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Title:
ENERGY CONVERSION SYSTEM
Document Type and Number:
WIPO Patent Application WO/1983/002693
Kind Code:
A1
Abstract:
A system for converting one form of energy into an alternate form of energy by means of a low-temperature process. A liquid flow loop with two vertical columns (13, 15) that are interconnected at the top and bottom circulates a fluid. A convective flow of this fluid is established by heating the fluid in one of the columns and cooling the fluid in the other column to establish a weight differential between the fluid in the two columns (13, 15). An electric generator (101) is placed on this loop so that, as the fluid flows through the loop and through the generator (101), electrical energy is generated. This electrical energy is used to electrolize a second fluid, such as a solution of sulphuric acid, into gasses such as hydrogen and oxygen. The gasses so generated are used to increase the rate of flow of the fluid, and consequently the rate of electric energy production. In one embodiment, the gasses are injected into the rising column (13) of the fluid to increase the weight differential between the fluid in the two columns (13, 15) and enhance the convective flow of that fluid. These gasses, which contain chemical energy, are then removed from the loop at the top (71) of this column (13). Alternatively, the gasses can be accumulated at high pressure, and the pressure used to inject a volatile fluid into the loop.

Inventors:
COVER JOHN H (US)
Application Number:
PCT/US1983/000117
Publication Date:
August 04, 1983
Filing Date:
January 25, 1983
Export Citation:
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Assignee:
COVER JOHN H
International Classes:
H02K44/08; (IPC1-7): H02K44/00
Foreign References:
DE2405134A11975-08-07
US4127453A1978-11-28
US3616334A1971-10-26
US3375664A1968-04-02
US3443129A1969-05-06
US3878410A1975-04-15
US3999089A1976-12-21
US4191901A1980-03-04
Other References:
See also references of EP 0099928A4
Download PDF:
Claims:
I CLAIM:
1. An apparatus for converting one form of energy into an alternate form of energy, including a fluid conduit [15] through which flows a fluid, first means [21] for establishing a flow of said fluid through said conduit [15], and second means [101] coupled to said conduit [15] for generating electrical energy from said flowing fluid, wherein said apparatus is characterized by: (a) third means [51] coupled to said second means [101] for using at least a portion of said electrical energy to form a gas; and (b) fourth means [59,211,213] for using at least a portion of said gas to increase the rate of flow of said fluid through said fluid conduit [15]. 2. The apparatus of Claim 1, wherein said fourth means is characterized by introducing means [59] for introducing into said conduit at least a portion of the "gas formed by said third means [51] so that the rate of flow of said fluid is increased. 3. The apparatus of any of Claims 1 to 2, wherein said fourth means is characterized by a fluid container [211,213] having a fluid outlet [217] that can be selectively opened and closed, wherein said container [211,213] is coupled to said third means [51] so that said gas pressurizes fluid in said container [211,213] so that when said fluid outlet [217] is opened, said fluid is propelled out of said container [211,213] into said fluid conduit to increase the rate of flow of said fluid in said conduit. 4. The apparatus of Claim 3, wherein said fourth means is additionally characterized by a gas accumulator 229 having an inlet coupled to said third means 51 and an outlet coupled to said fluid container 211,213 so that said gas accumulator: (a) receives said gas from said third means 51; (b) stores said gas at a pressure; and (c) supplies said gas under pressure to said fluid container [211,213].
2. 5 The apparatus of Claim 3, wherein said fourth means is further characterized by (a) means for receiving a second, volatile fluid; (b) a fluid coupling between said fluid container [221,213] and said introducing means [59], so that said second fluid is introduced into said fluid conduit [13,15].
3. 6 The apparatus of any of Claims 1 to 5, wherein: (a) said one form of energy is thermal energy; (b) said first means [21] for establishing a flow of said fluid through said conduit [15] is characterized by means for adding thermal energy to said fluid, to create a flow of said fluid; and (c) said gas formed by said third means [51] contains chemical energy.
4. 7 The apparatus of any of Claims 1 to 6, wherein: (a) said fluid has low electrical resistance; and (b) said second means [101] is a magnetohydrodynamic generator.
5. 8 The apparatus of any of Claims 1 to 7, wherein: (a) said fluid conduit is characterized by: (1) a first, substantially vertical leg [13]; (2) a second, substantially vertical leg [15]; (3) first communication means between the top of said first leg [13] and the top of said second leg [15] ; and (4) second communication means between the bottom of said first leg [13] and the bottom of said second leg [15] ; (b) said fluid flows upwardly through said first leg [13]; (c) said fluid flows downwardly through said second leg [15] ; and a (d) said second means [101] is coupled to said conduit near the bottom of said second leg [15]. 9. The apparatus defined in any of Claims 1 to 8, further characterized by means [71] for removing said gas from said conduit [13,15].
6. 10 The apparatus of any of Claims 7 to 9, wherein said magnetohydrodynamic generator [101] is characterized by: (a) a throat segment [17] of said second vertical column [15] through which said fluid flows; (b) a magnet [111] creating a magnetic field perpendicular to said flow of fluid through said throat segment [17] so that as said fluid flows through said throat segment [17] , an electric potential is created between two sides of said throat segment [17] ; and (c) electrodes [133,135] co.upled to said throat segment [17], said electrodes [133,135] tapping said electric potential.
7. 11 The apparatus of Claim 10, wherein said throat segment [17] is of smaller crosssectional area than another section of said second vertical column [15] to provide a venturi effect to said flow.
8. 12 The apparatus of any of Claims 1 to 11, wherein said third means is characterized by an electrolytic gas generator [51] coupled to said second means for generating electrical energy [101].
9. The apparatus of Claim 12, wherein: (a) said fluid is an electrolyte; (b) said electrolytic gas generator [51] electrolyzes at least a portion of said fluid; and (c) said electrolytic gas generator [51] is coupled to said conduit [13,15] so that said gas may be introduced into said conduit.
10. The apparatus of Claim 12, wherein: (a) said electrolytic gas generator [51] electrolyzes a second fluid; and (b) said fourth means for using said gas is characterized by introducing means [59] coupled to said conduit [13,15] for introducing said, gas into said conduit [13,15].
Description:
-1- ENERGY CONVERSION SYSTEM Background of the Invention With the advent of higher prices " for the energy t world consumes, much interest has been generated in ne sources of energy and in more efficient uses of thi energy. One of the energy conversion devices for whic promise has been held is the magnetohydrodynamic generato (MHD). The basis for the operation of an MHD is tha passing an electrically conducting fluid through a stron magnetic field will produce an electric potential betwee opposite sides of the throat through which the conductin fluid flows. The magnitude of the power generated with given fluid is proportional to the velocity of the " flui through the throat. MHD development has typically focused on the use o high temperature, high pressure gas or plasma, althoug some systems have been developed using an electricall conducting liquid. The temperature of the plasma o liquid used in these devices is usually on the order o several hundred to a few thousand degrees Celsius. Th pressure under which the working fluid operates is als very high in most systems, on the order of several hundre to a few thousand pounds per square inch. The use of suc high temperature and pressure fluids limits the choice o materials out of which the system can be made. The hig temperatures and high pressures in these systems also mak the systems prone to leaks and contribute to the rapi deterioration of machinery such as pumps used in th system. To provide the flow of conducting fluid through th MHD throat, some systems have incorporated means fo establishing a convective flow of the fluid around closed loop.' This convective flow is established by

heating the fluid at one point in the loop and cooling it at another. Such a system is shown in U.S. Patent No. 3,375,664 to Wells. It has been found, though, that the low velocity thus obtained has not been sufficient to 5 permit the MHD to generate more than a few milliwatts of power even with vertical leg members up to 100 feet tall. Another means of causing a flow of the conducting fluid through an MHD loop has been to establish a convective flow, by introducing a gas into part of the loop

*° to create a density differential between the fluid in different sections of the loop. This has " typically been accomplished by boiling either the conducting liqui or a second fluid and using the vapor bubbles to leviate one column of the fluid. A system that operates in this

15 manner is disclosed in U.S. Patent No. 3,443,129 to Ham itt. Such systems, however, have been troublesome, since boiling the fluid takes thermal energy from the system, reducing the heat in the conducting fluid in the rising column. Also, the height and temperature of the

20 rising, column are severely constrained by the need to prevent condensation of the gas bubbles before they reach the top of the column.

Summary of the Invention The present invention includes an apparatus for

2 5 converting one form of energy into an alternate form of energy, and comprises a fluid conduit through which flows a fluid, a first means for establishing a flow of said fluid through the fluid conduit, an electric generator coupled to the conduit to generate electric energy from

30 the flowing fluid, a gas generator that uses a portion of the electric energy generated by the electric generator to form a gas, and an apparatus that uses at least a portion of the gas generated by the gas generator to increase the rate of flow of the fluid through the conduit.

^ 5 The present invention efficiently converts thermal energy (heat) into an alternate form of energy by means of

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a low-temperature process. The invention consists of a fluid flow loop with two vertical columns interconnected at the top and the bottom. The fluid that flows in this loop is an electrically conducting fluid, preferably a liquid such as mercury. The column in which the fluid rises is heated to a temperature of approximately 40 - 150° C by a thermal source and the column in which the fluid flows down is cooled to a temperature of approximately 0 - 30° C by means of a lower temperature heat sink. The difference in the density of the fluid in these columns induces a convective flow of that fluid through the loop. An MHD is coupled to one of these vertical columns. The MHD includes a magnet that creates a strong magnetic field perpendicular to the flow of the fluid. As the fluid flows through throat sections that have electrodes in contact with the fluid, an electric potential is generated between the electrodes, causing an electric current to flow through the electrodes and through an external electric circuit, from which power may be drawn. The key to the present invention is that the electric power so produced is largely fed back to augment, or speed up, the flow of the conducting liquid. This is accomplished by using the electric power to dissociate water molecules in an electrolytic solution, such as sulfuric acid, H 2 SO 4 , and inject some, or all of the gasses obtained (H 2 and C^) into the rising column of conducting liquid. The gas is removed from the loop at the top of the rising column and may be put to any of a number of uses. The remainder of the gasses, which are not injected into the loop may be taken directly from the electrolysis and put to use. Among the possible uses for the gasses produced by this system are burning to produce heat, power and pure water using them to synthesize other fuels, such as methane or methanol. The introduction of the gas into the rising column greatly reduces the density and weight of the rising column of electrically conducting liquid.

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and hence increases the weight difference between the two columns of liquid. As the weight difference between the columns is increased, the convective flow of the liquid is increased, further increasing the production of electrical energy. With the increased electrical output, more gasses are produced, and the convective flow velocity of the liquid is further increased> which additionally increases the amount of electric power generated by the MHD. The rate of generation of the electrolyzed gasses is increased until an equilibrium is established between the generation of the gasses and the viscous and other flow retarding forces.

The Thermal Energy Conversion System of the present invention has numerous advantages over the MHD systems previously developed. These advantages include:

1) lower operating temperatures for the working fluid;

2) lower pressures in the system loop ?

3) less severe constraints on the design and size of the system components;

4) less severe constraints on the choice of materials out of which the system components are made; and

5) greater power output with a smaller system due to increased operating efficiency.

Brief Description of the Drawings FIGURE 1 is a schematic drawing of the Thermal Energy Conversion System of the present invention.

FIGURE 2 is a perspective view of the 20 magnetohydrodyna ic generator coupled to the fluid flow loop.

FIGURE 3 is a perspective view of the magnetohydrodynamic generator with the magnet withdrawn from the throat section of the fluid flow loop. FIGURE 4 is a cross-sectional view of .the magnetohydrodynamic generator . used in the present invention taken along lines 4-4 of Figure 2.

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FIGURE 5 is a cross-sectional view taken along line 5-5 of Figure 2.

FIGURE 6. is a cross-sectional view taken along line 6-6 of Figure 2. FIGURE 7 is a schematic drawing of a first alternative embodiment of the. Thermal Energy Conversion System.

FIGURE 8 is a schematic drawing of a second alternative embodiment of the Thermal Energy Conversion System.

FIGURE 9 is a schematic drawing of a third alternative embodiment of the Energy Conversion System of the present invention.

FIGURE 10 is a schematic drawing of a fourth alternative embodiment of the Energy Conversion System of the present invention. FIGURE 11 is a schematic drawing of a fifth alternative embodiment of the Energy Conversion System of the present invention.

Description of the Preferre Embodiment General System The system of the present invention is shown schematically in Figure 1. It comprises a fluid loop 11 that is preferably closed, including first and second vertical columns or legs 13 and 15 that are interconnected at the top and bottom. A conducting fluid, such as liquid mercury, flows through the loop 11. Liquid mercury is advantageous because of its high electrical conductivity, high density, and low specific heat value, but other electrically conductive fluids such as electrolytic solutions may also be used, depending on cost considerations, equipment design or availability, or other factors. On the second column 15 is an electric generaor 101, such as a magnetohydrodynamic generator (MHD) 101. Electrical, leads 43 transmit the electric potential generated by the MHD 101. A source of thermal energy 21 is coupled to the loop near the bottom of the first column 13. This source 21

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ay be virtually any type of thermal energy source, including a burner for fossil fuels or a heat exchanger drawing heat from a reservoir heated by either solar energy or geotheππal energy. The temperature ' increase provided by the thermal energy source 21 depends upon the environment in which the system operates. This temperature increase can range from 20 to 100° C or more, and is preferably at least 40° C.

A heat exchanger or other device for removing thermal energy from the working fluid 31 is connected to the loop near the top of the second column 15 to draw heat from the conducting fluid and transfer it to a heat sink, such as a large body of cool water that is isolated from the sun, or some other low temperature body, which may be a body of ice if the system is used in a particularly cold environment.

A gas injector 59 for introducing gas into the system loop is placed near the bottom of the first column 13.

Gas injector 59 is a gas nozzle outlet of conventional design and is substantially centrally located in column

13.

A gas separator 71 is coupled to the loop near the top of the first leg 13. Separator 71 may be of conventional design for drawing gas from a two-phase flow. Gas separator 71 permits the liquid mercury to continue flowing around the loop, while removing the gasses introduced by gas injector 59 to be drawn off through outlet 73. Outlet 73 is connected so that the gasses may be put to other uses, such as burned to produce heat or power, stored to be burned later, or used to snythesize other fuels, such as methane or methanol.

An electrolytic gas generator 51 uses the electrical energy generated by the MHD 101 to electrolyze an electrolyte, such as a solution of sulfuric acid (H2SO ) to generate hydrogen and oxygen * gas, which contain chemical energy. The pressure at which the gas generator

ust be capable of producing the gasses depends upon the static pressure in column 13 at gas injector 59 caused by the- column of. ercury, since, to enter the column, the gas must be at a pressure at least as great as that of that static pressure. This static pressure depends on the height of the columns 13 and 15. For a small system with short columns, the gas generator 51 need only produce the gas at a pressure of a few pounds per square inch, while a gas generator coupled to a system using much taller columns needs to produce the gas at a pressure on the order of a few hundred pounds per square inch.

Outlet 53 from the gas generator 51 is preferably designed to keep the oxygen and hydrogen formed by the gas

. generator separate, since together they form a potentially explosive mixture. Outlet 53 branches into pipes 55 and

57. Pipe 55 leads to gas injector 59, so that part or all

" of the gasses generated by the electrolytic gas generator

51 may be injected into the first column 13. Valve 63 is provided on pipe 55 to control the volume of gas entering the fluid flow loop. Pipe 57 leads to a device for either storing or using the gasses. Advantageously, pipe 57 also keeps the gasses segregated, so that some of whichever of the gasses is injected into the column 13 may, if desired, also be diverted away from the flow loop, and stored or used directly. Valve 65 on pipe 57 controls ,the volume of gas being diverted away from the flow loop. Adjusting the valves 63 and 65 permits careful control of the portion of gasses that goes directly to other uses and the portion introduced into the fluid flow loop.

Electrical leads 43 and 47 permit the power generated by the MHD 101 to be transferred to the electrolytic gas generator 51. This feedback of the power generated back into the system greatly increases the system's efficiency. Leads 45 permit power that is not used to operate the gas generator 51 to be drawn off the system and used for other purposes.

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The MHD The MHD 101, shown in Figures 2-6, includes a magnet 111 with closely juxtaposed north and south poles 115 and 113, a nonferromagnetic block 121, and electrodes 133 and 135. Between the poles 115 and 113 is a throat section 17 of the block 121 (Figure 4). This throat section 17 is defined by two closely juxtaposed rectangular walls 127 and 129 to allow a thin sheet of the mercury to pass between the poles of the magnet. The magnetic poles 113 and 115 are closely juxtaposed to maximize the intensity of the magnetic field across the sheet of mercury passing through throat section 17. Block 121 further includes threaded openings 122 and 124 for receiving the ends of the tubular piping that forms the remainder of the second column 15. The passage through which the mercury passes is tapered within the portions of the block 121 above and below the throat section 17 to form a transition between the tubular section of the second leg 15 and the thin throat section 17. As shown in Figure 2, the exterior of the block 121 is also narrowed at throat section 17 so it will fit between the poles 113 and 115 of the magnet 111.

Electrodes 133 and 135 (Figure 5) are placed on either side of this throat section 17 to tap the electric potential created between these two sides of the throat section. These electrodes are advantageously shaped so

' that continuous contact between the electrodes and the mercury flowing through the throat section 17 is promoted.

The throat section 17 is sized so that a venturi effect provides a ratio of approximately five to one between the speed of the mercury through the throat and the speed through the other sections of the loop.

The fluid flow passage through the MHD 101 must be constructed to contain the mercury flowing through it, particularly at the threaded openings 122 and 124, and at the points at which electrodes 133 and 135 enter throat section 17. But the passage is not subjected to the very

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- - high pressures that the MHD throat sections of systems that use a plasma as the working fluid must contain. The Electrolytic Gas Generator Electrolysis occurs when an electric current is passed through an electrolyte between two electrodes, an anode and a cathode. Ions in the solution move to and from the anode and cathode so that material may be transported and deposited on one of the electrodes, new compounds may be formed, or gasses may be liberated. Certain electrolytes, such as sulfuric acid, sodium hydroxide, and potassium carbonate, when dissolved in water, cause the water itself to decompose into its component parts, hydrogen and oxygen, when a current is passed through the solution.

The amount of material or gas formed by the electrolysis can be found using Faraday's Laws, which say that (1) the amount of chemical change produced by an electric current is proportional to the quantity of electricity and (2) the amount of different substances liberated by a given quantity of electricity are proportional to their chemical equivalent weights. (Equivalent weight = atomic weight divided by valence change.) Thus, the amount of material or gas produced is proportional to the current passed through the solution. When water is electrolyzed, the volume of hydrogen and oxygen produced is proportional to the current passed through the solution.

An example of a simple electrolytic gas generator that may be installed in the present system as gas generator 51 is a fully charged automobile storage battery comprising lead plates immersed in a solution of sulfuric acid. As current is passed through the solution in the cell the water in the solution is dissociated into hydrogen and oxygen. The hydrogen is given off at one of the electrodes, and the oxygen at the other. As the electrolyte solution is dissociated into its component parts to form the gasses, the water must be replaced, but

the acid itself remains in the solution.

The gasses produced should be kept separate, since, in the case of hydrogen and oxygen, the two gasses together form an explosive mixture. This separation can be maintained by placing a membrane between the electrodes.

Since the' amount of gas produced is proportional to the current, but not the pressure under which the cell operates (except at the extremes), the gasses may be produced at relatively high pressures with negligible increases in the power consumed. Generation of gasses at a pressume of forty atmospheres is possible with electrolysis. Even by conservative estimates, the electrolytic process can produce high pressures .in gasses 15% more efficiently than standard mechanical pumps. Other types of electrolytic cells may also be used as gas . generator 51. A cell comprising a nickle anode and iron cathode immersed in a solution of sodium hydroxide in water produces oxygen at the anode and hydrogen at the cathodes. Nickel electrodes immersed in a solution of potassium carbonate may also be used to produce hydrogen and oxygen.

The'Thermal Energy.Source The thermal energy source 21 may be one of a number of available apparatuses for transferring thermal energy to the fluid circulating in the loop. The purpose of the thermal energy source 21 is to increase the temperature of the liquid in column 13 relative to the liquid in column 15 so that a density differential is established between the mercury in the two. columns, causing a convective flow of the fluid liquid around the loop. Thus, the greater the temperature differential that can be established, the greater the convective flow of the liquid.

Particularly appropriate as a thermal energy source, in light of the interest in renewable resources, is a heat exchanger drawing heat from a solar heated reservoir. Panels for heating liquids such as water using solar

energy are Commercially available in many sizes from numerous sources, as are containers for storing the solar heated water. Heat exchangers are also readily available that can be coupled to the closed loop and are suitable for circulating the heated water from the reservoir and transferring its heat to the mercury circulating in the closed loop. Such apparatus can provide a 40° C temperature differential, which is suitable for operation of the system. . Also appropriate would be the use. of a heat exchanger circulating geothermally heated water. Geothermally " heated water often is at a much higher temperature than solar heated water would be, on the order of 120-180° C, and thus would be able to produce a greater temperature differential betv;een the mercury in column 13 and the mercury in column 15. This increased temperature differential is advantageous in that the density differential between the mercury in the two columns is greater, and consequently the convective flow of the mercury is increased. But, the availability of geothermal energy is limited.

In addition to the sources of thermal energy just discussed, a fossil fuel burner of conventional design may be used as thermal energy source 21 to directly heat the circulating mercury.

Since the- important consideration for operation of the system is the temperature differential between the liquid in the two columns 13 and 15, heat exchanger 31 must be connected to a heat sink capable of absorbing from the liquid the heat transferred to it by thermal energy source 21. In a system located in a temperature climate, this is most effectively done by circulating in the heat exchanger cool water drawn from a large reservoir kept cool by isolating it from exposure to the sun. In a colder climate, a large body of ice may be used, which would permit the temperature of the mercury to be reduced to 0t ( o

C, or perhaps, lower. *

Alternatives for Energ Input The thermal energy source 21 inputs energy into the system to create the flow of fluid through the conduit to allow the electrical generator 101 to produce electrical energy. Thus, the thermal energy source 21 can be replaced by any of a number of other mechanisms for inputting energy to the fluid, such as a pump that impacts kinetic energy directly to the fluid. The flow creator 21 begins the movement of fluid around the loop and through the electric generator 101 so that the production of electric energy is begun. Once the production of electric energy has begun, the gas generator 51 can be used to produce gas, and the gas can be used by the flow augmentation means to increase the rate of flow, and consequently increase the - rate of production of electric energy. The input of energy through the energy source 21 continues to ensure the continued flow of fluid through the conduit. if. the flow creator 21 is a pump or other non-thermal energy source, then obviously the heat sink. 31 is not necessary at the top of the second column 15, since there is no additional heat in the working fluid that must be removed. Operation ' o 'the System

In operation, thermal energy is added by heat source 21 to the conducting fluid in the first column 13 to lower the density of the fluid in that column, . thereby inducing a convective flow of the mercury. The heat so introduced into the conducting fluid is removed by the heat exchanger 31 at the top of the second column 15 to ensure the continuation of the temperature differential (and the density differential) between the mercury in the first and second columns. As the fluid flows downward in the second column, it flows through the throat section 17 of the MHD 101 in a direction perpendicular to the magnetic field

established by the magnet 111. This flow, by reason of Faraday's Laws, creates an electric potential between the sides of the throat section 17, which is tapped by the electrodes 133 and 135. This purely temperature-induced convective flow through the MHD will generate a very low power output. The power output is low due to the low velocity of the electrically conducting fluid through the MHD.

The electric potential is produced in the following manner: When a sheet of. conducting material, e.g., mercury, is passed through a magnetic field, that is perpendicular to the direction in which the conducting material is moving, an electric potential develops between points on the sheet of conductive material that lie on an axis perpendicular to both the direction of movement of -the conductive sheet and the direction of ' the magnetic field.

As the conductive fluid flows with velocity v through the perpendicular magnetic field B, a force is exerted on each charge carrier in a. third, mutually perpendicular direction. This force F is given by the vector equation:

F = qy x B in which q is the charge of each charge carrier. The electric field intensity (E) resulting from this force is given by the vector equation:

.F E = -^- = v x B.

This electric field yields an electric potential between two sides of the channel through which the conductor flows. This potential is:

E = / E'dL = / (v x B)*dL in which L represents the width of the. sheet of conductive fluid.

In the MHD loop, flow equilibrium is reached when the electromotive force so generated equals the force driving

the fluid flow, the difference in the weight of the mercury in the two columns.

By using the electric power generated by the MHD 101 to electrolyze a second fluid in gas generator 51 and introduce the gasses so generated into the rising first column 13, the efficiency of the system can be greatly increased due to the increased rate of flow of the . electrically conducting fluid through the MHD. When the gasses produced by the electrolytic gas generator 51 are introduced into the first column 13, the density and weight of the mercury in that column, is substantially decreased, which increases the density and weight differentials between the fluid in the first column 13 and the fluid in the second column 15. This increased differential greatly enhances the convective flow of the mercury around the loop, increasing the rate of flow of the conducting fluid through the throat 17 of the MHD section of the loop. As this flow through the throat section is increased, so is the power produced by the

MHD. This increase continues until a new flow equilibrium is reached. The gas injected into the upflow column 13 also contains mechanical energy, because it is under pressure. When the gas is injected, it occupies a small volume because of the high pressure at which the gas generator 51 creates it. As the gas bubbles rise in the column 13, the pressure of the surrounding fluid decreases, allowing the gas to expand. It has been found

•that the energy of compression of the gas is converted into kinetic energy of the working fluid as the expanding gas works on the fluid.

The gasses introduced into the loop, which also contain chemical energy, are separated from the conducting fluid at the top of the loop by the gas separator 71 and' may be put to any of a number of uses, as mentioned above. Each cycle of flow (once around the loop) extracts an amount of energy proportional to the weight difference

between the two columns (represented by the equation E = dW x h, in which dW is the difference in weight and h is the height of the column). The amount of power that can be obtained from the system depends upon the speed or time it takes to complete the stroke, i.e., the rate at which the work is done. Thus, the power is given by the equation P = dW x v, in which v is the speed of the fluid flow.

As the system continues to operate, the MHD 101 may generate more power than is needed to operate the electrolytic gas generator 51. When this occurs, electrical leads 45 may be attached to an external load suitable for using this excess power. Alternately, electrical leads 45 may be connected to a battery to store the power for later use. Accordingly, the system may be advantageously used to convert the thermal energy supplied •

" by thermal energy source 21 to both chemical energy in the form of gasses and electrical energy.

Alternative Embodiments General.System

Alternatively to using a single upflowing column 13 in the MHD loop 11, two or more columns 13a and 13b may be used, as shown in Figure 7. In this embodiment, one of the gasses produced by electrolytic gas generator 51, for example the oxygen may be injected into column 13a and the other gas, the hydrogen, may be injected into column

13b. In this way, both the gasses produced may be used to supplement the convective flow, while keeping the gasses separate. Since both gasses produced by the gas generator are used, the utility of the ' feedback of the electrical energy generated by the MHD 101 is enhanced. This embodiment requires at least two gas separators 71a and

71b (one to separate each gas out of the flow), and a gas injector 59a and 59b for each column 13a and 13b. The Electrolytic Gas Generator

As an alternative to using a liquid metal such as

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→ mercury in the MHD loop 11 and electrolysing a separate electrolyte in gas generator 51, an electrolyte may be circulated through the MED loop 11' (Figure 8) and passed through electrolytic gas generator 51' so that, the MHD working fluid itself is electrolyzed. From gas generator

51' part or all of the gasses may be injected into the column 13'. Pipe 57' allows whatever of the gasses are not injected into column 13' to be diverted and put directly to use.

Alternative Electrical Generator 101

As an alternative magnetohydrodynamic generator as the electric generator 101, any of a number of electric generators that generate electrical energy from a moving - fluid can be used. Fig. 9 is a schematic drawing of the system wit a general designation for the electrical generator 101. For example, the electrical generator 101 can be a homopolar or Faraday Disk type of generator. Another example of such an alternative electric generator is a common turbine generator, in which the moving fluid turns the blades of the turbine to generate electrical energy in a known fashion. Fig. 9 shows the system of Fig. 1 with a more general representation of the electric generator 101.

It would be apparent to those skilled in this art of electrical energy generation that any type of generator that converts the kinetic energy of a moving fluid to electric energy can be used as the means for generating, electric energy from the moving fluid.

First Alternative Flow Augmentation Means

Referring now to the embodiment of the system of the invention shown in Figure 10, the overall system is roughly the same as that described above, with a pair of substantially vertical flow conduits 13,15, an electric generator 101, and a gas generator 51 that uses the electric energy generated by the electric generator 101. The gas generator 51 and the electric generator 101 are

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connected by ' the electrical leads 43. The system again includes an energy input means 21, such as a thermal energy source or other means to begin the flow of fluid through the conduit, such as a pump.

Rather than injecting the gasses developed by the electrolytic gas generator 51 directly into the working fluid in the upflow column 13, the system of this alternative embodiment uses the gasses generated by the electrolytic gas generator 51 to pressurize a volatile fluid, which is then injected into the upflow tube 13, where it changes to its gas form and reduces the density of the working fluid to further increase the rate of flow of the working fluid through the conduit..

A pair of fluid containers 211,213 each have fluid inlets 215, fluid outlets 217, and gas inlets 219. Each of these inlets 215,219 and outlets 217 is controlled by a

^valve 221,223,225 to control the flow of fluid into and out of the container 211,213.

The gas from the gas generator 51 is alternately supplied to the first and second fluid containers 211,213. Initially, the fluid inlet valve 221 on the first fluid container 211 is opened and the first container is substantially filled with the volatile fluid from the reservoir 227. This volatile fluid readily changes from the liquid phase to the gas phase at relatively low temperatures, on the order of the temperature of the working fluid in the conduit loop. When the volatile luid enters the first container 211, it is in the liquid phase. After the first container 211 has been substantially filled with the fluid, the fluid inlet valve 221 is closed, and the gas inlet valve 225 is opened. The gas is supplied from the gas generator 51 to the gas inlet 219 at a high pressure, so the gas builds the pressure inside the container 211. When the pressure reaches a specified level, the fluid outlet valve 223 is opened, and the pressure inside the fluid container 211

-IB- drives the volatile fluid out of the first fluid container 211 through the injection conduit 55 and into the injection nozzle 59. The injection nozzle 59 is similar to the injection nozzle 59 of the embodiment shown in Fig. 1 and described above.

As the volatile fluid is injected into the upflow column of the fluid conduit 13, the fluid is transformed to its gas phase by the heat of the working fluid that surrounds the injection nozzle 59. As the volatile fluid is at a very high pressure as it enters the upflow tube 13 of the .conduit, the gas bubbles it forms are rather small. As the gas bubbles move up in the column with the upflowing fluid, these bubbles expand in size as the external pressure on them is less in the column 13 than it was in the injection conduit 55. These expanding bubbles further increase the flow of the working fluids through the conduit.

- While the first fluid container 211 is ' being pressurized, the fluid inlet valve 221 for the second fluid container 213 is opened and the volatile fluid is allowed to flow into the second fluid container '213 to substantially fill it. The second fluid container 213 is then pressurized in the same way as first fluid container 211 while the volatile fluid is being driven out of the -first fluid container 211.

While the second fluid container 213 is being pressurized, the first container 211 is again filled .with ' .the volatile fluid. As the volatile fluid is driven from the second fluid container 213, the first container 211 is again pressurized. • This alternating process continues indefinitely, using the two fluid containers 211,213 to maintain a constant flow of volatile fluid through the injection conduit 55 at a .high pressure. A mixer 233 where the two outlets 217 from the fluid containers 211,213 join ensures that the flow from the containers is properly alternated.

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Obviously, more than two of the fluid containers 211,213 may be used in a system that operates such as this to further increase the supply of the volatile fluid to the conduit.

To minimize the need for pumps and other expensive equipment, the fluid containers 211,213 are fed from the reservoir 227 that is at an elevation higher than the elevation of the fluid containers 211,213. In this way; when the fluid inlet valve 221 on one of the fluid containes 211,213 is open, the fluid will flow into the container by gravitational force, eliminating the need for a pump or other fluid moving apparatus to fill the containers.

To ensure an adequate high pressure supply of gas to pressurize the fluid containers 211,213, a gas accumulator 229 is connected to the output of the gas generator 51. This accumulator 229 collects the gas generated by the gas generator 51 and allows the gas to build up to a very high pressure. It is well known that the electrolysis process of gas generation can produce gasses at very high pressures without significant loss in efficiency or overall energy consumption. Thus, the gas accumulator 229 allows the pressure of gas to be built up before it is fed through the gas inlets 219 to the first and second fluid containers 211,213.

The gas separator 71 at the top of the upflow column 13 allows the gaseous volatile fluid to be removed from the conduit loop.

Second Alternative Flow .Augmentation Means Referring now to the embodiment of the system of the invention shown in Figure 11, the overall system is again roughly the same as that described above, with a pair of flow tubes .13, 15, an electric generator 101, and a gas generator 51 that uses the electric energy generated by the electric generator 101. The gas generator 51 and the electric generator 101 are connected by the electrical

leads 43. The system includes an energy input means 21, such as a thermal energy source or other means to begin the flow of fluid through the conduit, such as a pump. If the thermal energy source is used, then, as with the _ previously described system, the heat exchanger 31 is again necessary to remove the heat from the fluid to maintain the temperature differential between the portions of the fluid in each column.

Rather than using the gas generated by the gas 0 generator 51 to reduce the density of fluid in the upflow column.13, however, the embodiment shown in Figure 10 uses

. the gas generated by the gas generator 51 to build up pressure behind the fluid to drive the fluid through the conduit in an efficient manner. 5 To use the gas to propel the fluid through the conduit, a pair of fluid containers 211,213 each has a fluid inlet 215 and fluid outlet 217, in addition to a gas - inlet 219.- Each of these inlets 215,219 and outlets 217 is controlled by a valve 221,223,225 to control the flow 0 of fluid into and out of the container 211,213.

.The gas from the gas generator 51 is. supplied alternately to the first and second fluid containers 211,213. Initially, the fluid inlet valve 221 on the first fluid container 211 is opened and the first 5 container 211 is substantially filled with the system working fluid. Then the fluid inlet valve 221 is closed, and the gas inlet valve 225 is opened. The gas is

-supplie to the gas inlet 219 at a high pressure, so the gas builds the pressure inside the container 211. When 0 the pressure reaches a specified level, the fluid outlet valve 223 is opened, and the pressure inside the fluid container 211 drives the fluid out of the first fluid container 211 through the upflow tube 13 and down through the downflow tube 15 and the electric energy generator 5 101. As the flow is driven by the pressure, it is at a higher rate than the initial flow, thus increasing the

production of electric energy by the electric generator

101.

While the first fluid container 211 is being pressurized, the fluid inlet valve 221 for the second fluid container 213 is opened and the fluid is allowed to flow into the second fluid container 213 to substantially fill it. The second fluid container 213 is then pressurized in the same way as the first fluid container

211 while the fluid is being driven out of the first fluid container 211. .

While the second fluid container 213 is being pressurized, the first container 211 is again filled with fluid. As the fluid is driven from the second fluid container 213, the first container 211 is again pressurized. This alternating process continues indefinitely, using the two fluid containers 211,213 to maintain a constant flow of fluid through the conduit 13,15.

Obviously, more than two fluid containers may also be used in a system that operates such as this to further increase the fluid flow.

To minimize the need for pumps and other expensive equipment, the fluid containers 211,213 are fed from a reservoir 227 that is at the bottom of the downflow tube 15, and at an elevation higher than the elevation of the first and second fluid containers 211,213. In this way, when the fluid inlet valve 221 on one of the fluid containers 211,213 is opened, the fluid will flow into the container by gravitational force, eliminating the need for a pump or other fluid moving apparatus.

To ensure an adequate high pressure supply of gas to pressurize the first and second fluid containers 211,213 a gas accumulator 229 is connected to the output of the gas generator 51. This accumulator 229 collects the gas generated by the gas generator 51 and allows the gas to build up to a very high pressure. It is well known that

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the electrolysis process of gas generation can produce gasses at very high pressures without significant loss in efficiency or overall energy consumption. Thus, the gas accumulator 229 allows the pressure of gas to be . built up before it is fed through the gas inlets 219 to the first and second fluid containers 211,213.

A gas separator 71 at the top of the upflow column 13 allows any gas that has been introduced into the working fluid by the fluid flow augmentation to be removed before the working fluid flows downward through the second column

15 and the electric generator 101.

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