BACKGROUND OF THE INVENTION
Field of the Invention
[0001] The present invention relates to a device configuring a heat pump cycle in which
a two-stage compressor including a low stage compression part and high stage compression
part is provided, the heat pump cycle making use of NH
3 as a main circuit heat transfer medium; whereby, three kinds of heat extracting (or
supplying) circuits for extracting (or supplying) heat from the main circuit toward
the outside of the main circuit are provided; the temperature of the heat carrier
at the outlet of each heat extracting (or supplying) circuit is in a higher temperature
range (60 to 75 °C), a medium temperature range (40 to 60°C), or a lower temperature
range (-15 to 10°C) ; the heat extracting at each heat exchanging part can be performed
at the same time, and the refrigeration capacity as well as the coefficient of performance
is enhanced in comparison with the conventional level.
Background of the Invention
[0002] Patent Reference 1 (
JP2000-249413A) discloses a two-stage compression refrigerating device according to the conventional
technology; the explanation as to the configuration thereof is now given. A refrigerating
device 010 depicted in Fig. 7 is used as a business use refrigerator, a household
refrigerator, an ice plant, a refrigerator for a showcase and so on. A refrigerant
circuit 020 configures a two-stage compression heat pump cycle having a main circuit
02M provided with a high stage compressor 021H and a low stage compressor 021L. Further,
the two-stage compression heat pump cycle is provided with an intermediate cooler
022 so that the temperature of the refrigerant gas emitted by the low stage compressor
is reduced.
[0003] In other words, in the two-stage compression heat pump cycle, the gas discharge side
of the low stage compressor 021L is connected to the intermediate cooler 022 via a
refrigerant piping 023; the intermediate cooler 022 is connected to the high stage
compressor 021H via the refrigerant piping 023. Further, the discharge side of the
high stage compressor 021H is connected to a heat exchanger (a heat source side heat
exchanger) 024. The heat exchanger 024 may be, for instance, an air-cooled condenser,
and heat exchange is performed between the outdoor open-air and the main circuit refrigerant
so that the refrigerant is condensed; hereby, a heat carrier other than the outdoor
open-air may be used as a heat transfer medium absorbing heat from the refrigerant
in the main circuit; namely, the heat carrier other than the outdoor open-air is warmed
while passing through a pipe for the heat carrier in the heat exchanger 024.
[0004] From the heat exchanger (a heat source side heat exchanger) 024, a heat exchanging
part 022a in the intermediate cooler 022, an expansion valve 025, a heat exchanger
(a cooled object side heat exchanger) 026 are connected in the sequential order in
series via the refrigerant piping 023. Further, the heat exchanger 026 is, for instance,
configured so that the heat exchange between the air in a refrigerated warehouse and
the refrigerant in the refrigerant piping 023 is performed at the heat exchanger 026;
thereby, the refrigerant evaporates so as to cool the air in the warehouse. In addition,
the heat exchanger (a to-be-cooled object side heat exchanger) 026 is connected to
the gas inlet side of the low stage compressor 021L the refrigerant piping 023 so
that the evaporated refrigerant is guided to the low stage compressor 021L.
[0005] The passage of the refrigerant at the outlet of the heat exchanger (the heat source
side heat exchanger) 024 is branched out into a branched passage 030 from the main
circuit of the refrigerant; the branched passage 030 is provided with an auxiliary
expansion valve 031 on the downstream side of the heat exchanger 024, on a part way
of the branched passage 030; the refrigerant outlet side of the auxiliary expansion
valve 031 is connected to the intermediate cooler 022 via the branched passage 030.
The refrigerant in a liquid state streams through the branched passage 030 from the
auxiliary expansion valve 031 into the intermediate cooler 022; thereby, the refrigerant
streaming into the intermediate cooler 022 through the branched passage 030 evaporates
so as to super-cools (sub-cools) the liquid state refrigerant in the main circuit
02M and cools the refrigerant gas discharged by the low stage compressor 021L and
guided into the intermediate cooler 022 through the refrigerant piping 023.
[0006] The cooling workings (or working processes) of the two-stage compression refrigerating-device
are now explained based on a Mollier chart of Fig. 8. In the first place, the low
refrigerant gas in a state of the point A in Fig. 8 is sucked into the low stage compressor
021L and discharged from the compressor 021L; the discharged gas streams, via the
refrigerant piping 023, into the intermediate cooler 022 where the gas from the compressor
021L is cooled by the refrigerant from the branched passage 030, as is described later.
[0007] In the second place, the cooled gas in a state of the point C of Fig. 8 streams into
the high stage compressor 021H where the gas is compressed up to a state of the point
D. Further, the gas sucked by the compressor 021H is discharged from the compressor
021H and streams into the heat exchanger (a heat source side heat exchanger) 024;
thereby, heat exchange is performed between the gas streaming into the heat exchanger
024 and another heat carrier that absorbs heat from the gas. The gas streaming into
the heat exchanger 024 is cooled in the heat exchanger 024 so that the state of the
gas reaches a state of the point E (in a liquid state) and the gas is condensed.
[0008] The condensed liquid refrigerant at a high streams into two passages: one is the
main circuit 02M and the other is the branched passage 030. The pressure of the liquid
refrigerant streaming through the branched passage 030 is reduced at the auxiliary
expansion valve 031 to a state of the point F, and the liquid refrigerant streams
into the intermediate cooler 022. On the other hand, the liquid refrigerant passing
through the main circuit 02M streams through the heat exchanging part 022a in the
intermediate cooler 022. In the intermediate cooler 022, the liquid refrigerant passing
through the branched passage 030 evaporates so as to cool the refrigerant gas discharged
by the low stage compressor 021L (the state of the refrigerant in the main circuit
changes from point B to the point C in the intermediate cooler 022) as well as cools
the liquid refrigerant passing through the heat exchanging part 022a in the intermediate
cooler 022 (the state of the refrigerant in the main circuit changes from point E
to the point G in the intermediate cooler 022).
[0009] On the other hand, the refrigerant gas that evaporates in the intermediate cooler
022 joins, at a state of the point C, the refrigerant gas that is discharged by the
low stage compressor 021L and streams into the intermediate cooler 022; then, the
confluence refrigerant gas streams through the refrigerant piping 023 and is sucked
into the high stage compressor 021H. On the other hand, the pressure (at a state of
the point G) of the liquid refrigerant at the heat exchanging part 022a in the main
circuit 02M is reduced to the pressure at a state of the point H, just on the downstream
side of the expansion valve 025; then, the liquid refrigerant from the expansion valve
025 enters the heat exchanger (a to-be-cooled object side heat exchanger) 026 where
heat exchange is performed between the liquid refrigerant and a heat carrier such
as the air inside the refrigerated warehouse; and, the liquid refrigerant evaporates
so as to absorb the heat from the air inside the ice warehouse. After the evaporated
refrigerant leaves the heat exchanger 026, the state of the refrigerant returns back
to the state of the point A; thus, the refrigerant gas sucked into the low stage compressor
021L.
[0010] As described thus far, in removing heat from the heat transfer medium in the higher
temperature range or the medium temperature range, the heat carrier (of the heat removing
side) is warmed-up mainly by the sensible heat or the latent heat of the gas (heat
transfer medium) discharged by a compressor that configures the heat pump cycle; according
to this conventional approach, the heat removal from the heat amount (the enthalpy
drop from the gas phase to the condensed liquid phase) of the heat transfer medium
is performed in two processes, namely, in a process of the higher temperature process
(B to C) and a process of the medium temperature process (E to G) . When it is taken
into consideration that the heat removal in the higher temperature process is performed
mainly by use of the sensible heat of the heat-transfer medium, the heat amount that
can be removed in the higher temperature process is at most 20% level of the total
heat amount (the enthalpy drop from the gas phase to the condensed liquid phase) of
the heat transfer medium.
[0011] Further, in the heat exchanger (on the heat source side), the heat exchange is performed
in a counter flow heat exchanger regarding the refrigerant gas flow and the heat removal
carrier; thus, in a case where the temperature of the discharged gas is low according
to the operation condition of the refrigerant cycle, sufficient heat transfer cannot
be performed; accordingly, the heat exchange amount may remain under the to-be-exchanged
amount. In other words, it may be difficult that the heat carrier sufficiently removes
heat from the refrigerant gas in the higher temperature range.
[0012] It is conventionally disclosed to the public that, in a heat pump cycle device in
which CO
2 is used as a refrigerant, the heat removing heat carrier which temperature at the
outlet of the heat exchanger can be as high as the level of 90 °C, under a condition
that the pressure of the refrigerant gas (CO
2) discharged by the compressor is more than or equal to the pressure at the CO
2 transcritical point; namely, the compressor is operated so as to realize a transcritical
state regarding the working gas.
However, when the operated heat cycle with CO
2 includes a transcritical state thereof, the pressure of the transcritical state becomes
as high as 10 to 12 MPa; accordingly, it is required that the compressor be provided
with a pressure resistant structure so as to be operated under such a high pressure.
Further, in such a case where an after-burning (an additional heating) regarding the
working medium of the heat cycle including a transcritical state is performed, the
COP (coefficient of performance) of the heat cycle is deteriorated and the degree
of freedom regarding the operation of the compressor is reduced.
SUMMARY OF THE INVENTION
Subjects to be solved
[0013] In view of the above-described background, the present invention aims at providing
a two-stage compression heat pump cycle device; whereby, a stable and high temperature
condition regarding the heat transfer medium can be achieved; three heat extracting
(or supplying) heat-exchangers for extracting (or supplying) heat from the main circuit
toward the heat extracting (or supplying) side circuits can be simultaneously realized
so that the outlet temperature of the heat carrier at each heat exchanger outlet exists
in a higher temperature range, a medium temperature range, and a lower temperature
range; the COP (coefficient of performance) of the heat cycle can be enhanced; and,
the degree of freedom regarding the operation of the heat pump cycle can be enhanced.
Means to solve the Subjects
[0014] In order to reach the goals of the subjects, the present invention discloses a two-stage
compression heat pump cycle device using NH
3 as a heat-transfer medium in the heat pump cycle, the device being provided with
a two-stage compressor unit comprising a high stage compressor and a low stage compressor
and an intermediate cooler being arranged between the high stage compressor and the
low stage compressor on a part way of a line through which the heat-transfer medium
streams from the discharge side of the low stage compressor to the inlet side of the
high stage compressor; the heat-transfer medium in a gas state (the medium which is)
discharged from the high stage compressor reaches a condenser where the heat-transfer
medium is condensed into a liquid state, and the liquid heat-transfer medium enters
the intermediate cooler so that heat exchange between the liquid heat-transfer medium
and the gaseous heat-transfer medium discharged by the low stage compressor is performed;
the heat-transfer medium in the intermediate cooler proceeds to an evaporator where
the medium evaporates into a gas state; the heat-transfer medium gasified in the evaporator
returns back to the gas inhaling side of the low stage compressor so that the heat
pump cycle as a circulatory cycle is formed; wherein,
a first heat carrier line in which a first heat carrier streams is provided so that
the first heat carrier line passes through the condenser where the latent heat of
the heat-transfer medium is absorbed by the first heat carrier, the temperature of
the first heat carrier at the outlet of the condenser being in a higher temperature
range;
a second heat carrier line in which a second heat carrier streams is provided so that
the second heat carrier line passes through the evaporator where the latent heat of
the heat-transfer medium is supplied by the second heat carrier, the temperature of
the second heat carrier at the outlet of the evaporator being in a lower temperature
range;
a first sub-cooling device is provided on a part way of a line through which the heat-transfer
medium streams, between the condenser and the intermediate cooler;
a second sub-cooling device is provided on a part way of a line through which the
heat-transfer medium streams, between the intermediate cooler and the evaporator;
a third heat carrier line in which a third heat carrier streams is provided so that
the third heat carrier line passes through the second sub-cooling device and the first
sub-cooling device in order, the third heat carrier line connecting the sub-cooling
devices in a series arrangement; at each of the sub-cooling devices, the sensible
heat of the heat-transfer medium is absorbed by the third heat carrier, the temperature
of the third heat carrier at the outlet of the evaporator being in a medium temperature
range.
[0015] In the device according to the present invention, NH
3 is used as a heat-transfer medium in the heat pump cycle (i.e. in the main circuit);
the reasons (or advantageous points of NH
3) are that: NH
3 is friendly to the earth environment; the heat transfer coefficient as well as the
heat absorbing effect is great; the COP in a case where NH
3 is used can be kept high; the price of NH
3 in a unit weight is sufficiently cheap. Further, in addition to the enhanced COP
regarding the heat pump cycle, there is another advantage that the heat pump cycle
device can dispense with a high pressure resistant structure, and the easy operation
of the device can be achieved, as the maximum pressure appearing in the heat pump
cycle using NH
3 is as low as the level of 4 MPa in comparison with the heat pump cycle using CO
2 and no special pressure resistant structure for the high stage compressor is required.
Further, since the heat pump cycle using NH
3 does not include a transcritical states (i.e. high states) therein apart from the
heat pump cycle using CO
2, the COP is not deteriorated even when an after-burning (an additional heating) regarding
the working medium of the heat cycle is performed. Thus, the degree of freedom regarding
the operation of the heat pump cycle device is not reduced.
[0016] Further, the condensation temperature in the condenser can be within a range of 65
to 80°C; the intermediate temperature in the intermediate cooler can be within a range
20 to 40°C; the evaporation temperature in the evaporator can be within a range of
-20 to 10 °C. In addition, in a case where NH
3 is used as a heat-transfer medium in the heat pump cycle, the temperature of the
medium at the discharge side of the high stage compressor can be kept sufficiently
high; and, in the condenser, the heat carrier in the heat extracting circuit can stably
absorb the heat (including the latent heat) of the heat-transfer medium in the main
circuit.
[0017] The heat extracting from the heat-transfer medium in the main circuit to the heat
carrier (the third heat carrier, i.e. the intermediate temperature heat carrier) in
the heat extracting circuit is performed in the first sub-cooling device and the second
sub-cooling device; namely, the third heat carrier line (passage) in which a third
heat carrier streams is provided so that the third heat carrier line passes through
the second sub-cooling device and the first sub-cooling device in order, the third
heat carrier line connecting the sub-cooling devices in a series arrangement; in the
first sub-cooling device and the second sub-cooling device, heat exchange between
the third heat carrier and the heat-transfer medium is performed, the third heat carrier
absorbing the sensible heat of the heat-transfer medium in a counter flow arrangement
regarding the main circuit and the heat carrier line. In this way, the temperature
of the heat carrier at the outlet of the first sub-cooling device can be within a
range of 40 to 60°C.
[0018] Further, in the first sub-cooling device and the second sub-cooling device, the heat-transfer
medium in the main circuit is sub-cooled; thus, the heat transferred to the heat-transfer
medium from the (second) heat carrier streaming through the (second) heat carrier
line is increased; in particular, in comparison with the conventional technology,
the heat exchange increase brought by the heat exchange in the second sub-cooling
device relates to the COP increase regarding the heat pump cycle device.
[0019] Further, the degree of sub-cooling regarding the liquid heat-transfer medium is enhanced
while the liquid heat-transfer medium is sub-cooled in the second sub-cooling device
and the first sub-cooling device; accordingly, the degree of dryness regarding the
heat-transfer medium in the medium temperature range can be reduced. As a result,
the amount of flash gas by which the heat-transfer medium cools the medium itself
can be reduced. Therefore, the amount of the flow rate regarding the gaseous heat-transfer
medium streaming in the intermediate pressure range can be reduced; thus, the cycle
work needed in the intermediate pressure range can be reduced. Hence, the power consumption
of the high stage compressor and the low stage compressor can be reduced. Moreover,
the heat absorbing performance in the evaporator can be enhanced; thus, the COP of
the heat pump cycle device can be improved, and the stable high temperature at the
discharge side of the high stage compressor can be realized.
[0020] In addition, the heat absorbed by the first heat carrier in the high temperature
range can be used for, for instance, a heat supplying application or a heating system
in which a heat carrier is warmed from a level of 60 °C to a level of 70°C; the heat
absorbed by the first heat carrier can be used for a heat source of an adsorption
refrigerator. Further, the heat absorbed by the first heat carrier can be used for
a hot-water supply, whereby heat-exchange is performed between the to-be-heated water
and the first heat carrier via brine heat transfer medium. Moreover, the heat absorbed
by the third heat carrier in the medium temperature range can be used for a hot-water
supply, for instance, whereby water is heated-up from a level of 15°C to a level of
55 °C; or , the heat absorbed by the third heat carrier can be used for heating-up
the boiler feed water.
[0021] In addition, the heat absorbed by the second heat carrier in the low temperature
range can be made use of in the processes in cooling systems; or, the heat absorbed
by the second heat carrier can be used for an indirect system for supplying brine
(e.g. CO
2 brine), the indirect system comprising a combination of a low pressure liquid receiving
device and an evaporator; or, the heat absorbed by the second heat carrier can be
used for a NH
3-CO
2 brine liquid pump refrigeration system in which an evaporator works as a cascade
condenser that liquefies CO
2 refrigerant, the liquefied CO
2 refrigerant being circulated by a liquid pump.
[0022] A preferable embodiment according to the present invention is the two-stage compression
heat pump cycle device, the device comprising:
a first expansion valve on a part way of a line through which the heat-transfer medium
streams, between the first sub-cooling device and the intermediate cooler;
a second expansion valve on a part way of a line through which the heat-transfer medium
streams, between the second sub-cooling device and the evaporator.
Thus, the two-stage compression heat pump cycle device can be realized;
thereby, an intermediate pressure range other than the high pressure range and the
low pressure range can be formed so that the heat pump cycle device is configured.
[0023] In a case where the condensation temperature regarding the discharge gas discharged
by the high stage compressor reaches a level of 80°C, the discharge pressure of the
compressor reaches around a level of 4 MPa; the pressure level is high enough to install
a countermeasure against the NH
3 gas leakage. Hence, another preferable embodiment according to the present invention
is the two-stage compression heat pump cycle device, the device further comprising:
a hermetic type motor or an encapsulated IPM (interior permanent magnet) motor that
drives at least the high stage compressor out of the high stage compressor and the
low stage compressor; thereby, the winding of the stator is made of aluminium wire.
In this way, the motor that drives the high stage compressor can be protected against
the corrosion due to the attack of NH
3 heat-transfer medium; further, the NH
3 heat-transfer medium can be prevented from leaking outside of the device.
[0024] Another preferable embodiment according to the present invention is the two-stage
compression heat pump cycle device, the two-stage compressor unit being a single compressor
unit comprising the high stage compressor and the low stage compressor.
In this way, the two-stage compressor unit can be compactly configured; the space
where the heat pump cycle device is installed can be reduced; and, the power needed
to drive the compressors can be reduced. Further, when the hermetic type motor and
the single compressor unit are combined into an integrated configuration, the combination
can be synergistic.
[0025] Another preferable embodiment according to the present invention is the two-stage
compression heat pump cycle device, the device further comprising an oil separator
for separating the oil contained in the heat-transfer medium discharged from the high
stage compressor, whereby the oil separator is arranged on the downstream side of
the high stage compressor so that the heat-transfer medium NH
3 is pre-cooled by the condenser before the heat-transfer medium enters the oil mist
separator.
In this way, the high temperature heat-transfer medium of NH
3 gas discharged from the high stage compressor is once cooled in the condenser, before
the heat-transfer medium enters the oil mist separator; thus, the separation elements
of the separator can be prevented from being deteriorated. Further, the viscosity
of the oil mist that enters the gaseous heat-transfer medium is reduced while the
gaseous medium is cooled; thus, the separation of the lube-oil from the gaseous medium
can be effective. In addition, since the heat-transfer medium discharged from the
high stage compressor is guided into the separator after the medium is pre-cooled,
the volume of the gaseous heat-transfer medium passing through the separation elements
of the separator 12 can be reduced; thus, an appropriate velocity of flow of the gaseous
heat-transfer medium passing through the separation elements can be achieved.
[0026] Another preferable embodiment according to the present invention is the two-stage
compression heat pump cycle device, the oil separator comprising an oil separator
element for separating the oil contained in the heat-transfer medium so that the oil
separator element surrounds, in a saccate space, the mixed fluid of the oil and the
heat-transfer medium the mixed fluid which enters the saccate space through an opening;
whereby, the oil separator element comprising 3 layers-filter elements in order from
the inner side to the outer side, namely:
a rough separation pre-filter element through which rough oil particles in the mixed
fluid is separated;
a regular separation filter element that is provided with material being full of fine
holes with which a fine mesh size structure is formed so that even fine oil mist is
separated from the mixed fluid;
an oil scattering prevention filter element that is provided with a plenty of slots
through which the gaseous heat-transfer medium can pass so that the oil scattering
prevention filter element prevents the oil mist captured by the regular separation
filter element from scattering again.
[0027] The temperature of the heat-transfer medium NH
3 discharged from the high stage compressor reaches 100°C or more; on the other hand,
as described above, the oil separator is provided with the rough separation pre-filter
element through which rough oil particles in the mixed fluid is separated, inside
of the regular separation filter element that is provided with material being full
of fine holes with which a fine mesh size structure; thus, scales in the main circuit
or large size particles of the oil mist can be captured by the rough separation pre-filter
element; in this way, the regular separation filter element (i.e. filter element body)
can endure the condition of the temperature up to 150°C. Moreover, the oil separator
is provided with the oil scattering prevention filter element outside of the regular
separation filter element; thus, the oil mist once separated and captured can be prevented
from scattering again; accordingly, the oil mist separation performance can be enhanced.
[0028] Another preferable embodiment according to the present invention is the two-stage
compression heat pump cycle device; thereby the lube-oil used for the two-stage compressors
is indissoluble with the NH
3 refrigerant, namely the heat-transfer medium.
In this way, the oil mist separation performance can be further enhanced.
BRIEF DESCRIPTION OF THE DRAWINGS
[0029] The present invention will now be described in greater detail with reference to the
preferred embodiments of the invention and the accompanying drawings, wherein:
Fig. 1 shows, a schematic diagram of a heat pump cycle device according to a first
embodiment of the present invention;
Fig. 2 shows a Mollier chart according to the first embodiment of the present invention;
Fig. 3 shows a perspective view of a hermetic type motor, a part of the motor being
cut so that the inside of the motor is seen;
Fig. 4 shows an illustrative view of a compressor unit used for the first embodiment
of the present invention;
Fig. 5 shows a longitudinal cross-section as well as an elevation view of an oil separator
used in the first embodiment of the present invention;
Fig. 6 shows a schematic diagram in part regarding a heat pump cycle device according
to a second embodiment of the present invention;
Fig. 7 shows a schematic diagram of a two-stage compression refrigerator according
to the conventional technology;
Fig. 8 shows a Mollier chart regarding the two-stage compression refrigerator according
to the conventional technology.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
[0030] Hereafter, the present invention will be described in detail with reference to the
embodiments shown in the figures. However, the dimensions, materials, shape, the relative
placement and so on of a component described in these embodiments shall not be construed
as limiting the scope of the invention thereto, unless especially specific mention
is made.
[0031] The first embodiment according to the present invention is now explained based on
Figs. 1 to 5; Fig. 1 shows, a schematic diagram of a heat pump cycle device according
to the first embodiment of the present invention, the heat transfer medium NH
3 being used in the heat pump cycle device. As shown in Fig. 1, the gas-discharged
side of a high stage compressor 11 is connected to a heat-transfer medium piping 2
on which an oil separator 12 is provided; the oil separator 12 separates the oil content
included in the gas heat-transfer medium, the oil content being derived from the lube
oil used for the compressor 11; the separated lube-oil is returned back to the gas
inlet side of the high stage compressor 11 or a low stage compressor 19 that is described
later, via a return line 12a of the separated lube-oil. Incidentally, the lube-oil
used in this embodiment is, for instance, naphthenic mineral oil or alkylbenzene oil
(a synthetic oil), each oil being not compatible with the heat-transfer medium NH
3.
[0032] On a part way of the heat-transfer medium piping 2 on the downstream side of the
oil separator 12, a condenser 13 is provided; the condenser 13 is connected to a heat
carrier line 14 through which high temperature heat carrier (the first heat carrier)
is taken-out outward so that heat exchange between the heat carrier and the gaseous
heat-transfer medium NH
3 is performed; thus, the latent heat in the gas-to-liquid phase change regarding the
heat-transfer medium NH
3 is indirectly (i.e. without mixing) absorbed into the heat carrier "a" (the first
heat carrier) streaming through the heat carrier line 14; thereby, the heat carrier
"a" is heated-up, whereas the heat-transfer medium is cooled-down and liquefied.
[0033] On a part way of the heat-transfer medium piping 2 on the downstream side of the
condenser 13, a first sub-cooling device 15 is provided; the first sub-cooling device
15 is connected to a heat carrier line 16 through which the medium temperature heat
carrier "b" (the third heat carrier) is taken-out outward so that heat exchange between
the heat carrier (the heat carrier for removing heat in the medium temperature range)
and the liquefied heat-transfer medium NH
3 is performed; thus, the sensible heat in the liquid phase of the heat-transfer medium
NH
3 is absorbed into the heat carrier "b" streaming through the heat carrier line 16;
thereby, the heat carrier "b" is heated-up, whereas the heat-transfer medium is sub-cooled.
On a part way of the heat-transfer medium piping 2 on the downstream side of the first
sub-cooling device 15, a first expansion valve 17 is provided; after being depressurized
while passing through the first expansion valve 17, the heat-transfer medium reaches
the intermediate cooler 18.
[0034] On the other hand, the gaseous heat-transfer medium NH
3 is supplied to the intermediate cooler 18 from the low stage compressor 19 through
a heat-transfer medium piping 5 connected to the gas discharge side thereof. A part
of the liquid heat-transfer medium depressurized through the first expansion valve
17 evaporates in the intermediate cooler 18 so as to absorb the heat of the gaseous
heat-transfer medium (NH
3) supplied into the intermediate cooler 18 through the heat-transfer medium piping
5. Further, the gaseous heat-transfer medium (NH
3) n
1 in the intermediate cooler 18 is guided toward the high stage compressor 11 through
a heat-transfer medium piping 3; the liquid heat-transfer medium (NH
3) n
2 in the intermediate cooler 18 proceeds to a second sub-cooling device 21 through
a heat-transfer medium piping 4.
[0035] An upstream end of a heat carrier line 16 is connected to the second sub-cooling
device 21 in which, at first, the heat exchange between the heat carrier "b" (the
third heat carrier) for removing heat in the medium temperature range and the liquid
heat-transfer medium is performed so that the heat carrier "b" is preheated; on the
other hand, the liquid heat-transfer medium is further sub-cooled so that the degree
of sub-cooling as to the liquid heat-transfer medium is enhanced. In this way, the
heat carrier line 16 of the heat carrier "b" for removing heat from the liquid heat-transfer
medium in the medium temperature range is provided so that the line 16 passes through
the second sub-cooling device 21 and the first sub-cooling device 15 in a series arrangement;
thus, after the heat carrier for removing heat in the medium temperature range is
preheated in the second sub-cooling device 21, the heat carrier (the third heat carrier)
is further heated-up in the first sub-cooling device 15.
[0036] On a part way of the heat-transfer medium piping 4 on the downstream side of the
second sub-cooling device 21, a second expansion valve 22 is provided; the pressure
of the liquid heat-transfer medium is further reduced while passing through the second
expansion valve 22; then the depressurized heat-transfer medium reaches an evaporator
23. The evaporator 23 is connected to a heat carrier line 24 through which the lower
temperature heat carrier "c" is taken-out outward so that heat exchange between the
heat carrier (the second heat carrier, namely, the heat carrier for removing heat
in the lower temperature range) and the heat-transfer medium NH
3 in the liquid-to-gas phase change is performed; thus, the heat corresponding to the
latent heat is removed from the heat carrier "c", whereas the heat-transfer medium
is heated up by the heat, and the heat-transfer medium evaporates. Further, the evaporated
heat-transfer medium in a gas state reaches the lower stage compressor 19 where the
heat-transfer medium gas is compressed. On the other hand, the heat carrier "c" (the
second heat carrier) is cooled in the evaporator 23 and delivered toward a device
to use the cold.
In the above-explanation, the second expansion valve 22 is installed between the second
sub-cooling device 21 and the evaporator 23; however, the second expansion valve 22
may be installed between the intermediate cooler 18 and the second sub-cooling device
21, as is described in "SUMMARY
OF THE INVENTION."
[0037] In addition, in this embodiment, the rotating shaft of the high stage compressor
11 and the rotating shaft of the low stage compressor 19 are connected to each other
in a series arrangement so that a single compressor unit of a two-stage compressor
is formed; each of the high stage compressor 11 and the low stage compressor 19 is
a reciprocating compressor. The piston of the high stage compressor 11 and the piston
of the low stage compressor 19 are connected to a common crankshaft via the connecting
rod corresponding to each piston; each compressor is driven by the common crankshaft.
[0038] In the next place, the workings as to the heat pump cycle device 1 according to this
embodiment are now explained by use of a Mollier chart in Fig. 2. In Fig. 2, each
of the symbols A to H without or with a dash mark denotes a point in response to a
state of the heat-transfer medium in the heat pump cycle process; the symbol without
a dash mark in Fig. 2 corresponds to the same symbol in Fig. 8 (a Mollier chart) that
explains the workings as to the two-stage compression refrigerating device 010 of
Fig. 7 according to the conventional technology. The workings as to the device 010
are already explained by use of the Mollier chart of in Fig. 8.
In addition, the workings along the processes (that start from the point A and end
at the point E, passing on the points A, B, C, D and E) in the heat pump cycle device
1 according to this embodiment are the same as the workings along the processes in
the two-stage compression refrigerating device 010 according to the conventional technology.
[0039] The low refrigerant gas in a state of the point A in Fig. 2 is sucked into the low
stage compressor 19 and compressed to a state of the point B; the compressed gas (the
heat-transfer medium) discharged by the compressor 19 streams into the intermediate
cooler 18 where the gas is cooled by the liquid heat-transfer medium that streams
into the intermediate cooler 18 through the heat-transfer medium piping 2 so that
the gaseous heat-transfer medium reaches a state of the point C
[0040] The gaseous heat-transfer medium (NH
3) n
1 in the intermediate cooler 18 is guided toward the high stage compressor 11 where
the heat-transfer medium (NH
3) is compressed to a state of the point D; the heat-transfer medium (NH
3) discharged from the high stage compressor 11 enters the condenser 13 so as to be
cooled and condensed to a state of the point E. after passing through the condenser
13, the heat-transfer medium in a liquid state proceeds to the first sub-cooling device
15 where the heat-transfer medium is further cooled so as to reach a sub-cooled state
of point E'. After passing through the first sub-cooling device 15, the liquid heat-transfer
medium is depressurized while passing through the first expansion valve 17; then,
the heat-transfer medium reaches the intermediate cooler 18; thereby, the heat-transfer
medium reaches a state of the point F'.
[0041] A part of the liquid heat-transfer medium depressurized through the first expansion
valve 17 evaporates in the intermediate cooler 18 so as to absorb the heat of the
gaseous heat-transfer medium (NH
3) supplied into the intermediate cooler 18 through the heat-transfer medium piping
5; in the
Mollier chart of Fig. 2, the evaporation process regarding the part (to be evaporated)
of the liquid heat-transfer medium corresponds to the process from the point F' to
the point C. Then, the gaseous heat-transfer medium (the evaporated gas and the gas
from the low stage compressor) in the intermediate cooler 18 is guided toward the
high stage compressor 11.
On the other hand, the remaining part n
2 of the liquid heat-transfer medium in the intermediate cooler 18 proceeds to the
second sub-cooling device 21; whereby, the liquid heat-transfer medium is cooled by
the heat carrier "b" for removing heat in the medium temperature range; the cooling
process regarding the liquid heat-transfer medium corresponds to the process from
the point F' to the point G' in the Mollier chart of Fig. 2.
After passing through the second sub-cooling device 21, the liquid heat-transfer medium
is depressurized while passing through the second expansion valve 22; the depressurizing
process corresponds to the process from the point G' to the point H'. Subsequently,
the liquid heat-transfer medium evaporates in the evaporator 23 so as to take the
evaporating latent heat from the heat carrier "c" for removing heat in the lower temperature
range; the evaporating process corresponds to the process from the point H' to the
point A. Then, the low stage compressor 19 again compresses the heat-transfer medium
gasified through the evaporation; the compression process corresponds to the process
from the point A to the point B.
[0042] In this embodiment, NH
3 is used as the heat-transfer medium; however, NH
3 is inflammable (combustible) and poisonous. Thus, it is necessary to prevent NH
3 gas from leaking outside of the compressor. In a case where the condensation temperature
regarding the discharge gas discharged by the high stage compressor 11 reaches a level
of 80°C, the discharge pressure of the compressor 11 reaches around a level of 4 MPa;
the pressure level is high enough to install a countermeasure against the NH
3 gas leakage. Hence, a hermetic type motor for driving the high stage compressor 11
is usually used. Based on Fig. 3, the structure of the hermetic type motor is hereafter
explained.
[0043] A hermetic type motor 30 (as depicted in Fig. 3) is coupled with a crankshaft 52
(cf. Fig.4) for driving at least one piston of the high stage compressor 11 as well
as the low stage compressor 19; thus, the compressors 11 and 19 are driven. For instance,
the hermetic type motor 30 is a three-phase induction motor, being provided with a
pressure resistant sealed casing 31 of a substantially cylindrical shape; a rotating
shaft 33 is rotation-freely supported by sealed ball bearings 32 installed in the
casing 31; an end (on the right side of Fig. 3) of the rotating shaft 33 protrudes
toward the outside of the casing, and the rotating shaft 33 is coupled with the crankshaft
of the high stage compressor 11 as well as the low stage compressor 19.
[0044] On the inner periphery side of the casing 31, a flame 31a is provided; inside of
the flame 31a, a stator 35 is arranged so as to surround a rotator 34 that is fitted
to the rotating shaft 33. The stator 35 is equipped with a winding 36; a terminal
box 37 is fitted on the casing 31; the winding 36 communicates with thermal relays
39, electromagnetic contactors 41, circuit breakers 42 and a three-phase current power
source 43, through wiring 38 that is extended from the winding 36 at the terminal
box 37. The hermetic type motor 30 is driven by the electric power transferred through
the power supply system as described above.
[0045] As shown in Fig. 4, a compressor (unit) 50 used for the heat pump cycle device 1
according to this embodiment is configured with the high stage compressor 11 and the
low stage compressor 19 as if the two compressors form a multi-cylinder reciprocating
machine. In a crankcase 51 of the compressor unit, at least one piston of the high
stage compressor 11 as well as the low stage compressor 19 is connected to the crankshaft
52 common to both the compressors, via a connecting rod corresponding to each piston
(not shown) of each compressor.
[0046] Between the crankcase 51 and the casing 31 of the hermetic type motor 30, a coupling
casing 54 is provided so that the compressor unit 50 and the hermetic type motor 30
is integrated into one unit, completely under a gas-tight sealing condition. The rotating
shaft 33 of the hermetic type motor 30 is coupled with the crankshaft 52 via a coupling
53 that is arranged inside of the coupling casing 54.
[0047] When the hermetic type motor 30 is operated, the rotation thereof is transferred
to the crankshaft 52 of the compressor unit 50; thus, the high stage compressor 11
as well as the low stage compressor 19 is operated. Incidentally, the casing 31 is
provided with an inlet hole (not shown) and a discharge hole (not shown) regarding
the heat-transfer medium NH
3; a part of the heat-transfer medium NH
3 is supplied to the inside of the casing 31 of the motor 30, so as to cool the hermetic
type motor 30.
[0048] In relation to Fig. 3, the rotator 34 is manufactured by die-casting aluminium material,
whereas the stator 35 is made of, for example, magnetic steel plate (e.g. JIS C2522).
Insulation coating is applied on the surface of the magnetic steel plate used for
the stator. The winding is made of aluminium wire of high purity, the surface of the
wire being covered with PFA (perfluoro alkoxyfluoro plastic) that is a kind of fluorocarbon
resin. The conductivity of aluminium wire is lower than that of copper wire, whereas
aluminium wire is not subject to corrosion caused by NH
3 gas. Further, the aluminium wire of the winding is coated with PFA that is excellent
in insulation properties, tracking properties as to aluminium thermal deformation,
anti-crack properties, and anti-heat deterioration properties; thus, high durability
of the aluminium wire against NH
3 gas can be maintained.
[0049] In addition, the hermetic type motor may be an IPM (interior permanent magnet) motor
other than the three-phase induction motor; in a case of the IPM motor, permanent
magnets are embedded in the rotator; thereby, the stator is arranged so as to surround
the rotator. When the IPM motor is used, the efficiency of the motor driving the compressor
unit 50 can be enhanced and the compressor unit 50 can be made compact; moreover,
the optimal control regarding the driving motor can be realized by introducing speed
control such as what-they-call IPM speed control.
Incidentally, Patent Reference (now made public with the number
JP2004-56990) which application was submitted by the present applicant prior to the present application
discloses the detailed configuration in a case where the hermetic type motor or the
IPM motor is applied; in either of the motors, the aluminium wire is used for the
winding. The entire contents of Patent Reference
JP2004-56990 are hereby incorporated by reference.
[0050] In the next place, the configuration of the oil separator 12 is explained based on
Fig. 5. As shown in Fig. 5, an inlet opening 10a is provided in a partition 10 of
the separator 12 so that the mixed fluid "d" including the heat-transfer medium NH
3 and the lube-oil streams into the separator through the inlet opening 10a; at the
lower part of the inlet opening 10a, the oil separator 12 is fitted; the oil separator
12 comprises an upper cover 122 having an opening 122a at the center of the upper
cover 122, an oil separator element 123 forming a cylindrical shape (a saccate space),
and a lower cover 124; whereby, the lower cover 124 is supported by a large-diameter
end part 121a of a cylindrical shape that is screwed in the lower end part of a shaft
121 which is vertically installed along a center axis of the oil separator; thus,
the oil separator 12 is fitted to the inlet opening 10a of the partition 10 of the
separator 12.
[0051] The oil separator element 123 is provided with an opening on the upper side of the
element; the mixed fluid "d" that has streamed into the inside of the separator through
the opening passes through a rough separation element 125 from the inside thereof
toward the outside thereof; namely, the mixed fluid "d" passes through (the rough
meshes of) the rough separation element 125 along the direction (from inside to the
outside) of the arrows in Fig. 5. In this way, the contaminations are separated from
the mixed fluid. Further, the oil separator element 123 comprises a 3-layer-structure;
from the inner side to the outer side, the layers are the rough separation element
125, a regular separation element 126, and an oil scattering prevention element 127.
On the outer periphery side of the regular separation element 126, a support member
128 for supporting the regular separation element 126 is provided; on the outer periphery
side of the oil scattering prevention element 127, a guard member 129 for protecting
the oil scattering prevention element 127 is provided. The rough separation element
125 is configured with a rough-meshed metal wire sieve, and the element 125 separates
oil mists and contaminations of large particle size from the mixed fluid "d."
[0052] The regular separation element 126 is made of porous spongy material such as glass
wool, the material being full of fine holes with which a fine mesh size structure
is formed; at the regular separation element 126, oil mist of even a fine particle
size is separated from the mixed fluid. The oil scattering prevention element 127
is provided with a plenty of slots through which the gaseous heat-transfer medium
can pass; the oil scattering prevention element 127 prevents the oil mist captured
by the regular separation element 126 from scattering again. With the above-described
configuration of the oil separator element 123, the oil mist which particle sizes
are as fine as micron levels can be separated; further, thanks to the installation
of the rough separation element 125, the apprehension that the regular separation
element is damaged by the contaminations can be relieved.
[0053] According to this embodiment as described above, the heat-transfer medium NH
3 having excellent heat-transfer properties is used in the heat pump cycle; thereby,
the temperature of the refrigerant (the heat-transfer medium NH
3) discharged by the high stage compressor 11 reaches 100°C or more, and the condensation
temperature in the condenser 13 is within a range of 65 to 80°C. Further, the condenser
13 is connected to the heat carrier line 14 through which the high temperature heat
carrier (the first heat carrier) is taken-out outward so that heat exchange between
the heat carrier and the gaseous heat-transfer medium NH
3 is performed; incidentally, the condenser forms a counter flow heat exchanger; thus,
the latent heat in the gas-to-liquid phase change regarding the heat-transfer medium
NH
3 is indirectly (i.e. without mixing) absorbed into the heat carrier "a" streaming
through the heat carrier line 14; thereby, the heat carrier "a" (the first heat carrier)
is heated-up, whereas the heat-transfer medium is cooled-down and liquefied; the heat
absorbed by the heat carrier corresponds to the enthalpy change of the heat-transfer
medium from the point D to the point E in Fig. 2. In this way, the temperature of
the heat carrier "a" at the outlet side of the condenser 13 can reach a level of 60
to 75°C.
[0054] Taking into consideration that, in the intermediate cooler 18, the temperature of
the heat-transfer medium NH
3 is within a range 20 to 40°C, attention is paid to the heat carrier line 16 through
which the medium temperature heat carrier "b" (the third heat carrier) is taken-out
outward. The heat carrier line 16 is arranged so that it passes through the second
sub-cooling device 21 and the first sub-cooling device 15 in a series arrangement;
the heat carrier "b" absorbs the sensible heat of the liquid heat-transfer medium
NH
3 in the second sub-cooling device 21 and the first sub-cooling device 15; the heat
absorbed by the heat carrier "b" corresponds to the enthalpy change of the heat-transfer
medium from the point E to the point G' in Fig. 2. On the other hand, it is also taken
into consideration that the temperature of the liquid heat-transfer medium at the
outlet of the condenser 13 is at least 60°C. Accordingly, the temperature of the medium
temperature heat carrier "b" at the outlet of the first sub-cooling device 15 is within
a range of 40 to 60°C. For instance, in a case where the temperature of the condensed
liquid heat-transfer medium at the outlet of the condenser 13 is 60°C, the temperature
of the heat carrier "b" can be at the level of 55°C.
[0055] Further, in the evaporator 23, the heat carrier line 24 is arranged so that it passes
through the evaporator 23; whereby, the heat carrier "c" (the second heat carrier)
for removing heat in the lower temperature range absorbs the minus-heat from (i.e.
gives heat to) the heat-transfer medium; the heat (warming the heat-transfer medium)
corresponds to the enthalpy change of the heat-transfer medium from the point H' to
the point A in Fig. 2. In this way, the temperature of the heat carrier "c" at the
outlet of the evaporator 23 can be within a range of -15 to 10°C.
[0056] The heat carrier line 16 of the medium temperature heat carrier "b" sub-cools the
heat-transfer medium in the second sub-cooling device 21 and the first sub-cooling
device 15; thus, as shown in Fig. 2, the refrigerant effect increases by Δh in comparison
with the conventional refrigerant device. In other words, the evaporating latent heat
of the heat-transfer medium in the evaporator 23 can be increased.
[0057] A further explanation regarding the increase Δh is hereby given. As for the liquid
the heat-transfer medium in the intermediate cooler 18 in which the temperature of
the heat-transfer medium is, for example, 40°C, the enthalpy thereof is 145.6 kcal/kg;
when the heat-transfer medium is subsequently sub-cooled to 15°C in the second sub-cooling
device 21, the corresponding enthalpy becomes 117.8 kcal/kg; accordingly, the increase
in the refrigerant effect becomes Δh = 14506-11708 = 27.8 kcal/kg. The increase Δh
corresponds to approximately 10% of the evaporating latent heat of the liquid heat-transfer
medium in the case where the medium is heated-up from -20 to 10°C in the evaporator
23. Therefore, it can be estimated that the maximum increase in the refrigerant effect
is approximately 10%.
[0058] Further, the degree of sub-cooling regarding the liquid heat-transfer medium is enhanced
while the liquid heat-transfer medium is sub-cooled in the second sub-cooling device
21 and the first sub-cooling device 15; accordingly, the degree of dryness regarding
the heat-transfer medium in the medium temperature range can be reduced. As a result,
the amount of flash gas by which the heat-transfer medium cools the medium itself
can be reduced. Therefore, the amount of the flow rate regarding the gaseous heat-transfer
medium streaming in the intermediate pressure range (i.e. the intermediate range between
the high stage and the low stage) can be reduced; thus, the cycle work needed in the
intermediate pressure range can be reduced. Hence, the power consumption of the high
stage compressor 11 and the low stage compressor 19 can be reduced. Moreover, the
heat absorbing performance in the evaporator 23 is enhanced; thus, the COP of the
heat pump cycle device 1 can be improved, and the stable high temperature at the discharge
side of the high stage compressor 11 can be achieved.
[0059] Further, the heat-transfer medium NH
3 is used; and, apart from the case where CO
2 is used as a heat-transfer medium, the high pressure in the heat pump cycle is as
low as the level of 4 MPa; thus, no special pressure resistant structure for the high
stage compressor is required, and the compressor can be easily operated. Moreover,
the level of the high pressure in the heat pump cycle is lower than the transcritical
pressure regarding NH
3; therefore, even when the additional heating is performed so that a higher maximum
temperature is reached, the reduction of COP can be evaded. In this way, an advantage
in relation to the degree of freedom as to the operation of the heat pump cycle device
can be obtained.
[0060] Further, a reciprocating type compressor is used for the high stage compressor 11
in the compressor unit 50; in the case of reciprocating type compressor, the discharged
gaseous heat-transfer medium discharged by the compressor does not include a plenty
of lube-oil; thus, it becomes easier to achieve a necessary flow rate as well as a
higher max-temperature regarding the heat-transfer medium circulating in the heat
pump cycle. Incidentally, in a case of a screw compressor, the discharged gaseous
heat-transfer medium includes a plenty of lube-oil; thus, it is difficult to maintain
a sufficient flow rate as well as a higher max-temperature.
[0061] Further, in this embodiment, the hermetic type motor 30 as a driving means of the
compressor unit is provided; the winding 36 of the stator 35 in the hermetic type
motor 30 is made of aluminium wire; the compressor unit forms a sealed structure so
that the heat-transfer medium NH
3 does not leak outside of the compressor unit; accordingly, the inflammable (combustible)
, poisonous and highly corrosive NH
3 gas can be prevented from leaking outside; and the driving motor of the compressor
unit 50 can be free from the corrosion attack caused by NH
3 gas.
[0062] cf. [0036] Further, in this embodiment, each of the high stage compressor 11 and
the low stage compressor 19 is a reciprocating compressor; the rotating (driving)
shaft of the high stage compressor 11 and the rotating (driving) shaft of the low
stage compressor 19 forms a common crankshaft 52 so that the crankshaft is driven
by the driving motor; thus, a single compressor unit of a two-stage compressor is
formed. Hence, the installation space regarding the heat pump cycle unit 1 can be
reduced; and, the driving power to drive the high stage compressor 11 and the low
stage compressor 19 can be reduced.
[0063] Further, in this embodiment, the oil separator 12 configured as shown in Fig. 5 is
provided on the downstream side of the gas outlet regarding the high stage compressor
11; thus, the lube-oil that intrudes into the gaseous heat-transfer medium discharged
from the high stage compressor 11 can be separated with high accuracy; further, since
the lube-oil that is indissoluble with the heat-transfer medium NH
3 is used, the lube-oil even of a micron size particle can be separated.
[0064] In the next place, a second embodiment according to the present invention is explained
based on Fig. 6; in the second embodiment as shown in Fig. 6, the heat pump cycle
device is provided with: a heat-transfer medium piping 2a that guides the gaseous
heat-transfer medium discharged from the high stage compressor 11 into the condenser
13; and, a heat-transfer medium piping 2b that guides the refrigerant (the heat-transfer
medium) which sensible heat is absorbed in the condenser 13, into the oil separator
12. Incidentally, it is noted that the heat-transfer medium being guided through the
heat-transfer medium piping 2b is in a gas state.
The configuration in this second embodiment other than the hereby-described configuration
is the same as the configuration in the first embodiment; the explanation regarding
the same configuration is not repeated.
[0065] In this second embodiment, the gaseous heat-transfer medium of a high temperature
discharged from the high stage compressor 11 is once guided into the condenser 13;
whereby, heat exchange between the heat-transfer medium (in the line 2b) and the heat
carrier "a" (the first heat carrier in the line 14) for removing heat in a higher
temperature range is performed, the heat exchange being performed in the condenser
13 that forms a counter flow heat exchanger (namely, the lines 14 and 2b are in a
counter flow arrangement so that a part of the sensible heat of the heat-transfer
medium is transferred to the heat carrier "a"). In this way, the heat-transfer medium
is pre-cooled before the medium is guided into the oil separator 12. The temperature
of the heat-transfer medium NH
3 discharged from the high stage compressor 11 reaches 100°C or more; the heat-transfer
medium of that high temperature is not directly guided into the separator 12, but
the heat-transfer medium enters the separator 12 after being pre-cooled to a temperature
level of 100°C or less. In this way, the separation elements of the separator 12 can
be prevented from being deteriorated by the high temperature of the heat-transfer
medium discharged from the high stage compressor.
[0066] Further, since the heat-transfer medium discharged from the high stage compressor
is guided into the separator 12 after the medium is pre-cooled, the volume of the
gaseous heat-transfer medium passing through the separation elements of the separator
12 can be reduced; thus, an appropriate velocity of flow of the gaseous heat-transfer
medium passing through the separation elements can be achieved. It is needless to
say that the effects obtained by the first embodiment are also obtained by this second
embodiment.
Industrial Applicability
[0067] According to the present invention, a two-stage compression heat pump cycle device
using NH
3 as a heat-transfer medium in the heat pump cycle can be realized; whereby, , a stable
and high temperature condition regarding the heat transfer medium discharged by the
high stage compressor can be achieved; three heat extracting (or supplying) heat-
exchangers for extracting (or supplying) heat from the main circuit toward the heat
extracting (or supplying) side circuits can be simultaneously realized so that the
outlet temperature of the heat carrier at each heat exchanger outlet exists in a higher
temperature range, a medium temperature range, and a lower temperature range; the
COP (coefficient of performance) of the heat cycle can be enhanced; and, the degree
of freedom regarding the operation of the heat pump cycle can be enhanced.