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WO2019098997A1 - 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
WO2019098997A1
WO2019098997A1 PCT/US2017/061609 US2017061609W WO2019098997A1 WO 2019098997 A1 WO2019098997 A1 WO 2019098997A1 US 2017061609 W US2017061609 W US 2017061609W WO 2019098997 A1 WO2019098997 A1 WO 2019098997A1
Authority
WO
WIPO (PCT)
Prior art keywords
ballast
assembly
silo
plunger
tank
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/US2017/061609
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.)
Individual
Original Assignee
Individual
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
Application filed by Individual filed Critical Individual
Priority to PCT/US2017/061609 priority Critical patent/WO2019098997A1/fr
Publication of WO2019098997A1 publication Critical patent/WO2019098997A1/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
    • F03B17/04—Alleged perpetua mobilia

Definitions

  • the present invention relates to a system for converting acceleration to rotational energy to actuate various devices or assemblies.
  • FIG 1 represents front elevational view of the present system in its operating environment after the initial phase.
  • ballast assembly 20 is filled with water 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 into and sink ballast assembly 20 back to the bottom in
  • Intermediary tank assembly 60 can begin filled with compressed air in its initial stage.
  • plunger 1007 that is in the lowered position ready to push
  • 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 filled or refilled with compressed air and intermediary tank 62 filled with water that entered from J-pipe 66.
  • FIG. 4 shows a front elevational view wherein ballast member 22 is permitted to begin rising using brake 23 within silo once it is filled with compressed air moving chain 1020 along gear 1010 to urge plunger rod
  • plunger 1006 to rise and compress air within plunger tank 1003.
  • plunger 1007 rises and the psi delivered to valve 64 reaches a predetermined amount the compressed air from plunger tank 1003 enters intermediary tank assembly 60 in preparation for the next cycle.
  • Figure 5 shows plunger rod 1006 at its uppermost point any intermediary tank assembly 60 completely filled with compressed air.
  • 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.
  • Output shaft assembly 1002b includes output shaft 1000 that can be used to provide rotational force and/or drive various equipment such as fans, engines, etc.
  • Gear train assembly 1002a includes pulleys 302a, cable 1020, gear 1010 and pulley 302b.
  • the system also includes support beam 1005 that holds the entire output shaft assembly 1002b and silo 42.
  • FIG. 7 represents a front elevational view of the present invention wherein ballast member 22 has begun its descent within silo 42 by valves 24; 24a having been 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 illustrates an embodiment of the present invention wherein shaft 1000 is used to actuate a centrifugal blower.
  • Figure 9 illustrates an embodiment of the present invention wherein shaft 1000 is used to actuate a centrifugal pump.
  • Figure 10 illustrates an embodiment of the present invention wherein shaft 1000 is used to actuate a motor.
  • Figure 11 shows a view of the present invention with the proportions that can be used.
  • 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 and upper valves 24; 24a. 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.
  • Output shaft assembly 1002b 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, a motor, or a pump.
  • the present invention can be optionally 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 a plurality of pulleys 28 and brake 23. In one embodiment, first end 52 does not meet with second end 54.
  • Rack assembly 200 supports silo 42.
  • 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.
  • 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 assembly includes J-Pipe 66 that connects intermediary tank assembly 60 to silo assembly 40 and allows water to flow in and out of intermediary tank assembly 60.
  • Intermediary tank 60 also includes bottom valve 64 that can be a one way 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.
  • 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.
  • brake 23 reengages, valve 65 is actuated to release the compressed air inside intermediary tank 60 through pipe 63 and back into ballast assembly 20.
  • Compressed air is delivered to intermediary tank assembly 60 until lower float sensor 68b again detects that there is not enough liquid left because it is filled with compressed air. While intermediary tank 60 is being filled with compressed air, 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.
  • 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.
  • intermediary tank 62 is filled with compressed air
  • ballast 22 is filled with water and at the bottom of silo 42
  • plunger tank 1003 of plunger assembly 1009 is filled with air either compressed or not by plunger 1007.
  • Plunger assembly also includes one-way valve 1008 that allows the plunger to work as a syringe.
  • compressed air is transferred to ballast 22 using pipe 63 and one-way valve 65 until ballast 22 is filled with compressed air.
  • ballast 22 travels up silo 42 its buoyancy is translated to a force on cable 50 which translates the force to output shaft assembly 1002b that moves chain 1020 urging gear 1010 to move against plunger rod 1006 making it rise and in turn making plunger 1007 rise thereby compressing air inside plunger tank 1003.
  • the compressed air is allowed to travel out of plunger tank 1003 as it is being compressed and through plunger tank pipes 1004 which end on one end at valve 64.
  • Valve 64 only allows the compressed air to enter
  • intermediary tank 62 upon a certain psi being reached. When the predetermined psi is achieved, the compressed air will begin filling intermediary tank 62.
  • plunger 1007 lowers once again to the bottom of plunger tank 1003.
  • ballast 22 reaches the topmost height of silo 42 valves 24; 24a are opened to allow water to enter therein and begin causing ballast 22 to sink to the bottom.
  • output shaft 1000 is receiving rotational force to drive a predetermined device connected thereon.
  • plunger 1007 has returned to its lowered position ready to compress more air in plunger tank 1003 and intermediary tank 62 is filled again with compressed air ready to refill ballast 22.
  • Figure 4 depicts the cycle where the intermediary tank 62, is refilling with air and is thus“recharging” for the next cycle.
  • the next cycle occurs after the ballast tank 20 has totally risen and then has totally descended, as depicted in Figure 6, Figure 7, and Figure 1 respectively.
  • the predominant forces at work here are gravity, and pressure which is a byproduct of gravity.
  • a height to tank 40 is given of 100 feet, the water pressure at the bottommost part of the tank is 43.3 pounds per square inch. Note that this lowest point of 100 feet is actually located on j -pipe 66. If we set ballast 20, to have a dimension of 10 feet, then it’s buoyancy/displacement would be 62,436 LBS in fresh water. This buoyancy/displacement is calculated by multiplying the volume of the ballast 20 1000 cubic feet, by the weight of a water per cubic foot, 62.427 LBS. Boyles law states: For a fixed amount of gas kept at a
  • ballast 20 https://www.scubatoys. com/education/boylel .asp” [024] As the pressure at the bottom of ballast 20 is 43.3 pounds per square inch, this approximates to 3 atmospheres. Plunger 1003 is transferring the entirety of itss air content to the intermediary tank 62, plunger 1003 must have 4 times the air capacity, and its dimensions are 10 feet* 10 feet*40 feet respectively.
  • gear 1010 The function of gear 1010, is to apply a power increasing gear ratio to the plunger 1003.
  • gear ratio .9: 1.
  • This gear ratio thus makes it possible for a force of 67,144 LBS to be applied to the plunger 1003, (60,436 LBS buoyancy/displacement + 6,708 LBS gained through ratio) thus creating a pressure of 46.62 pounds per square inch, an amount greater than the bottommost pressure of 43.3 pounds per square inch, an amount sufficient to operate one-way valve 64, and amount sufficient allow for the refilling cycle to occur.
  • ballast would have to travel roughly 25% more than the height of the plunger to compensate for the power increasing gear ratio. Therefore, under these different conditions the ballast would have to rise 50 feet and leave a power phase of only 40 feet. This would leave less of a power phase and could thus be considered less efficient as the machines power cycle time would be shorter and less power per cycle would be converted.
  • buoyancy is always experienced. This machine would not function whatever in an environment without an acceleration, such as space, further testament that the machine requires the constant input of gravity. So long as buoyancy is experienced the machine would run as per the laws of physics and the calculations provided.

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (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 celui-ci est rempli d'air comprimé. La montée initiale du ballast est commandée par un élément de frein. Cette flottabilité associée à la montée du ballast amène un élément plongeur à s'élever ce qui comprime l'air utilisé afin de recharger le réservoir intermédiaire de sorte que le cycle peut se répéter de façon autonome. L'élément de ballast génère de l'énergie de rotation le long de la voie à l'aide d'un câble monté qui se déplace autour d'un ensemble arbre de sortie. 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/US2017/061609 2017-11-14 2017-11-14 Système de conversion d'accélération en énergie de rotation Ceased WO2019098997A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PCT/US2017/061609 WO2019098997A1 (fr) 2017-11-14 2017-11-14 Système de conversion d'accélération en énergie de rotation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/US2017/061609 WO2019098997A1 (fr) 2017-11-14 2017-11-14 Système de conversion d'accélération en énergie de rotation

Publications (1)

Publication Number Publication Date
WO2019098997A1 true WO2019098997A1 (fr) 2019-05-23

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023063908A1 (fr) * 2021-10-11 2023-04-20 Ziada Ramadan Machine à mouvement perpétuel

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB112893A (en) * 1917-06-23 1918-01-31 Philip Arthur Newton Arrangement for Non-automatic Regulation of the Bouyancy of Submarines.
GB207395A (en) * 1922-12-16 1923-11-29 Larner Johnson Valve And Engin Improvements in valves for ballast tanks
US20080264056A1 (en) * 2007-04-26 2008-10-30 Jui-Chi Tung Hydraulic buoyancey kinetic energy apparatus
US20100307149A1 (en) * 2007-12-19 2010-12-09 James Kwok Hydrodynamic energy generation system
WO2016026894A1 (fr) * 2014-08-19 2016-02-25 Architecture Et Conception De Sytemes Avances Procédé et système de contrôle d'un dispositif de réglage de flottabilité comprenant un récipient prévu pour contenir un gaz et un liquide

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB112893A (en) * 1917-06-23 1918-01-31 Philip Arthur Newton Arrangement for Non-automatic Regulation of the Bouyancy of Submarines.
GB207395A (en) * 1922-12-16 1923-11-29 Larner Johnson Valve And Engin Improvements in valves for ballast tanks
US20080264056A1 (en) * 2007-04-26 2008-10-30 Jui-Chi Tung Hydraulic buoyancey kinetic energy apparatus
US20100307149A1 (en) * 2007-12-19 2010-12-09 James Kwok Hydrodynamic energy generation system
WO2016026894A1 (fr) * 2014-08-19 2016-02-25 Architecture Et Conception De Sytemes Avances Procédé et système de contrôle d'un dispositif de réglage de flottabilité comprenant un récipient prévu pour contenir un gaz et un liquide

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023063908A1 (fr) * 2021-10-11 2023-04-20 Ziada Ramadan Machine à mouvement perpétuel
US12467429B2 (en) 2021-10-11 2025-11-11 Ramadan Ziada Hydro-mechanical energy transfer system with dynamic water tanks and turbine generator

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