condition observed in Figure 5 of the drawings.
  • variables will be provided for every relevant force involved in the process of the machine, and for simplicity are cited below; a) .
  • Force of Gravity 9.807 meters per second
  • the air filled ballast is released from the latching assembly and rises, transferring power from the Ballast's positive buoyancy to the power output shaft, for use in whatever system the output shaft is connected to.
  • This phase can go on for as long as is required the per the requirements of the system to which it is connected.
  • the system's output can be modulated by modifying the speed at which the Ballast rises through the partial engagement of the brake. It can operate in slow cycles for use in electrical generation, or in fast cycles for use in high demand situations. However, the output speed of the rising ballast is limited by the water resistance around the ballast when it rises, promoting it's use for more torque intensive procedures.
  • valves on it's topmost position are opened. This lets out any air contained within it's chamber allowing it to descend to the bottom of the tank.
  • the ballast refilling phase has three distinct stages labeled A, B, and C
  • A The ballast has just reached the bottom of the tank and has latched onto the assembly, also the brake is fully engaged, thus preventing the ballast from moving.
  • B The remote valve located in between the intermediary tank and the ballast tank is opened, allowing an exchange of air and water to take place between the intermediary tank and the ballast. Water can be seen entering the intermediary tank from the main tank by the presence of arrows in the J-pipe. Water enters the chamber through the J-Pipe and pushes the air from the intermediary tank into the ballast tank.
  • the intermediary refilling phase is powered by the positive buoyancy of the ballast, 9946 Kg of buoyance respectively.
  • the bottommost point of the tank is 100 meters, specifically, 99 meters for the height of the tank, and 1 meter for the height of the intermediary tank. Under 100 meters of fresh water, the total pressure equals 9.672 atmospheres or 142.121 psi.
  • the speed at which the ballast rises is manipulated. This is done through the use of a brake which slows the rise of the ballast to a predetermined speed, and also thorough the use of a gear train to convert the buoyancy force into the proper format to be received for use by the compressor.
  • Figure 4 and Figure 5 show the process by which the intermediary tank is refilled.
  • gear train for use in converting the ballast's power for use by the compressor is as follows:
  • the ballast is permitted to rise at a rate of 2 inches per second, which rotates a gear with a radius of 5 inches.
  • the 5" radius gear has a sheave/gear attached to it which has a radius of 6.8", this uses either a chain or a v-belt to rotate the attached sheave/gear that has a radius of 5".
  • This sheave/gear is attached to the inner portion of a larger gear, which has a radius of 10".
  • This 10" gear is meshed with a smaller 4" gear.
  • the 4" gear is attached to a gear of 10" that uses a v-belt to run the compressors sheave of 5.9375". This system procures the final result of 1750 RPM to the 5.9375 inch sheave. (Ingersoll- and 2475).
  • the compressor runs on 7.5 hp, which is 5595 Watts. Which means it requires 30.53 Joules of energy through torsion. Therefore, the tension on the belt running the 5.9375" compressor sheave clockwise should be around 404.9 Newtons, which is the equivalent of 91 lbf. This means the gears meshed would have a force of 1012.2 Newtons between them, which is equivalent to 227.5 lbf. Therefore, the tension in the V-Belt being driven counter clockwise should be approximately 2024.4 Newtons, which is 454.9 lbf. Therefore, the tension in the line needed for this to occur will have to be reduced to 2753.2 Newtons, which is 618.7 lbf.
  • the upward velocity of the ballast is: 0.05144 (m/s). Which is 5.144 cm/s, which is equivalent to 2.03 (in/s).
  • ballast displaces 10 cubic meters (353.147 cubic feet).
  • the water inside the intermediary tank is under 9.67 atmospheres or a pressure of 142.1 PSI.
  • the compressor cited is capable of moving 24 cubic feet of air per minute at a pressure of 175 psi when operating at 7.5 horse power.
  • the ballast travels upward and is totally engaged to a power output of any kind, providing its buoyancy torque of 21,9301bs or
  • the compressor's output is cited at 175 psi, yet a pressure of only 146 psi is needed in order to overcome the pressure inside the intermediary tank. Therefore, according to Boyles Law as the air enters into the intermediary tank, the
  • volumetric constraint of the air leaving the compressor will change. As it's pressure changes from 175 psi to 146 psi it will increase volumetrically by 20%. Thus the compressor will truly only need to pump 8.35 cubic meters of air or work for 737 seconds.
  • Compressor Ingersoll- and 2475;
  • Ballast Tank One-time air filling of Ballast Tank on date of machine manufacturing: ⁇ 6 kwh (energy cost).
  • This system condition is then sustained for 972 seconds, 50 meters of upward ballast travel.
  • the upward velocity of the ballast is: 0.05144 (m/s). Which is 5.144 cm/s, which is equivalent to 2.03 (in/s).
  • ballast displaces 10 cubic meters (353.147 cubic feet).
  • the water inside the intermediary tank is under 9.67 atmospheres or a pressure of 142.1 PSI.
  • the compressor cited is capable of moving 24 cubic feet of air per minute at a pressure of 175 psi when operating at 7.5 horse power.
  • the ballast travels upward and is totally engaged to a power output of any kind, providing its buoyancy torque of 21 ,9301bs or 21,31 libs to an electrical generating alternator, centrifugal water pump, centrifugal air pump, or any other process which requires a rotating shaft with sustained torque.
  • an electrical generating alternator centrifugal water pump, centrifugal air pump, or any other process which requires a rotating shaft with sustained torque.
  • 2 or more of my systems to work in unison, linked together through a transmission allowing for a more continuous output, but this is beyond the scope of this explanation as 1 system alone provides sufficient utility in generating electricity for use on a public grid or for pumping water or air, in or out of a large mine.
  • the compressor's output is cited at 175 psi, yet a pressure of only 146 psi is needed in order to overcome the pressure inside the intermediary tank. Therefore, according to Boyles Law as the air enters into the intermediary tank, the
  • volumetric constraint of the air leaving the compressor will change. As it's pressure changes from 175 psi to 146 psi it will increase volumetrically by 20%. Thus the compressor will truly only need to pump 8.35 cubic meters of air or work for 737 seconds.
  • the present invention has the industrial application of converting acceleration to rotation to convert one form of energy to another that requires or would greater benefit from rotational energy.
  • Other uses of the present invention include harnessing wasted energy from one process, such as heat, and transferring it to another more useful process using rotational energy

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)

Abstract

L'invention concerne un système qui convertit l'accélération en énergie de rotation en utilisant la gravité pour faire descendre un élément de ballast et la flottabilité pour le faire monter lorsque l'élément de ballast est rempli d'air comprimé. La montée initiale du ballast est commandée par un élément de frein. Cette montée fait monter un ensemble crémaillère qui actionne un compresseur pour recharger le réservoir intermédiaire en air comprimé de sorte que le cycle peut se répéter de lui-même. La phase initiale commence avec l'élément de ballast contenant de l'air comprimé de sorte qu'il peut monter dans un silo rempli de liquide, générant de l'énergie de rotation sur le parcours à l'aide d'un câble monté qui passe autour d'un tambour de fil. Une fois atteinte la partie supérieure du silo, des vannes s'ouvrent pour permettre à l'eau d'entrer dans le ballast, ce qui le fait plonger jusqu'au fond, créant ainsi une énergie de rotation supplémentaire.
PCT/US2017/029783 2017-04-04 2017-04-27 Système de conversion d'accélération en énergie de rotation Ceased WO2018186896A1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/479,115 2017-04-04
US15/479,115 US9926905B2 (en) 2016-01-21 2017-04-04 System for converting acceleration to rotational energy

Publications (1)

Publication Number Publication Date
WO2018186896A1 true WO2018186896A1 (fr) 2018-10-11

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PCT/US2017/029783 Ceased WO2018186896A1 (fr) 2017-04-04 2017-04-27 Système de conversion d'accélération en énergie de rotation

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115355131A (zh) * 2021-05-17 2022-11-18 方廷谆 双向位能发电设备及其动力输出装置

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060080957A1 (en) * 2003-01-10 2006-04-20 Fernandez Gomez Josejoaquin System for multiple harnessing and complemented conversion of energy from sea waves
US20090193808A1 (en) * 2008-02-06 2009-08-06 Launchpoint Technologies, Inc. System and method for storing energy
US20120285544A1 (en) * 2009-11-24 2012-11-15 Tov Westby Method for operating a buoyant body of a wave power plant and a wave power plant
US20160229297A1 (en) * 2015-02-08 2016-08-11 Hyperloop Technologies, Inc. Power supply system and method for a movable vehicle within a structure

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20060080957A1 (en) * 2003-01-10 2006-04-20 Fernandez Gomez Josejoaquin System for multiple harnessing and complemented conversion of energy from sea waves
US20090193808A1 (en) * 2008-02-06 2009-08-06 Launchpoint Technologies, Inc. System and method for storing energy
US20120285544A1 (en) * 2009-11-24 2012-11-15 Tov Westby Method for operating a buoyant body of a wave power plant and a wave power plant
US20160229297A1 (en) * 2015-02-08 2016-08-11 Hyperloop Technologies, Inc. Power supply system and method for a movable vehicle within a structure

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115355131A (zh) * 2021-05-17 2022-11-18 方廷谆 双向位能发电设备及其动力输出装置

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