Technical Field
[0001] The present disclosure relates generally to the field of electricity storage and
more particularly to the storage of electricity in the form of thermal energy. The
present disclosure is especially concerned with pumped heat electricity storage (PHES).
Specific embodiments relate to a thermal energy storage system.
Technical Background
[0002] Further penetration of fluctuating renewable energy production requires economic
solutions for bulk electricity storage. Today's leading technology is Pumped Hydro
Storage (PHS). A possible alternative is Compressed Air Energy Storage (CAES). Whilst
PHS requires the right topography (mountains), CAES relies on the presence of specific
geological underground structures, such as salt caverns. Other forms of energy storage
include batteries and flywheels.
[0003] Pumped Heat Electricity Storage (PHES) has been proposed as an alternative storage
technique. During charging a PHES system pumps heat from a low temperature reservoir
to a high temperature reservoir, it therefore operates as a heat pump. During discharging
the high temperature heat is used to drive a power cycle whilst the residual heat
is rejected into the low temperature reservoir. The obvious advantage of such a system
is that the electricity is stored only under the form of heat or thermal energy, i.e.
it requires only some kind of thermally isolated containment that is independent of
geology or topography.
[0004] An implementation of PHES based on air or other non-condensing gases is described
in
US 2010/257862 A1. During charging this system is basically an air heat pump. Air or another non-condensing
gas is compressed which causes it to heat up. The thermal energy is passed to a high
temperature thermal energy store. The now cold compressed gas is expanded back to
the original pressure and cools down far below ambient temperature. The cold expanded
air is heated back up to approximately ambient temperature by cooling a cold thermal
energy store. After charging the electricity is stored under the form of heat at different
temperature levels. During discharging low pressure air is cooled in the low temperature
thermal energy store and compressed to a higher pressure level. The compressed air
then picks up thermal energy from the hot thermal energy store before it is expanded
in a turbine operatively connected to an electrical generator for electricity generation.
The losses that accumulate during charging and discharging have to be rejected against
the environment. This can happen at different points, most obviously at the exhaust
of the turbine.
[0005] Some drawbacks of this non-condensing PHES system have to be mentioned. During charging
and discharging there are always two turbomachines active: a hot compressor and a
cold turbine during charging, a cold compressor and a hot turbine during discharging.
Therefore component efficiencies of these turbomachines have a large impact on the
overall electrical-to-electrical (i.e. round-trip electrical) efficiency. Furthermore,
this PHES system requires turbomachines, heat exchangers and thermal energy stores
to operate at temperatures far below zero, which makes material selection a critical
factor. The capital expenditure for the turbomachines is proportional to the sum of
the power of the components, while the charging power is related to the difference
in power of the hot compressor and cold turbine. Similarly, the discharging power
is given by the difference in power of the cold compressor and hot turbine while the
capital expenditure is proportional to the sum of the power of the components. Therefore,
specific costs may be high. Finally, the non-condensing PHES system cannot produce
any power once the hot and the cold thermal energy stores are emptied. This is the
same as for an adiabatic compressed air energy storage (A-CAES) system where no power
can be generated if there is no pressurised air in the cavern. Non-condensing PHES,
A-CAES or batteries and flywheels are pure electricity storage devices and cannot
deliver power if they have not been charged before. Although this is commonly accepted,
it is a major drawback since expensive hardware is installed but cannot help if renewable
energy sources such as wind fail to produce electricity for a few days.
[0006] Some of theses drawbacks are at least partially mitigated by the thermoelectric energy
storage system described in
WO 2010/020480 A2 which employs a heat exchanger to transfer thermal energy between a condensable working
fluid and a sensible heat thermal storage medium circulating between cold and hot
storage tanks. Thermal energy is transferred from the working fluid to the thermal
storage medium during a charging cycle and is transferred from the thermal storage
medium to the working fluid during a discharging cycle in which electrical energy
is generated by expansion of the heated working fluid in a turbine. The condensable
working fluid is heated and compressed to a supercritical state during both the charging
and discharging cycles and this maximises the round-trip electrical efficiency of
the system.
[0007] Round-trip electrical efficiency is increased further in the thermoelectric energy
storage system described in
WO 2011/045282 A2 due to the provision of an internal heat exchanger. The internal heat exchanger preheats
the working fluid during both the charging and discharging cycles, thereby maximising
system efficiency.
[0008] There remains a need for an improved thermal energy storage system which achieves
a high round-trip electrical efficiency with minimal capital expenditure.
Summary of the Disclosure
[0009] According to one aspect, there is provided a thermal energy storage system comprising:
a first thermal energy store arrangement having an upper operating temperature (T1max) and a lower operating temperature (T1min);
a second thermal energy store arrangement having an upper operating temperature (T2max) and a lower operating temperature (T2min), wherein the upper operating temperature (T2max) of the second thermal energy store arrangement is less than or equal to the lower
operating temperature (T1min) of the first thermal energy store arrangement; and
a working fluid circuit containing a working fluid for circulation through the first
and second thermal energy store arrangements;
the thermal energy storage system having a charging cycle in which thermal energy
is transferred from the circulating working fluid to the first and second thermal
energy store arrangements and a discharging cycle in which thermal energy is transferred
from the first and second thermal energy store arrangements to the circulating working
fluid.
[0010] The first thermal energy store arrangement may be regarded as a high-temperature
thermal energy store arrangement whilst the second thermal energy store arrangement
may be regarded as a medium-temperature thermal energy store arrangement. The provision
of the second, medium-temperature, thermal energy store arrangement enables the storage
temperature of the first, high-temperature, thermal energy store arrangement to be
increased. More particularly, the upper and lower operating temperatures (T1
max, T1
min) of the first thermal energy store arrangement can be increased because the thermal
energy storage is shared between the first and second thermal energy store arrangements.
Increasing the upper and lower operating temperatures of the first thermal energy
store arrangement enables a suitable and commercially available high-temperature thermal
energy storage medium to be used in the first thermal energy store arrangement.
[0011] The first thermal energy store arrangement may utilise a first, high-temperature,
thermal energy storage medium to receive and store thermal energy. The first thermal
energy storage medium is typically a liquid and may advantageously be a molten salt
such as a nitrate salt or a carbonate salt, or a mixture of molten salts. Other forms
of storage medium could, however, be used such as thermal oil, water, sand, gravel
or any other suitable particulate material. The first thermal energy storage medium
is capable of absorbing heat in a highly efficient manner, i.e. with a small temperature
approach, at almost constant heat capacity from the working fluid.
[0012] The second thermal energy store arrangement may utilise a second, low-temperature,
thermal energy storage medium to receive and store thermal energy. The second thermal
energy storage medium may be pressurised water.
[0013] The first thermal energy store arrangement may comprise first and second storage
tanks, for example high-temperature and medium-temperature storage tanks, for the
first thermal energy storage medium and may comprise a heat exchange device arranged
between the storage tanks to transfer thermal energy between the working fluid and
the first thermal energy storage medium as it flows through the heat exchange device
between the storage tanks. The high temperature storage tank may have an upper operating
temperature (T1
max) between 300 and 600°C and the medium temperature storage tank may have a lower operating
temperature (T1
min) between 200 and 400°C.
[0014] The second thermal energy store arrangement may comprise first and second storage
tanks, for example medium-temperature and low-temperature storage tanks, for the second
thermal energy storage medium and may comprise a heat exchange device arranged between
the storage tanks to transfer thermal energy between the working fluid and the second
thermal energy storage medium as it flows through the heat exchange device between
the storage tanks. The medium temperature storage tank may have an upper operating
temperature (T2
max) between 100 and 300 °C and the low temperature storage tank may have a lower operating
temperature (T2
min) between 20 and 100 °C.
[0015] The system may further comprise first and second heat exchangers and a compressor.
The first and second heat exchangers may be operable during the charging cycle to
transfer thermal energy to the circulating working fluid to heat the working fluid
prior to compression in the compressor. The compressor may be operable during the
charging cycle to compress the heated working fluid prior to circulation through the
first and second thermal energy store arrangements. The compressor may be arranged
to compress the working fluid to a supercritical state.
[0016] The working fluid may be a condensable working fluid. The condensable working fluid
may be an organic fluid such as an alkane. The condensable organic working fluid may
advantageously be a C
3 alkane, a C
4 alkane or a C
5 alkane.
[0017] The first heat exchanger may be operable during the charging cycle to transfer thermal
energy from the ambient environment to the circulating working fluid to heat the circulating
working fluid. The first heat exchanger may be operable during the discharging cycle
to transfer thermal energy from the circulating working fluid to the ambient environment
to cool the circulating working fluid. The first heat exchanger is typically arranged
to transfer thermal energy between ambient temperature sea water or river water and
the circulating working fluid.
[0018] The first heat exchanger may be an evaporator/condenser that is operable during the
charging cycle as an evaporator to evaporate the circulating condensable working fluid
and operable during the discharging cycle as a condenser to condense the circulating
condensable working fluid.
[0019] The system may include a first flow divider/combiner valve between the first and
second thermal energy store arrangements. The first flow divider/combiner valve may
be operable during the charging cycle to divide the circulating working fluid into
a first fluid flow to the second heat exchanger to transfer thermal energy from the
first fluid flow to the circulating working fluid output from the first heat exchanger;
and a second fluid flow to the second thermal energy store arrangement to transfer
thermal energy from the second fluid flow to the second thermal energy store arrangement.
The first fluid flow may comprise between about 60 and 90% of the total flow of circulating
working fluid whilst the second fluid flow may comprise between about 10 and 40% of
the total flow of circulating working fluid.
[0020] The system may include a second flow divider/combiner valve which may be operable
during the charging cycle to combine the first and second fluid flows respectively
from the second heat exchanger and the second thermal energy store arrangement.
[0021] The system may further comprise an expander which may be operable during the charging
cycle to expand the circulating working fluid output from the second flow divider/combiner
valve. The expander may be a liquid expander which may be arranged to expand the circulating
working fluid to a pressure above which evaporation of the working fluid occurs.
[0022] The system may further comprise a throttle which may be operable during the charging
cycle to reduce the pressure of the circulating working fluid output from the expander.
The throttle may be arranged to reduce the pressure of the expanded circulating working
fluid at least to level at which the working fluid separates into a vapour and a liquid
phase. The throttle thus closes the reversible cycle and after throttling into the
wet region, the circulating working fluid is returned to the first heat exchanger.
[0023] The system may further comprise a third heat exchanger which may be operable during
the charging cycle to transfer thermal energy to the circulating working fluid output
from the second heat exchanger prior to compression of the heated circulating working
fluid in the compressor. The third heat exchanger may be operable during the charging
cycle to transfer thermal energy from the circulating working fluid output from the
first thermal energy store arrangement to the circulating working fluid output from
the second heat exchanger prior to compression of the heated circulating working fluid
in the compressor.
[0024] The system may further comprise a turbine which may be operable during the discharging
cycle to expand heated circulating working fluid. The second flow divider/combiner
valve may be operable during the discharging cycle to divide the circulating working
fluid into a first fluid flow to the second heat exchanger to enable the transfer
of residual thermal energy from the circulating working fluid output from the turbine
to the first fluid flow to thereby heat the first fluid flow; and a second fluid flow
to the second thermal energy store arrangement to enable the transfer of thermal energy
from the second thermal energy store arrangement to the second fluid flow to thereby
heat the second fluid flow. The first fluid flow may comprise between about 60 and
90% of the total flow of circulating working fluid whilst the second fluid flow may
comprise between about 10 and 40% of the total flow of circulating working fluid.
The first flow divider/combiner valve may be operable during the discharging cycle
to combine the heated first and second fluid flows output respectively from the second
heat exchanger and the second thermal energy store arrangement.
[0025] The third heat exchanger may be operable during the discharging cycle to transfer
residual thermal energy from the circulating working fluid output from the turbine
to the combined flow of circulating working fluid output from the first flow divider/combiner
valve. The circulating working fluid is, thus, preheated during the discharging cycle
before it is supplied to the first thermal energy store arrangement for further heating.
[0026] The compressor may be an adiabatic compressor. The system may include an electric
motor which is arranged to drive the compressor during the charging cycle. The turbine
may be an adiabatic turbine. The turbine may be operatively associated with an electrical
generator to generate electrical power during the discharging cycle.
Brief Description of the Drawings
[0027]
Figure 1 is schematic illustration of a charging cycle of a first embodiment of a
thermal energy storage system;
Figure 2 is schematic illustration of a discharging cycle of the thermal energy storage
system illustrated in Figure 1; and
Figure 3 is a schematic illustration of a discharging cycle of a second embodiment
of a thermal energy storage system similar to that illustrated in Figure 2.
Detailed Description of Embodiments
[0028] Embodiments will now be described by way of example only and with reference to the
accompanying drawings.
[0029] Referring initially to both Figures 1 and 2, there is shown a first embodiment of
a thermal energy storage system in the form of a pumped heat electricity storage (PHES)
system. Electricity is stored in the form of thermal energy during the charging cycle
illustrated in Figure 1 in which the system operates as a heat pump. Electricity is
generated by recovering thermal energy during the discharging cycle illustrated in
Figure 2 in which the system operates as a Rankine cycle.
[0030] The thermal energy storage system comprises a reversible closed cycle working fluid
circuit 8 in which the circulating working fluid is a condensable organic working
fluid. The condensable organic working fluid may typically be a C
3 alkane such as propane, a C
4 alkane such as butane or a C
5 alkane such as pentane.
[0031] The system comprises a first heat exchanger in the form of an evaporator/condenser
10 which is arranged to transfer thermal energy between ambient temperature sea water
or river water and the circulating working fluid. The system comprises a second heat
exchanger in the form of a recuperator 12, a third heat exchanger in the form of a
recuperator 30, a first (high-temperature) thermal energy store arrangement 16, a
second (medium-temperature) thermal energy store arrangement 32, a liquid expander/pump
18 and a throttle 20. The system further comprises an adiabatic compressor 14 which
is driven by a motor M during the charging cycle illustrated in Figure 1 and an adiabatic
turbine 22 operatively connected to a generator G so that electricity can be generated
during the discharging cycle illustrated in Figure 2.
[0032] The high temperature thermal energy store arrangement 16 utilises molten salt as
a sensible heat storage medium and includes an insulated hot salt storage tank 24,
an insulated relatively warm salt storage tank 26 and a heat exchanger 28 to transfer
heat between the working fluid and the molten salt as the molten salt flows between
the hot and warm salt storage tanks 24, 26. During the charging cycle, the heat exchanger
28 transfers heat from the circulating working fluid to the molten salt as the molten
salt flows from the relatively warm salt storage tank 26 to the hot salt storage tank
24. During the discharging cycle, the heat exchanger 28 recovers heat from the hot
molten salt as it flows from the hot salt storage tank 24 to the relatively warm salt
storage tank 26 and transfers the recovered heat to the working fluid as it is circulated
through the heat exchanger 28.
[0033] The medium temperature thermal energy store arrangement 32 utilises pressurised water
as a thermal energy storage medium and includes a relatively warm insulated pressurised
water storage tank 34, a relatively cool pressurised water storage tank 36 and a heat
exchanger 38 to transfer heat between the working fluid and the pressurised water
as the pressurised water flows between the warm and cool water storage tanks 34, 36.
During the charging cycle, the heat exchanger 38 transfers heat from the circulating
working fluid to the pressurised water as the pressurised water flows from the relatively
cool water storage tank 36 to the relatively warm water storage tank 34. During the
discharging cycle, the heat exchanger 38 recovers heat from the warm pressurised water
as it flows from the relatively warm water storage tank 34 to the relatively cool
water storage tank 36 and transfers the recovered heat to the working fluid as it
is circulated through the heat exchanger 38.
[0034] The high-temperature thermal energy store arrangement 16 operates at a higher temperature
than the medium-temperature thermal energy store arrangement 32. In one implementation
of the system illustrated in Figures 1 and 2, molten salt is stored in the hot salt
storage tank 24 at an upper operating temperature (T1
max) in the region of 440°C and in the relatively warm salt storage tank at a lower operating
temperature (T1
min) in the region of 290°C, whereas pressurised water is stored in the relatively warm
water storage tank 34 at an upper operating temperature (T2
max) in the region of 240°C and in the relatively cool water storage tank 36 at a lower
operating temperature (T2
min) in the region of 50°C.
[0035] The system includes first and second flow divider/combiner valves 40, 42 which are
selectively operable to divide and combine the flow of circulating working fluid into
first and second fluid flows. More particularly, during the charging cycle the first
flow divider/combiner valve 40 divides the flow of circulating working fluid into
a first fluid flow that is supplied to the recuperator 12 and a second fluid flow
that is supplied to the medium-temperature thermal energy store arrangement 32 whilst
the second flow divider/combiner valve 42 combines the first and second fluid flows.
Conversely, during the discharging cycle the second flow divider/combiner valve 42
divides the flow of circulating working fluid into a first fluid flow that is supplied
to the recuperator 12 and a second fluid flow that is supplied to the medium-temperature
thermal energy store arrangement 32 whilst the first flow divider/combiner valve 40
combines the first and second fluid flows.
[0036] The operation of the thermal energy storage system in the charging and discharging
cycles will now be explained in more detail.
Charging Cycle - Electricity Storage
[0037] As indicated above, the system operates as a heat pump during the charging cycle
illustrated in Figure 1. In more detail, the condensable organic working fluid is
evaporated in the evaporator 10 by absorbing heat from ambient sea water or river
water. The resulting vapour is then preheated in the recuperators 12, 30 by absorbing
residual heat recovered from the high pressure side of the closed cycle. The preheated
vapour is compressed in the adiabatic compressor 14, driven by the motor M, to supercritical
conditions, i.e. so that it has a temperature and pressure in the supercritical range.
[0038] The supercritical working fluid is passed to the heat exchanger 28 of the high-temperature
thermal energy store arrangement 16 where heat is transferred to the molten salt as
it flows from the relatively warm salt storage tank 26 to the hot salt storage tank
24. Because the working fluid is compressed in the compressor 14 to supercritical
conditions, the supercritical working fluid entering the heat exchanger 28 has an
almost constant heat capacity that is well matched to the molten salt. This maximises
the efficiency of the transfer of thermal energy to the molten salt.
[0039] After exiting the heat exchanger 28, the circulating working fluid is supplied to
the recuperator 30 which recovers residual heat from the circulating working fluid
and transfers the recovered residual heat as described above to the working fluid
in the low pressure side of the cycle to preheat the low pressure working fluid prior
to delivery to the compressor 14.
[0040] The high-pressure working fluid output from the recuperator 30 is then divided by
the first flow divider/combiner valve 40 into first and second fluid flows. The first
fluid flow, comprising approximately 60 to 90% of the total flow of working fluid,
is supplied to the recuperator 12 which recovers residual heat from the first fluid
flow and transfers the residual heat as described above to the working fluid in the
low pressure side of the cycle to preheat the working fluid before it is further preheated
by the recuperator 30 as described above. The second fluid flow comprising the remaining
proportion of the total flow of working fluid is supplied to the heat exchanger 38
of the medium temperature thermal energy store arrangement 32 where heat is transferred
to the pressurised water as it flows from the relatively cool water storage tank 36
to the relatively warm water storage tank 34. The split of the working fluid flow
is advantageous since the heat capacity of the working fluid in the high pressure
side of the closed cycle is larger than that of the low pressure vapour in the low
pressure side of the closed cycle.
[0041] The first and second fluid flows output respectively from the recuperator 12 and
the medium-temperature thermal energy store arrangement 32 are combined by the second
flow divider/combiner valve 42 to once again form a single flow of working fluid.
[0042] In order to close the cycle, it is necessary to reduce the pressure of the working
fluid to a sufficient level that it evaporates. The necessary pressure reduction is
achieved by firstly expanding the pressurised working fluid in the liquid expander
18. The working fluid is then throttled by the throttle 20 into the wet region before
the working fluid is returned to the evaporator 10.
Discharging Cycle - Electricity Generation
[0043] During the discharging cycle illustrated in Figure 2 in which electricity is generated,
the system operates as an organic Rankine cycle. In more detail, the condensable organic
working fluid is condensed in the condenser 10 by rejecting heat to ambient temperature
sea water or river water. The condensed working fluid is then pumped to a supercritical
pressure by the liquid pump 18.
[0044] The condensed working fluid is then divided by the second flow divider/combiner valve
42 into first and second fluid flows. The first fluid flow comprising approximately
60 to 90% of the total flow of working fluid is supplied to the recuperator 12 where
it is preheated using the residual exhaust heat in the working fluid output from the
turbine 22 on the low pressure side of the cycle. The second fluid flow comprising
the remaining proportion of the total flow of condensed working fluid is supplied
to the heat exchanger 38 of the medium-temperature thermal energy store arrangement
32 where heat is transferred from the pressurised water to the working fluid as the
pressurised water flows from the relatively warm water storage tank 34 to the relatively
cool water storage tank 36.
[0045] The first and second fluid flows output respectively from the recuperator 12 and
the medium-temperature thermal energy store arrangement 32 are combined by the first
flow divider/combiner valve 40 to once again form a single flow of working fluid.
[0046] The recombined flow of circulating working fluid is further preheated in the recuperator
30 using the residual exhaust heat in the working fluid output from the turbine 22
on the low pressure side of the cycle. The preheated working fluid is then supplied
to the heat exchanger 28 of the high-temperature thermal energy store arrangement
16 where heat is transferred from the molten salt to the circulating working fluid
as the molten salt flows from the hot salt storage tank 24 to the relatively warm
salt storage tank 26.
[0047] The heated working fluid is expanded in the turbine 22. This drives the electrical
generator G to generate electricity. After expansion in the turbine 22, residual waste
heat from the working fluid is transferred via the recuperators 30, 12 to the high
pressure side of the cycle to preheat the high pressure working fluid in the manner
described above. The working fluid is finally returned to the condenser 10 to close
the cycle.
[0048] There may be circumstances in which insufficient heat is stored in the high-temperature
and medium-temperature thermal energy store arrangements 16, 32 to enable the system
illustrated in Figures 1 and 2 to generate electricity during the discharging cycle.
In such circumstances, external heat input(s) Q as shown in the system illustrated
in Figure 3 can be used to raise the temperature of the molten salt and pressurised
water in the high-temperature and medium-temperature thermal energy store arrangements
16, 32 for recovery during the discharging cycle. The external heat input(s) Q could,
for example, be provided by means of a combustion process, or a renewable energy source
such as a geothermal or solar heat source, and each of the high-temperature and medium-temperature
thermal energy store arrangements 16, 32 includes a heat exchange arrangement 44,
46 via which thermal energy from the external heat input(s) can be transferred respectively
to the molten salt and pressurised water.
[0049] The use of a first, high-temperature, thermal energy store arrangement 16 and a comparatively
smaller scale second, medium-temperature, thermal energy store arrangement 32 is advantageous
because the circulating working fluid has different heat capacities in the low pressure
and supercritical high pressure conditions. In particular, the high pressure working
fluid possesses too much thermal energy during the charging cycle and requires too
much thermal energy during the discharging cycle. The second, medium-temperature,
thermal energy store arrangement 32 overcomes this problem by temporarily storing
excess thermal energy during charging and supplying it during discharging. This arrangement,
along with the recuperator 30, allows the operating temperature of the high-temperature
thermal energy store arrangement 16 to be shifted to a level that is favourable with
regard to the storage medium. For example, in embodiments in which the condensable
organic working fluid is butane, the operating temperature range can be shifted from
approximately 100°C in the relatively warm salt storage tank 26 and 270°C in the hot
salt storage tank 24 to values of approximately 290°C and 450°C respectively. These
higher temperatures are within the operating range of economic molten salts used in
solar thermal power plants, whereas operating temperatures in the range of 100°C to
270°C can only be achieved using molten salts with the expensive addition of lithium
nitrates.
[0050] As indicated above, the thermal energy storage system according to embodiments of
this disclosure operates as an organic Rankine cycle during the discharging cycle
and such cycles are well-known in the industry. The system also operates as a heat
pump during the charging cycle. Accordingly, the density of the working fluid vapour
after the evaporator 10 is an important factor in order to have a reasonably sized
compressor 14. It is believed that methane and ethane have a too high pressure and
density for a reasonable range of evaporation temperatures. N-butane and iso-butane
have a pressure in the order of 1 to 2 bar with densities of 3 to 4 kg/m
3 at evaporation temperature (2 to 3 bar in front of the compressor 14). N-pentane
and iso-pentane have a lower vapour pressure and density that is, however, comparable
at high temperature to the properties of the butanes at low temperature. Propane has
a higher vapour pressure and density that is, however, comparable at low temperature
to the properties of the butanes at high temperatures.
[0051] In summary it appears that a C
3 alkane (propane), C
4 alkanes (n-butane or isobutane) or C
5 alkanes (n-pentane or isopentane) could be used as the organic working fluid for
the system according to embodiments of the present disclosure. The selection could
be adapted to the evaporation temperature. Assuming river or sea water cooling/heating
as described above, a lighter blend (C
3 or C
4) could be used in winter and a heavier blend (C
4 or C
5) could be used in summer.
[0052] Although exemplary embodiments have been described in the preceding paragraphs, it
should be understood that various modifications may be made to those embodiments without
departing from the scope of the appended claims. Thus, the breadth and scope of the
claims should not be limited to the above-described exemplary embodiments. Each feature
disclosed in the specification, including the claims and drawings, may be replaced
by alternative features serving the same, equivalent or similar purposes, unless expressly
stated otherwise.
[0053] For example, the recuperator 30 (third heat exchanger) is not essential and could
be omitted from the embodiments described with reference to Figures 1 to 3. The hot
and warm salt storage tanks 24, 26 could be replaced by a single thermocline storage
tank. Likewise, the warm and cool water storage tanks 34, 36 could alternatively or
additionally be replaced by a single thermocline storage tank.
[0054] Unless the context clearly requires otherwise, throughout the description and the
claims, the words "comprise", "comprising", and the like, are to be construed in an
inclusive as opposed to an exclusive or exhaustive sense; that is to say, in the sense
of "including, but not limited to".
1. A thermal energy storage system comprising:
a first thermal energy store arrangement (16) having an upper operating temperature
(T1max) and a lower operating temperature (T1min);
a second thermal energy store arrangement (32) having an upper operating temperature
(T2max) and a lower operating temperature (T2min), wherein the upper operating temperature (T2max) of the second thermal energy store arrangement is less than or equal to the lower
operating temperature (T1min) of the first thermal energy store arrangement (16); and
a working fluid circuit (8) containing a working fluid for circulation through the
first and second thermal energy store arrangements (16, 32);
the thermal energy storage system having a charging cycle in which thermal energy
is transferred from the circulating working fluid to the first and second thermal
energy store arrangements (16, 32) and a discharging cycle in which thermal energy
is transferred from the first and second thermal energy store arrangements (16, 32)
to the circulating working fluid.
2. A system according to claim 1, wherein the first thermal energy store arrangement
(16) utilises a first thermal energy storage medium and the second thermal energy
store arrangement (32) utilises a second thermal energy storage medium which is different
from the first thermal energy storage medium.
3. A system according to claim 2, wherein the first thermal energy storage medium is
a molten salt or a mixture of molten salts and the second thermal energy storage medium
is pressurised water.
4. A system according to claim 2 or claim 3, wherein the first thermal energy store arrangement
(16) comprises high-temperature and medium-temperature storage tanks (24, 26) for
the first thermal energy storage medium and a heat exchange device (28) arranged between
the storage tanks (24, 26) to transfer thermal energy between the circulating working
fluid and the first thermal energy storage medium as it flows through the heat exchange
device (28) between the storage tanks (24, 26), the high temperature storage tank
(24) having an upper operating temperature (T1max) between 300 and 600°C and the medium temperature storage tank (26) having a lower
operating temperature (T1min) between 200 and 400°C.
5. A system according to any of claims 2 to 4, wherein the second thermal energy store
arrangement (32) comprises medium-temperature and low-temperature storage tanks (34,
36) for the second thermal energy storage medium and a heat exchange device (38) arranged
between the storage tanks (34, 36) to transfer thermal energy between the circulating
working fluid and the second thermal energy storage medium as it flows through the
heat exchange device (38) between the storage tanks (34, 36), the medium temperature
storage tank (34) having an upper operating temperature (T2max) between 100 and 300°C and the low temperature storage tank (36) having a lower operating
temperature (T2min) between 20 and 100°C.
6. A system according to any preceding claim, further comprising first and second heat
exchangers (10, 12) and a compressor (14), wherein:
the first and second heat exchangers (10, 12) are operable during the charging cycle
to transfer thermal energy to the circulating working fluid to heat the working fluid
prior to compression in the compressor (14); and
the compressor (14) is operable during the charging cycle to compress the heated working
fluid prior to circulation through the first and second thermal energy store arrangements
(16, 32).
7. A system according to claim 6, wherein the system includes a first flow divider/combiner
valve (40) between the first and second thermal energy store arrangements (16, 32)
which is operable during the charging cycle to divide the circulating working fluid
into:
a first fluid flow to the second heat exchanger (12) to transfer thermal energy from
the first fluid flow to the circulating working fluid output from the first heat exchanger
(10); and
a second fluid flow to the second thermal energy store arrangement (32) to transfer
thermal energy from the second fluid flow to the second thermal energy store arrangement
(32).
8. A system according to claim 7, wherein the system includes a second flow divider/combiner
valve (42) which is operable during the charging cycle to combine the first and second
fluid flows respectively from the second heat exchanger (12) and the second thermal
energy store arrangement (32).
9. A system according to any of claims 6 to 8, further comprising a third heat exchanger
(30) operable during the charging cycle to transfer thermal energy to the circulating
working fluid output from the second heat exchanger (12) prior to compression of the
heated circulating working fluid in the compressor (14).
10. A system according to claim 9, wherein the third heat exchanger (30) is operable during
the charging cycle to transfer thermal energy from the circulating working fluid output
from the first thermal energy store arrangement (16) to the circulating working fluid
output from the second heat exchanger (12) prior to compression of the heated circulating
working fluid in the compressor (14).
11. A system according to any of claims 8 to 10, further comprising a turbine (22) operable
during the discharging cycle to expand heated circulating working fluid, wherein the
second flow divider/combiner valve (42) is operable during the discharging cycle to
divide the circulating working fluid into:
a first fluid flow to the second heat exchanger (12) to enable the transfer of residual
thermal energy from the circulating working fluid output from the turbine (22) to
the first fluid flow; and
a second fluid flow to the second thermal energy store arrangement (32) to enable
the transfer of thermal energy from the second thermal energy store arrangement (32)
to the second fluid flow.
12. A system according to claim 11, wherein the first flow divider/combiner valve (40)
is operable during the discharging cycle to combine the first and second fluid flows
output respectively from the second heat exchanger (12) and the second thermal energy
store arrangement (32).
13. A system according to claims 9, 11 and 12 or claims 9, 10, 11 and 12, wherein the
third heat exchanger (30) is operable during the discharging cycle to transfer residual
thermal energy from the circulating working fluid output from the turbine (22) to
the combined flow of circulating working fluid output from the first flow divider/combiner
valve (40).
14. A system according to any preceding claim, wherein the working fluid is a condensable
working fluid, preferably a condensable organic working fluid.
15. A system according to claim 14, wherein the condensable organic working fluid is an
alkane, preferably a C3 alkane or a C4 alkane or a C5 alkane.