[0001] This invention relates to a hydraulic air compressor. In particular, the invention
relates to a hydraulic air compressor in which a gas can be compressed to a desired
pressure at the temperature of the water used in the compressor. The energy of the
compressed air can be put to a variety of uses.
[0002] Hydraulic air compressors are veil known and have been used on a substantial scale
in the past to compress air using the energy possessed by a head of water (under pressure).
[0003] Whilst the hydraulic air compressor has attractions, it was superceded by the internal
combustion engine and cheap sources of other energy, at that time, mainly because
of the inefficiencies of the velocity flow principle adopted by all to entrain the
air.
[0004] However in the modern world these alternatives are becoming less viable, and the
attractive features of the hydraulic air compressor are once again worth investigation.
[0005] One problem with the design of the conventional hydraulic air compressor was that
the drive head of the compressor was regarded merely as that head of water existing
between the inlet and tail race of the compressor.
[0006] In fact, the excess of mass per unit volume of water in the down pipe of the compressor
over the mass per unit volume of water in the tail race, or 'up pipe' is critical
in the determination of the water velocity, since the drive head varies in accordance
with the degree to which air has been entrained in the falling column of water.
[0007] Different degrees of air entrainment result in variations in the mass of the column
and therefore the height to which the drive column must be above the tail race outlet
for the same velocity and pressure.
[0008] The invention provides a hydraulic air compressor having a drive and compression
down pipe, an air inclusion chamber at the head of the down pipe arranged to be fed
with water from a water source, an air separating chamber at the bottom of the down
pipe, an air pipe leading from the separating chamber, an upwardly directed water
return pipe leading from the separating chamber, means at the exit of the return pipe
for pressurising water flowing from the return pipe and for directing the water into
the air inclusion chamber when the air inclusion chamber is not fed with water from
the water source the air inclusion chamber being arranged so that water enters it
in a vortex and so that a venturi effect is created in the water stream and having
an air inlet arranged so that, in use, air is drawn into the air inclusion chamber
as a result of the vortical motion of the water; the venturi effect due to the velocity
of the issuing jet, the inertia of which, permits the introduction of air into the
air inclusion chamber at pressures higher than atmospheric.
[0009] Freferably, the air inclusion chamber tapers downwardly and includes a double wall
with a gap between the walls, the gap being open at the bottom of the chamber, air
inlet communicating with the gap, and tangential inlet or inlets to the tcp of the
chamber for the introduction of water flowing from the water source or from the pressurising
means, as the case may be.
[0010] It is intended that the compressor will serve to provide a supply of gas compressed
by a liquid to the hydrostatic head at the point of separation when the temperatures
of the gas will be that of the liquid. If the water source is not able to supply water
at a sufficient head to maintain the supply of compressed air, then the pressurising
means will be actuated to ensure that an adequate flow of water to the air inclusion
chamber is provided.
[0011] In one application of the hydraulic air compressor, the compressed air is fed directly
to the combustion chamber of a gas turbine or ram jet, so that no filters or turbine
powered compressor stage is required. In another application of the invention, the
compressed air from the hydraulic air compressor is fed to the chambers of a pneumatic
displacement pump.
[0012] The pump may be arranged to inject water into the combustion chamber of a gas turbine.
[0013] In addition, the pump can be used for dosing water with chemicals such as chlorine
or soda-ash, or for irrigation.
[0014] Another important feature of the hydraulic air compressor is that it compresses air
isothermally.
[0015] If this isothermally compressed air is allowed to expand adiabatically in doing work,
it will produce sub-zero temperatures which can be used to provide a freezer capability.
[0016] The invention will now be further described, by way of example, with reference to
the accompanying drawings, in which:
Figure 1 is a schematic view of a hydraulic air compressor installation. The source
of water being from behind a dam wall or the pneumatic displacement pump shown in
the sump.
Figure 2 is an enlarged view of part of the installation shown in Figure 1.
Figure 3 shows a schematic view of a pneumatic displacement pump suitable for use
with a hydraulic air compressor of the invention.
[0017] The compressor shown in Figure 1 is indicated generally by reference numeral 1.
[0018] It is fed with water 2 retained behind a dam wall 3. The water 2 passes out from
behind the dam wall 3 through a feed pipe 4 to an air inclusion chamber 7 at the head
of a drive and compression down pipe 5.
[0019] As can be seen in Figure 2, there are tangential inlets from the feed pipe 4 to the
chamber 7.
[0020] The tangential inlets 6 serve to impart a swirl to the jet of water entering the
chamber 7.
[0021] The water moved downwardly in this chamber and air enters through an inlet 8.
[0022] The air is entrained by the water stream in the form of bubbles, so that when the
narrow cylindrical section of the pipe 5 is reached the water is impregnated with
bubbles of air.
[0023] The air is carried to the bottom of the pipe 5 to an air/water separating chamber
9.
[0024] As the air/water mixture descends, the air is compressed.
[0025] When the descent of the air/water column is checked in the chamber 9, the direction
of the flow is reversed.
[0026] The air separates from the water and passes upwardly via an air pipe 10.
[0027] The water passes around a baffle 11 and returns upwardly through a return pipe 12.
[0028] The pipe 12 feeds into a surge tank 13 in which is arranged a pump 14. The pump 14
serves to raise water into the air inclusion chamber 7 via a tangantial inlet 15 when
there is an inadequate flow of water through the feed pipe 4.
[0029] When there is an inadequate flow of water through the pipe 4 under sufficient head,
water will overflow from the chamber. In this case, the valve 51 between the pump
and the chamber is closed, and a valve in the feed pipe 4 can be operated to control
inlet water pressure.
[0030] If there is an inadequate flow through the pipe 4, a valve 50 in the pipe 4 is closed
and the pump 14 is actuated to raise water to the air inclusion chamber 7.
[0031] A suitable design velocity can, therefore, be maintained at all times in the compressor
so that a correct supply of compressed air is produced.
[0032] The pressure of water from the pump is controlled by operation of the valve 51 and
this permits air at a pressure higher than atmospheric at the venturi throat.
[0033] The drive head of the compressor is determined by the excess of the mass of the water/air
mixture per unit volume in the pipe 5 over that in the pipe 12.
[0034] This drive head must be sufficient to ensure that the velocity in the down pipe 5
is greater than the velocity at which air bubbles would rise in the water column if
it were stationary.
[0035] The maximum drive head possible is designated in Figure 1 by the symbol H
d, which represents the elevation of the top of the pipe 5 over that of the maximum
hydrostatic height of the pipe 12.
[0036] The compression of the air is dependent on the hydrostatic head of the water in fne
return pipe 12, represented in Figure 1 by the symbol H.
[0037] The design and function of the air inclusion chamber 7 is of critical importance
to the successful operation of the hydraulic air compressor of the invention.
[0038] There are a number of factors which contribute to the efficiency of air entrainment
in the stream of water entering the chamber. Firstly, the voluted entry of the water
through the inlets 6 or 15 (depending on whether the water is supplied from storage
behind the
dam wall 3 of is supplied via the pump 14) causes a swirl in the water stream.
[0039] This swirling or vortical motion of the water serves to draw air into the water stream.
[0040] Also, the turbulent nature of the water as it enters the chamber 7 is conducive to
the introduction of air.
[0041] In combination with these factors the venturi effect created as the water passes
the throat section at the bottom of the chamber 7 acts to increase air entrainment.
[0042] As a result of the swirl and of the turbulent nature at speed of the flow, the water
may form into droplets with the result that entrainment is enhanced since the air
can enter the stream above zero gauge pressure assisted by the venturi effect for
uniform distribution throughout the body of water.
[0043] In addition, the inertia of the issuing jet at the venturi throat enables the entrainment
of air at pressure substantially above atmospheric pressure.
[0044] Air which has already been compressed can therefore be recycled via the hydraulic
air compressor for further compression from a volume equal to that of the chamber
from which liquid is being displaced.
[0045] The actual form of one type of air inclusion chamber 7 is shown in Figure 2.
[0046] The chamber has an upper cylindrical portion 40 and a lower frustro- concial portion
41.
[0047] Within the portion 41 there is a shorter member 42 of fustro-conical shape so that
there is a gap between the walls of the portion 41 and the member 42.
[0048] The air inlet 8 is in communication with this gap 43.
[0049] A further important feature of the invention is the fact that the air can actually
be cooled down while undergoing compression in the compressor.
[0050] The compression of the air can be considered to be sub-isothermal. In one experiment
which has been conducted, the water had an inlet temperature of 15,5
oC while ambient temperature was 21,1 C. The air temperature was thus some 5,6°C lower
than the ambient or inlet air temperatures.
[0051] A modification to the compressor which is not shown in the drawings involves the
use of a second air/water separating chamber part-way up the return pipe 12.
[0052] The air which separates from the water in the chamber 9 is oxygen deficient, since
oxygen will have become dissolved in the water at the high pressure involved in the
operation of the hydraulic air compressor of the invention.
[0053] The inclusion of a second separating chamber allows for the separation of oxygen
rich air at a pressure determined by the hydrostatic head existing between the water
level in the second separating chamber and the upper level of the return pipe 12.
[0054] In addition, it is proposed to provide an excess air relief pipe for the compression
section of the pipe 5 so that uniform flow through the pipe will not be interrupted
by blow back when volume of gas compressed exceeds draw off.
[0055] The surplus could provide a freezer capability.
[0056] The particular advantage of having a pressurised feed to produce a constant drive
head at the top of the pipe is that it is then possible to have a constant flow compressor
in which the rate of flow down the pipe 5 is maintained at a steady level.
[0057] Pressurised feed can be provided by a conventional centrifugal pump as shown in Figure
2.
[0058] Preferably however, the pressurisation is provided by a pump arrangement with twin
pneumatic displacement chambers as shown schematically in Figure 1.
[0059] In this arrangement, air displaced from the pneumatic chambers of the pump is fed
to the air inclusion chamber 7.
[0060] The principle of operation of such an arrangement can be understood from the description
of the application of the hydraulic compressor ) to a pneumatic displacement pump
which follows.
[0061] The capacity of the surge tank 13 as measured from the top of the pump 14 to the
top of the tank should be at least 10% more than the total volume of the air pipe
10 and the excess air relief pipe between the chamber 9 and the top of the pump, or
a separate relief tank could be provided.
[0062] The hydraulic air compressor of the invention has a number of important applications:
HYDRAULIC AIR COMPRESSOR AND GAS TURBINE.
[0063] A conventional gas turbine drives its own adiabatic compressor stage and the air
must be filtered.
[0064] As a result, up to 70% of the turbine effort may be expended in powering the air
compression stage, so hat only 30 % of the effort is available for useful work.
[0065] In addition, the high temperatures encountered in a conventional adiabatic compressor
stage can have the effect of limiting the permissible compression ratio.
[0066] Also, the compressor stage represents a considerable bulk and weight factor.
[0067] It is therefore proposed to use a hydraulic air compressor to provide a supply of
filtered compressed air, so that the conventional compressor stage and filters can
be done away with.
[0068] The pressure available from the hydraulic air compressor of the invention may be
substantially greater than those available from the conventional compressor stage.
[0069] The compressed air from the hydraulic air compressor can be fed directly at exact
pressure required by the combustion chamber of a ram jet or turbine, and can be fed
to the combustion chamber, after passing through a heat exchanger, at the best temperature.
[0070] In the combustion chamber, fuel is burnt in the oxygen enriched compressed air environment
to produce hot compressed gases which are then expanded adiabatically through a turbine
stage.
[0071] The resulting energy can be used for electrical generation or the operation of other
devices.
[0072] Because the gas turbine proposed does not have to power its own compressor, there
can be a considerable increase in efficiency over conventional turbines and a saving
in first cost.
[0073] Efficiency is further improved by regeneration.
[0074] It is anticipated that the amount of fuel necessary for the firing functions will
be some 1,4 times that which would be expended in the standard designed output of
the turbine.
[0075] Nevertheless, it is anticipated that the power output from this turbine could be
three times that achievable with the standard turbine. ) Because the hydraulic air
compressor can produce filtered air at very high pressures, it may be possible to
expand this air to some extent through a turbine which would replace the conventional
filter and adiabatic compressor in a gas turbine.
[0076] This should still further increase the efficiency of the turbine, and could be carried
out in a simple way merely be reversing the blades of the compressor.
[0077] The adiabatic expansion of the air through what was compressor blading producing
extremely low temperatures which can be used for freezing purposes, due to the energy
expended in asaiating the gas turbine and 0 precipitated water could be drained off
at appropriate stages of adiabatic expansion.
HYDRAULIC AIR COMPRESSOR AND PNEUKATIC DISPLACEMENT PUMP.
[0078] A typical pump is shown in Figure 3.
[0079] This has chambers 21 and 22 each of which has an inlet 23, 24 for
5 high pressure air, an outlet 25, 26 for water, a water feed pipe 27, 28 and an air
evacuation pipe 29, 30.
[0080] Both the inlets 23 and 24 are connected to the air pipe 10 of the hydraulic air compressor,
and a two-way valve 31 can be operated to feed the compressed air either to the inlet
23 or to the inlet 24. 30 The operation of the other valves will become clear from
the following description of operation.
[0081] When compressed air is passed through the inlet 23 to the chamber 21, the outlet
25 is opened and valves in the pipes 27 and 29 are closed.
[0082] The compressed air in the upper part of the chamber 21 therefore pushes the water
out through the outlet 25, and to a common water line 32. At the same time, the chamber
22, having exhausted to atmospheric pressure, or recycled is being recharged with
water via the line 28. The outlet 26 is closed, the inlet 24 is closed but the air
pipe 30 is open.
[0083] Water enters at a relatively low pressure through the pipe 28 and displaces the air
in the top of the chamber 22.
[0084] As stated previously, it is preferred to use a pump of this general nature to raise
water from the surge tank 13 to the air inclusion chamber 7 with air displaced from
the empty chamber also returned to the air inclusion chamber 7.
[0085] In this case, the displacement or air can be aided by the suction generated in the
air inclusion chamber 7 of the compressor which can serve to suck the air out of the
upper part of the chamber 22. In any case, the pressure of the air to the air mixing
chamber 7 can be higher than atmospheric because of the inertia of the jet issuing
from the venturi orifice.
[0086] When 'the chamber 21 is nearly empty, the chambers are switched over and compressed
air is passed to the inlet 24 so that the chamber 22 which is now full of water, can
be pumped out by the air. Whilst this is happening the chamber 21 is being refilled.
One can therefore get a continuous feed of water under pressure through the line 32.
[0087] The pump can be used to pump irrigation water using eg. the overflow from surge tank
13 or to provide any sort of pumping facility as pumping from mines, wells, boreholes,
lakes or even shallow swamps, to any head.
[0088] The compressed air could also be used to inject water into the combustion chamber
of a gas turbine or ram jet as described in the preceding section of this specification,
to ensure atomisation and therefore to produce greater power from the turbine, or
for the injection of chemicals such as chlorine or soda-ash into water to make it
potable. The air from the injector pump exhaust is at very low temperature.
[0089] An advantage of the use of pneumatic displacement pump for the pressurisation of
a liquid is that the air is filtered and the liquid uncontaminated with oil etc.
[0090] In addition, the nature of the pressurisation which takes place is suitable for the
production of liquid velocities for the transportation of solids in pipelines.
HYDRAULIC AIR COMPRESSOR TO PROVIDE FREEZER TEMPERATURES.
[0092] Gases such as A5 NH
3 (anhydrous ammonia) can be delivered to distant points from any remo te source by
condensing the gas to liquid wherever required.
1. A hydraulic air compressor having a drive and compression down pipe, an air inclusion
chamber at the head of the down pipe arranged to be fed with water from a water source,
an air separating chamber at the bottom of the down pipe, an air pipe leading from
the separating chamber, an upwardly directed water return pipe leading from the separating
chamber,means at the top of the return pipe for pressurising water flowing from the
return pipe and for directing the water into the air inclusion chamber when the air
inclusion chamber is not fed with water from the water source, the air inclusion chamber
being arranged so that water enters it in a vortex and a venturi effect is created
in the water stream and having an air inlet arranged so that, in use, air is drawn
into the air inclusion chamber as a result of the vortical motion of the water and
the venturi effect created by the velocity of the issuing jet and also the blocking
effect at the nozzle (orifice) because of the inertia of the issuing jet which permits
entry of air at pressures well above atmospheric.
2. A hydraulic air compressor according to Claim 1, in which the air inclusion chamber
tapers downwardly and includes a double wall with a gap between the walls, the gap
being open at the bottom of the chamber an air inlet communicating with the gap, and
tangential inlets to the top of the chamber for the introduction of water flowing
from the water source or from the pressurising means, as the case may be.
3. A hydraulic air compressor according tc either one of the preceding claims, including
a further separating chamber arranged in the path of the upwardly directed return
pipe.
4. A hydraulic air compressor according to any one of the preceding claims, including
an excess air relief pipe which is designed to spill water from the relief pipe into
a relief water tank; if the relieved air is cut off to achieve an expansion ratio
of 1 to 6 from air at 15°C in the air/water chamber then a temperature of minus 100oC can be obtained.
5. A hydraulic air compressor according to any one of the preceding claims, in which
the pressurising means includes a pneumatic displacement pump arranged at the exit
of the water return pipe.
6. A hydraulic air compressor according to Claim 5, including means for directing
air displaced from the pneumatic displacement pump to the air inlet of the air inclusion
chamber.
7. A hydraulic air comprssor according to any one of Claims 1 to 4 in which fne pressurising
means includes a pump arranged at the exit of the water return pipe.
8. A hydraulic air compressor according to any one of the preceding claims, including
valves for controlling the flow of water from the pressurising means to the air inclusion
chamber or from the water source to the air inclusion chamber.
9. A hydraulic air compressor according to any one of the preceding claims, arranged
in combination with a gas turbine or ram jet to provide compressed air to the combustion
chamber of the turbine or to the coumbustion chamber or a ram jet for heating or producing
steam for whatever purpose or high temperature gas for gas turbines.
10. A hydraulic air compressor according to Claim 9, in which the gas turbine is arranged
to power a generator of electricity or similar devices.
11. A hydraulic air compressor according to any one of Claims 1 to 8 in combination
with a pneumatic displacement pump having two chambers arranged to be filled alternatively
with liquid and having means for the introduction of compressed air selectively from
the hydraulic air compressor to each chamber in turn to expel liquid in the chamber.
12. A hydraulic air compressor according to Claim 11, in which water separated from
the air in the hydraulic air compressor is fed to the air inclusion chamber from the
water source alternatively by the chambers of the pneumatic displacement pump.
13. A hydraulic air compressor according to either one of Claims 11 or 12, including
means for direoting water expelled from the chambers of the pneumatic displacement
pump into the combustion chamber of a gas turbine.
14. A hydraulic air compressor according to Claim 11 in which the liquid is dosing
chemicals for water treatment and the pump is arranged to inject the chemical into
the water.
15. A hydraulic air compressor according to either one of Claims 11, 12 or 13 including
means for dirscting water into a water main.