U.S. patent application number 09/859524 was filed with the patent office on 2002-01-17 for energy generating system using differential elevation.
Invention is credited to Alkhamis, Mohammed.
Application Number | 20020005042 09/859524 |
Document ID | / |
Family ID | 26941443 |
Filed Date | 2002-01-17 |
United States Patent
Application |
20020005042 |
Kind Code |
A1 |
Alkhamis, Mohammed |
January 17, 2002 |
Energy generating system using differential elevation
Abstract
A system generates energy using the difference in elevation
between an upper elevation (e.g., at the top of a mountain) and a
lower one (e.g., at or near the bottom of the mountain.) The system
includes a compressor located at the upper location which supplies
compressed gas through a conduit to a mixing chamber at the lower
elevation. A plurality of turbine-generator sets are located at
different elevations along the conduit for extracting energy from
the compressed gas. A control unit connected to the conduit
supplies pulses of the compressed gas to the mixing chamber for
mixing with mercury to produce a mercury-gas mixture. An injector
injects pulses of the mercury-gas mixture into a turbine so as to
impact against the turbine blades and drive the turbine.
Inventors: |
Alkhamis, Mohammed; (Riyadh,
SA) |
Correspondence
Address: |
LARSON & TAYLOR, PLC
1199 NORTH FAIRFAX STREET
SUITE 900
ALEXANDRIA
VA
22314
US
|
Family ID: |
26941443 |
Appl. No.: |
09/859524 |
Filed: |
May 18, 2001 |
Related U.S. Patent Documents
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Application
Number |
Filing Date |
Patent Number |
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09859524 |
May 18, 2001 |
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09251152 |
Feb 17, 1999 |
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09251152 |
Feb 17, 1999 |
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08887604 |
Jul 3, 1997 |
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5873249 |
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Current U.S.
Class: |
60/641.1 ;
60/643; 60/670 |
Current CPC
Class: |
F02C 6/14 20130101; F03G
3/00 20130101 |
Class at
Publication: |
60/641.1 ;
60/643; 60/670 |
International
Class: |
F03G 007/00; F01K
027/00; F01K 001/00 |
Claims
What is claimed:
1. A system for generating energy using the difference in elevation
between a relatively high elevation and a relatively low elevation,
said system comprising: compressor located at the relatively high
location for compressing a vapor form of a working medium into a
compressed gas; a first conduit for conveying said compressed gas
to said relatively low elevation; mixing chamber at said relatively
low elevation; mercury supply means for supplying mercury to said
mixing chamber; control means connected to said first conduit for
supplying pulses of said compressed gas to said mixing chamber for
mixing with said mercury to produce a mercury-gas mixture; a
turbine having turbine blades; injecting means for injecting pulses
of said mercury-gas mixture into said turbine so as to impact
against said turbine blades and drive the turbine; separator means
for recovering the mercury and gas from said turbine and for
separating the gas from the mercury; connector means for conveying
mercury separated from said gas to said mercury supply means; a
further conduit for conveying gas separated from the mercury to
said compressor; and a plurality of liquid turbine-generator units
each respectively located at different elevations along said first
conduit between said relatively high elevation and said relatively
low elevation, said units each comprising a liquid turbine driven
by said compressed gas and a generator driven by the associated
liquid turbine for supplying power to the remainder of the
system.
2. A system for generating energy as claimed in claim 1 wherein
said control means comprises a control valve connected to said
conduit and having an open state wherein said compressed gas is
supplied to said mixing chamber and a closed state wherein said
compressed gas is blocked from said mixing chamber, and an
electrical control means for providing periodical opening and
closing of said control valve to generate said pulses.
3. A system for generating energy as claimed in claim 2 wherein
said valve comprises a rotary valve.
4. A system for generating energy as claimed in claim 3 wherein
said mixing chamber includes an internal electric heater for
heating the mercury and gas supplied to said chamber.
5. A system for generating energy as claimed in claim 1 wherein
said injecting means includes a connection between said mixing
chamber and said turbine for increasing the rate of injection of
the mercury-gas mixture into said turbine.
6. A system for generating energy as claimed in claim 1 further
comprising heating means for heating the mercury prior to supplying
of the mercury to the mixing chamber.
7. A system for generating energy as claimed in claim 6 wherein
said heating means comprises at least one heater tank containing
mercury, and supply means for supplying gas from said separator
means into a bottom portion of said tank such that the gas bubbles
up through the mercury in the tank to thereby cause heating of the
mercury.
8. A system for generating energy as claimed in claim 7 wherein
said separator means comprises a separator tank containing mercury
and defining a mercury level, said separator tank including an
inlet connected to said turbine, an outlet disposed below said
mercury level for supplying mercury to said at least one heater
tank, and an outlet at an upper portion of said separator tank for
supplying gas to said at least one heater tank.
9. A system for generating energy as claimed in claim 8, wherein at
least one heater tank comprises a plurality of interconnected
heater tanks arranged in serial relation and disposed at different,
increasing elevations, in sequence, beginning with the heater tank
connected to said separator tank.
10. A system for generating energy as claimed in claim 9 further
comprising a gas pipe connector for connecting each heater tank to
the next adjacent heater tank in sequence, and an electrically
controlled, cyclically operated rotary valve connected in each gas
pipe connection.
11. A system for generating energy as claimed in claim 10 wherein
said rotary valves are controlled to cyclically operate at
different, decreasing rates beginning with said heater tank
connected to said separator tank.
12. A system for generating energy as claimed in claim 11 wherein
said rates decrease, in sequence, by a factor of two beginning with
said heater tank connected to said separator tank.
13. A system for generating energy as claimed in claim 7 wherein
said supply means comprises a connection conduit of a first
diameter connected to said separator tank and a plurality of
connecting pipes of diameters smaller than said first diameter
connected between said connector conduit and said bottom portion of
said heater tank.
14. A system for generating energy as claimed in claim 13 wherein
each of said pipes includes an outlet end opening into said heater
tank and an air filled float valve located at said outlet end.
15. A system for generating energy as claimed in claim 1 wherein
said mixing chamber includes an ovoid shaped cavity.
16. A system for generating energy as claimed in claim 15 wherein
said mixing chamber includes an ovoid shaped heater therein.
17. A turbine system including: a mixing chamber; mercury supply
means for supplying mercury to said mixing chamber; control means
for supplying a compressed gas to said mixing chamber for mixing
with said mercury to produce a mercury-gas mixture; a turbine
having turbine blades; and injecting means for injecting pulses of
said mercury-gas mixture into said turbine so as to impact against
said turbine blades and drive the turbine.
18. A system according to claim 1 further comprising: separator
means for recovering the mercury and gas from said turbine and for
separating the gas from the mercury; and connector means for
conveying mercury separated from said gas to said mercury supply
means.
Description
RELATIONSHIP TO OTHER APPLICATIONS
[0001] The present application is a continuation-in-part
application of Ser. No. 09/215,152, filed on Feb. 17, 1999, which
is itself a continuation-in-part of application of Ser. No.
08/887,604, filed on Jul. 3, 1997 and now U.S. Pat. No.
5,873,249.
FIELD OF THE INVENTION
[0002] The present invention relates to an improved energy
generating system which, in part, derives or generates energy based
on as large differential elevation between different parts of the
system.
BACKGROUND OF THE INVENTION
[0003] It is an understatement to say that an extremely large
amount of research has gone into developing existing energy
sources, as well as exploring alternative energy sources such as
solar, tidal and wind energy.
[0004] As indicated above, the present invention is concerned, in
part, with using the difference in elevation between different
parts of the system in generating energy. Patents of interest in
this particular field include the following U.S. Pat. Nos.:
3,953,971 (Parker); 5,255,519 (Katovitch); 4,760,706 (Nasser);
5,488,828 (Brossard); 4,318,275, (Brown et al); 4,187,686
(Pommier); and 1,085,703 (Rochelle).
[0005] Briefly considering these patents, the Parker patent
discloses a system for generating power wherein liquid stored at a
higher elevation travels down a conduit to a power generation unit
at a lower elevation. The liquid is then vaporized and heated
before traveling up a conduit back to the higher elevation where
the vapor condensed to a liquid for reuse. The Katovitch patent
discloses a power generation system wherein helium is utilized as a
working recycled fluid which is heated to convert the fluid to a
vapor form for powering a generator. The Nasser, Broassard, and
Brown et al patents each disclose a power generation system wherein
a coolant is evaporated at a lower position, allowed to rise via
tubing to a higher position, liquefied at the higher position, and
then allowed to flow down to the lower reposition where the liquid
drives a turbine connecting to a generator. The Pommier patent
discloses a power generation system wherein fluid is warmed at a
lower level to convert the fluid to a gas and cooled at an upper
level to convert the gas back to a fluid. The hydraulic pressure of
the liquid moving from the upper level to the lower level is used
to generate power. The Rochelle patent discloses a water motor
which utilizes a water, and gravity, to pull down buckets from an
upper elevation and thereby generate energy.
SUMMARY OF THE INVENTION
[0006] In accordance with the invention, an energy generating
system is provided which, in part, derives or generates energy
based on a large differential in elevation between different parts
of the system, e.g., between parts of the system located at or near
the top of a mountain and other parts of the system located at or
nears the bottom of the mountain. Among the suitable candidate
locations for the system is the mountain of Sarawat in the Kingdom
of Saudi Arabia which is a relatively high mountain having a steep
face, about 2400 m. above sea level.
[0007] In accordance with the invention, a system is provided for
generating energy using the difference in elevation between a
relatively high elevation and a relatively low elevation, the
system comprising: a compressor located at the relatively high
location for compressing a vapor form of a working medium into a
compressed gas; a first conduit for conveying the compressed gas to
the relatively low elevation; a mixing chamber at the relatively
low elevation; mercury supply means for supplying mercury to the
mixing chamber; control means connected to the first conduit for
supplying pulses of the mercury-gas mixture into the turbine so as
to impact against the turbine blades and drive the turbine;
separator means for recovering the mercury and gas from the turbine
and for separating the gas from the mercury; connector means for
conveying mercury separated from the gas to the mercury supply
means; and a further conduit for conveying gas separated from the
mercury to the compressor.
[0008] Preferably, the control means comprises a control valve
connected to said conduit and having an open state wherein the
compressed gas is supplied to said mixing chamber and a closed
state wherein the compressed gas is blocked from the mixing
chamber, and an electrical control means for providing periodical
opening and closing of the control valve to generate said pulses.
Advantageously, the valve comprises a rotary valve.
[0009] The mixing chamber preferably includes an internal electric
heater for heating the mercury and gas supplied to the chamber. The
injecting means preferably includes a connection between the mixing
chamber and the turbine for increasing the rate of injection of the
mercury-gas mixture into said turbine.
[0010] Preferably, the system further comprises heating means for
heating the mercury prior to supplying of the mercury to the mixing
chamber. The heating means preferably comprises at least one heater
tank containing mercury, and supply means for supplying gas from
the separator means to a bottom portion of the tank such that the
gas bubbles up through the mercury in the tank to thereby cause
heating of the mercury. Advantageously, the separator means
comprises a separator tank containing mercury and defining a
mercury level, the separator tank including an inlet connected to
said turbine, an outlet disposed below the mercury level for
supplying mercury to the at least one heater tank, and an outlet at
an upper portion of said separator tank for supplying gas to said
at least one heater tank.
[0011] In a preferred implementation of the embodiment described
above, at least one heater tank comprises a plurality of
interconnected heater tanks arranged in serial relation and
disposed at different, increasing levels or elevations, in
sequence, beginning with the heater tank connected to the separator
tank. The system preferably further comprises a gas pipe connector
for connecting each heater tank to the next adjacent tank in
sequence, and an electrically controlled, cyclically operated
rotary valve connected in each gas pipe connection. Advantageously,
the rotary valves are controlled to cyclically operate at
different, decreasing rates beginning with the heater to the
separator tank. Preferably, these rates decrease, in sequence, by a
factor of two, beginning with the heater tank connected to said
separator tank.
[0012] The supply means preferably comprises a connection conduit
of a first diameter connected to the separator tank and a plurality
of connecting pipes of diameters smaller than said first diameter
connected between the connector conduit and the bottom portion of
the heater tank. Advantageously, each of the pipes includes an
outlet end opening into the heater tank and an air filled float
valve located at the outlet end.
[0013] The mixing chamber preferably includes an ovoid shaped
cavity. Advantageously, the mixing chamber includes an ovoid shaped
heater therein.
[0014] Other features and advantages of the invention will be set
forth in, or apparent from, the detailed description of the
preferred embodiments of the invention which is found
hereinbelow.
BRIEF DESCRIPTION OF THE DRAWINGS
[0015] The single FIGURE in the drawings is a schematic diagram of
an energy generating system in accordance with a preferred
embodiment of the invention.
DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0016] Referring to the drawings, there is shown a schematic
representation of an energy generating system in accordance with a
first embodiment of the invention. The system includes a compressor
10 located at or near the top of a mountain or, more generally, at
a high relative differential elevation with respect to the rest of
the system, the latter being indicated as a unit denoted 12.
[0017] Compressed gas is conveyed from the compressor 10 down the
mountain through a supply line 14 to a mixing chamber 16 of unit
12. Connected in the supply line 14 at various spaced points along
the descent thereof down the mountain are turbine-generator units
17 described in more detail hereinbelow. A main valve 18 connected
in supply line 14 upstream of chamber 16 serves, when closed, to
block the gas in line 14 from reaching chamber 16. An electrically
driven rotary ball valve 20, connected in line 14 between valve 18
and chamber 16, is driven by an electric motor control unit 21
which also drives additional rotary ball valves described
below.
[0018] Mixing chamber 16, which is, as shown, preferably
"egg-shaped" or elliptical, includes an electric heater 22 which is
also preferably egg-shaped, as shown, and which, in use, heats the
contents of chamber 16. The volume of the chamber 16, or, stated
differently, the distance between the longitudinal center line of
the chamber and the inner wall surface, is selected to be the
greatest at the center of the chamber and the smallest near the
chamber outlet. An injector nozzle 24 receives compressed gas from
line 14 as well as hot mercury from an injector unit 26. The heater
22 heats both the gas and mercury in chamber 16 and the hot mixture
is supplied from chamber 16 in shock waves or pulses controlled by
rotary valve 20. In particular, the timing and duration of these
shock waves or pulses is controlled by opening and closing times of
valve 20 under the control of the electric motor control unit 21
referred to above.
[0019] A turbine 28 is connected to chamber 16 through a venturi
connection 30, and is driven by the shock waves, or pulses, of the
hot mixture of mercury and gas referred to above. The venturi
connection 30 accelerates the flow rate of the mixture. The
distance between the turbine 28 and mixing chamber 16 should be
chosen to provide the maximum rate of speed for the pulses of the
mercury and gas mixture so as to exert the optimum force on the
turbine 28. Further, the blades 28a of the turbine 28 should be
shaped so as to maximize the driving force produced thereon by the
pulses. The overall operation of this aspect of the system is
roughly similar to that of an air gun wherein pulses of air are
used to generate propulsive forces. A power take-off shaft for
turbine 28 is indicated at 28a.
[0020] The compressed gas and mercury in turbine 28 are recycled
from the turbine to a separation tank 32 wherein the gas rises to
the top and the mercury, indicated at M, collects at the bottom of
the tank. Separation tank 12 is connected to a system of further
heater tanks, generally denoted 34. These tanks are of different
sizes and are disposed at different levels, as shown. In the
embodiment illustrated, four tanks 36, 38, 40 and 42 are employed.
The mercury M from separation tank 32 is transferred in the other
tanks, in sequence, through a series of connecting pipes 44.
Similarly, gas is made to flow or pass from separation tank 32
through the other tanks, in sequence, through a further series of
connecting pipes 46. An electrically-operated rotating ball valve
48 is connected to the output of each of the tanks 32, 36, 38, 40
and 42 at one end of pipes 46 and while, at the other end, each of
the pipes 46 branches into a plurality of small thin pipes 50 which
extend into the corresponding tank. As indicated by circle 46a and
circle 50a, the diameter of pipe 46 is greater than that of thin
pipes 50.
[0021] As noted above, each of the tanks is disposed, as viewed
from the left of FIG. 1, at a higher level than the next adjacent
tank so as to minimize the quantity of mercury required. Float
valves, one of which is indicated schematically at 52, are filled
with air to reduce the pressure exerted by the mercury and thus
assist the gas to travel upwardly through the collected mercury to
the space thereabove. The float valves 52, with their floating
balls, control the flow of mercury for each tank. The valves 52
reduce the high pressure of the mercury on the small pipes 50
themselves to enhance the travel of the gas through the mercury.
Thin curved pipes corresponding to pipes 50 can also be employed.
The curvature of such pipes can be used to reduce the pressure of
the mercury thereon in the manner of the curve of a medical
thermometer.
[0022] As the gas travels through the mercury in the form of
bubbles, each bubble will be under high pressure (thirteen times
the pressure of water) thereby creating friction and generating
heat. The heat increased in the following tanks in sequence, i.e.,
tanks 36, 38 and 40, and is absorbed in the relatively shallow
mercury pool in the last tank 42.
[0023] The aforementioned rotary valves 48 associated with the
heater tanks 46 control the pressure from the mixing chamber 16
wherein shock waves are produced to assist in injecting the gas and
mercury mixture. Preferably, the rotational speed of each valve 48
will differ and the speeds will vary in a predetermined pattern. In
a specific implementation, the valve 48 for separation tank 32 will
rotate at 960 revolutions per minute (rpm), that for tank 36 will
rotate at 480 rpm, that for tank 38 at the 240 rpm, that for tank
42 at 120 rpm, and that for the final tank 40 at 60 rpm. In this
way, hammering waves or pulses are created at twice the rate as the
previous tank to help in forcing or pushing the gas through the
mercury.
[0024] The gas from the last tank 42 in the series is transported
through piping indicated at 54 to the compressor 10 at the top of
the mountain for compression and continuation of the cycle. It will
be, of course, appreciated that other units may be located at the
top of the mountain along with condenser (compressor) 10 including
a liquid reservoir or gas storage tank (not shown) and control
valving (not shown). These units may, of course, also include a
power supply 10a such as a battery or gasoline driven
motor-generator for supplying electrical power to the compressor
10.
[0025] As is believed to be evident from the foregoing description
of the overall system, in operation, gas under pressure from
compressor 10 is routed down through pipeline or supply conduit 14
to the level of unit 12 wherein the gas is under high pressure. The
gas is supplied to mixing chamber 16 along with mercury injected by
injector unit 26 for mixing and heating by heater 22. The hot
mercury-gas mixture is caused to flow, in the form of pulsations or
shock waves, to turbine 28 wherein pulses of the mixture impact on
the blades 28a of the turbine 28, and thus drive the turbine. The
gas and mercury mixture is then collected and transported to the
separation tank 32 wherein the gas it separated from the mercury
and is caused to bubble through the mercury in the series of heater
tanks 36, 28, 40 and 42 thereby creating frictional forces and
heating the mercury. The heated mercury is ultimately delivered to
the injector 26 for injection into mixing chamber 16 while the
separated gas is returned to compressor 10.
[0026] Turning now to liquid turbine-generator units 17 mentioned
above, these units are installed at regularly spaced points (e.g.,
every 500 meters in a specific embodiment) along the descent of the
supply pipe 14 down, e.g., the mountain and each comprises a liquid
turbine 56 and an electrical generator 58 driven by the associated
turbine 56. This approach breaks the high pressure generated as the
liquefied gas travels down pipe 14 and avoids the serious problem
created by the heat that would otherwise be generated by the high
pressure flow. The turbines 56 each convert the gravitational force
produced by the liquefied gas into a rotational force for driving
the associated generator 58. The high pressure supply line or
conduit 14 is of a diameter chosen such that the required pressure
is produced while the frictional forces exerted on the conduit
walls are minimized. The electrical energy produced by generators
58 is then used to provide power for the rest of the system. For
example, as indicated in the drawings, electrical power is provided
to compressor 10 and to motor control unit 21. Thus, energy
produced as the result of differences in elevation is converted
into electrical energy to assist in driving the overall system.
[0027] Heat is necessary at the end of the process taking place at
the bottom of the mountain to convert the liquefied gas into a
gaseous state for travel through line 54 back to compressor 10. In
the first instance, heat from the liquefied gas supply line 14 is
used in driving turbine 28 and to generate surplus energy in
accordance with the basic aim of the system as described above. The
heat needed is further provided in a natural way, by compression,
using the remaining pressure to inject the gas into mercury thereby
causing the gas to be heated by the bubbling thereof through the
mercury as discussed hereinbefore. The heated gas will then easily
travel upwardly and will lose heat during this travel before
reaching the compressor 10 at the completion of the overall cycle.
Thus, the energy generated at various points along the way is
efficiently utilized.
[0028] Additional heat for the system is provided by a series of
heat exchangers 60 which derive heat from relatively warm sea
water, indicated at 62, or another body of such water. This part of
the system can be similar to the system disclosed in U.S. Pat. No.
5,400,619 (Husseiny et al) and can use the principles of that
patent to provide potable water, with the compressor of the
Husseiny et al patent being located at the upper part of the
mountain. The pipes 64 between the heat exchangers 60 preferably
increase in diameter so as to accommodate the high pressures
generated. Alternatively, pressure extracting tanks (not shown) can
be located between the heat exchangers.
[0029] The problem of the heat created as the liquefied gas travels
down the supply pipe 14 could also be combated by cooling of the
pipe 14. This can be done by employing an outer shell or conduit
and using some of the gas from the main conduit to provide cooling
of the space between the main and outer conduits. A liquid turbine
at the bottom of the mountain would then be used to generate
electrical energy for the heater and other electrical uses.
[0030] It is also noted that cooling rather than heating can be
provided by reversing the heating process described above. Mercury
can be used to compress the gas and drawing or sucking the gas
through the mercury enables the use of the low boiling point gasses
employed in conventional cooling systems. The cost of such cooling
can be decreased and the needed compressible forces reduced because
use is made of the natural compression exerted by mercury on a
single bubble.
[0031] It will be appreciated that there is a significant
difference between the energy consumed in recovering the helium
gas, as here, and the refining of helium, since the latter
generally requires purifying a mixture of rare gases and this takes
substantial energy. In the plastics industry, a conventional four
stage liquefying system is used to recover helium gas at low
cost.
[0032] Although the present invention has been described to
specific exemplary embodiments thereof, it will be understood by
those skilled in the art that variations and modifications can be
effected in these exemplary embodiments without departing from the
scope and spirit of the invention.
* * * * *