Information
-
Patent Grant
-
6829905
-
Patent Number
6,829,905
-
Date Filed
Friday, September 19, 200321 years ago
-
Date Issued
Tuesday, December 14, 200420 years ago
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Inventors
-
Original Assignees
-
Examiners
- Esquivel; Denise L.
- Zec; Filip
Agents
- Harness, Dickey & Pierce, PLC
-
CPC
-
US Classifications
Field of Search
-
International Classifications
-
-
Disclaimer
Terminal disclaimer
Abstract
In an ejector cycle having an ejector, a throttle is provided inside a passenger compartment adjacent to an evaporator so that a length of a refrigerant passage between the throttle and the evaporator is shortened. Therefore, it can restrict a part of liquid refrigerant after being decompressed in the throttle from being evaporated in the refrigerant passage, before being introduced into the evaporator. In addition, a refrigerant inlet is provided at a lower header tank of an evaporator. Therefore, a gas-liquid refrigerant distribution difference due to the density difference between gas refrigerant and liquid refrigerant can be effectively restricted. Thus, refrigerant distributed into the plural tubes from the lower header tank can be made uniform, even if the refrigerant flow speed is low in the ejector cycle.
Description
CROSS REFERENCE TO RELATED APPLICATION
This application is based on Japanese Patent Application No. 2002-275681 filed on Sep. 20, 2002, the disclosure of which is incorporated herein by reference.
BACKGROUND OF THE INVENTION
1. Field of the Invention
The present invention relates to an ejector cycle (vapor-compression refrigerant cycle) having an ejector that is used as a decompression unit, and an arrangement structure of the ejector cycle in a vehicle.
2. Related Art
In a conventional ejector cycle described in JP-A-5-149652, low-pressure gas refrigerant in an evaporator is sucked into an ejector while high-pressure refrigerant is decompressed in a nozzle of the ejector, and pressure of refrigerant to be sucked into a compressor is increased in a pressure-increasing portion of the ejector. Therefore, liquid refrigerant in a gas-liquid separator is circulated to the evaporator by a pump operation of the ejector. In the ejector cycle, a throttle unit such as an orifice and a capillary tube is generally provided between the evaporator and the gas-liquid separator, for sufficiently reducing the pressure and the temperature of the refrigerant supplied to the evaporator. However, when a refrigerant passage length between the throttle and the evaporator is long, a part of refrigerant in the refrigerant passage may be evaporated by absorbing heat from outside before flowing into the evaporator. Thus, gas-liquid two-phase refrigerant is introduced into the evaporator, and a cooling capacity (heat-absorbing capacity) in the evaporator is decreased.
Furthermore, when the gas-liquid two-phase refrigerant is supplied into plural tubes extending vertically in an evaporator from an upper side thereof, high-density liquid refrigerant tends to flow into the plural tubes in the vicinity of its inlet, and gas refrigerant tends to flow into the plural tubes separated from the inlet. Thus, the surface temperature of the evaporator is different at different positions, and the temperature distribution of the evaporator is deteriorated.
SUMMARY OF THE INVENTION
In view of the above-described problems, it is an object of the present invention to provide an ejector cycle, which effectively improves a cooling capacity.
It is another object of the present invention to restrict a temperature distribution difference in an evaporator of the ejector cycle.
It is further another object of the present invention to provide a simple arrangement structure of the ejector cycle in a vehicle while improving the cooling capacity.
According to the present invention, an ejector cycle includes a compressor for compressing refrigerant, a high-pressure heat exchanger disposed outside of a compartment for radiating heat of high-pressure refrigerant discharged from the compressor, a low-pressure heat exchanger disposed in the compartment for evaporating low-pressure refrigerant after being decompressed, an ejector including a nozzle for decompressing and expanding high-pressure refrigerant flowing from the high-pressure heat exchanger, a gas-liquid separator for separating refrigerant discharged from the ejector into gas refrigerant and liquid refrigerant, and a throttle for decompressing refrigerant flowing from the gas-liquid separator into the low-pressure heat exchanger. The ejector sucks gas refrigerant evaporated in the low-pressure heat exchanger by using a refrigerant flow jetted from the nozzle, and increases a pressure of the refrigerant to be sucked to the compressor. In the ejector cycle, the throttle is provided in the compartment. Therefore, a length of a refrigerant passage from the throttle to the low-pressure heat exchanger can be made shorter. Thus, it can restrict a part of refrigerant from the throttle from being evaporated by absorbing heat from the atmosphere, before being introduced to the evaporator. As a result, cooling capacity of the low-pressure heat exchanger can be improved when the ejector cycle is used for an air conditioner. In addition, because it can restrict gas-liquid two-phase refrigerant from flowing into the low-pressure heat exchanger, a refrigerant distribution to be introduced to the low-pressure heat exchanger can be improved.
Further, when the ejector cycle is disposed in a vehicle, the low-pressure heat exchanger is disposed in a passenger compartment, and the gas-liquid separator and the ejector are disposed in an engine compartment. Even in this case, because the throttle is disposed in the passenger compartment adjacent to the evaporator, the refrigerant pipe length between the throttle and the low-pressure heat exchanger can be made shorter, so that cooling performance in the low-pressure heat exchanger can be improved.
Preferably, an additional heat exchanger is disposed to perform heat exchange between refrigerant flowing from the gas-liquid separator to the low-pressure heat exchanger and refrigerant to be sucked to the elector from the low-pressure heat exchanger. In this case, the throttle is disposed in a refrigerant passage through which liquid refrigerant is introduced from the gas-liquid separator to an inlet of the low-pressure heat exchanger, between an outlet of the additional heat exchanger and the inlet of the low-pressure heat exchanger. Therefore, the refrigerant to be introduced to the low-pressure heat exchanger can be cooled, and refrigerant approximately in one liquid phase state can be introduced to the low-pressure heat exchanger.
On the other hand, the low-pressure heat exchanger includes a plurality of tubes extending substantially vertically, an upper header tank connected to upper ends of the tubes to communicate with the tubes, and a lower header tank connected to lower ends of the tubes to communicate with the tubes. In this case, a refrigerant inlet is provided in the lower header tank. Therefore, refrigerant is introduced into the low-pressure heat exchanger upwardly through the refrigerant inlet. Accordingly, it can reduce a temperature difference in a surface of the low-pressure heat exchanger due to a density difference between gas refrigerant and liquid refrigerant.
BRIEF DESCRIPTION OF THE DRAWINGS
Other objects, features and advantages of the present invention will become more apparent from the following detailed description made with reference to the accompanying drawings, in which:
FIG. 1
is a schematic diagram showing an ejector cycle according to a first embodiment of the present invention;
FIG. 2
is a schematic diagram showing an arrangement structure of the ejector cycle on a vehicle, according to the first embodiment;
FIG. 3
is a schematic perspective view showing an evaporator according to the first embodiment;
FIG. 4
is a bottom view when being viewed from the arrow IV in
FIG. 3
, according to the first embodiment;
FIG. 5A
is a schematic diagram for explaining a temperature distribution in an evaporator when an inlet and an outlet are provided at a lower side of the evaporator, and
FIG. 5B
is a schematic diagram for explaining a temperature distribution in an evaporator when an inlet and an outlet are provided at an upper side of the evaporator, according to the first embodiment;
FIG. 6
is a view showing the effects of throttle positions in the ejector cycle, according to the first embodiment;
FIG. 7
is a schematic diagram showing an ejector cycle according to a second embodiment of the present invention; and
FIG. 8
is a schematic view showing a structure of a throttle according to a third embodiment of the present invention.
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS
(First Embodiment)
In the first embodiment, an ejector cycle shown in
FIG. 1
is typically used for a vehicle air conditioner. In the ejector cycle shown in
FIG. 1
, a compressor
10
is driven by an engine to compress refrigerant. A gas cooler
20
is a high-pressure side heat exchanger for performing heat-exchange between high-pressure refrigerant discharged from the compressor
10
and outside air so as to cool the high-pressure refrigerant. An evaporator
30
is a low-pressure side heat exchanger for cooling air to be blown into a passenger compartment by performing heat-exchange between air passing therethrough and low-pressure refrigerant after being decompressed. Low-pressure refrigerant is evaporated in the evaporator
30
by absorbing heat from air passing through the evaporator
30
, so that air passing through the evaporator
30
is cooled.
As shown in
FIG. 3
, the evaporator
30
includes plural tubes
31
extending vertically, upper and lower header tanks
33
extending horizontally to communicate with the tubes
31
. A core portion is constructed with the tubes
31
, and fins
32
contacting outer surfaces of the tubes
31
. The fins
32
are provided between the tubes
31
, for accelerating heat-exchange performance between air and refrigerant. A refrigerant inlet
33
a
and a refrigerant outlet
33
b
are provided in the lower header tank
33
positioned on the lower side of the core portion. The tubes
31
are arranged two layers in an air flow direction to form upstream tubes
31
positioned upstream in the air flow direction, and downstream tubes
31
positioned downstream in the air flow direction. In this embodiment, refrigerant flowing into the evaporator
30
from the refrigerant inlet
33
a
, flows through the core portion from the downstream tubes
31
toward the upstream tubes
31
, and flows out of the evaporator
30
from the refrigerant outlet
33
b.
As shown in
FIG. 1
, an ejector
40
decompresses and expands refrigerant flowing from the gas cooler
20
, and sucks gas refrigerant evaporated in the evaporator
30
. The ejector
40
includes a nozzle
41
, a mixing section
42
and a diffuser
43
. The nozzle
41
transfers pressure energy of the high-pressure refrigerant into speed energy, and decompresses and expands the refrigerant isentropicly. The mixing section
42
mixes the high-speed refrigerant injected from the nozzle
41
and the gas refrigerant evaporated in the evaporator
30
. The gas refrigerant evaporated in the evaporator
30
is sucked by entrainment function of the high-speed refrigerant injected from the nozzle
41
. The diffuser
43
further mixes the refrigerant and transfers the speed energy of the mixed refrigerant into pressure energy so that the refrigerant pressure to be sucked into the compressor
10
is increased.
Here, a drive flow injected from the nozzle
41
and a suction flow from the evaporator
30
are mixed inside the mixing section
42
so that a momentum of the drive flow and a momentum of the suction flow are conserved. Therefore, static pressure of refrigerant is raised in the mixing section. Further, in the diffuser
43
, the dynamic pressure of the refrigerant is transferred into the static pressure by gradually increasing cross-sectional area of the refrigerant passage inside the diffuser
43
. Therefore, refrigerant pressure is increased in both of the mixing section
42
and the diffuser
43
. Hence, the mixing section
42
and the diffuser
43
are generically named as a pressurizing section. A Laval nozzle is adopted as the nozzle
41
in this embodiment. The Laval nozzle has a most reduced throat in its passage to increase the injected refrigerant speed up to more than sound speed.
The gas-liquid separator
50
separates refrigerant from the ejector
40
into gas refrigerant and liquid refrigerant, and accumulates the liquid refrigerant therein. A gas refrigerant outlet of the gas-liquid separator
50
is connected to a suction port of the compressor
10
, and a liquid refrigerant outlet of the gas-liquid separator
50
is connected to the evaporator
30
.
A throttle
60
decompresses liquid refrigerant supplied from the gas-liquid separator
50
to the evaporator
30
. As shown in
FIG. 4
, the throttle
60
is constructed of an orifice
91
a
provided in a joint block
91
(connection portion) for connecting the evaporator
30
and an interior refrigerant pipe
90
. The interior refrigerant pipe
90
is provided in the passenger compartment, to be coupled to the gas-liquid separator
50
mounted in the engine compartment. The inner diameter of the orifice
91
a
is approximately 1.5 mm, and is approximately ¼ of the inner diameter of the refrigerant pipe
90
, for example, in this embodiment. The throttle
60
is provided in a refrigerant path at a position near the evaporator
30
between the evaporator
30
and the gas-liquid separator
50
, and is positioned in the passenger compartment. A joint block
92
adjacent to the evaporator
30
is brazed to the evaporator
30
, and is joined to the joint block
91
of the interior refrigerant pipe
90
. The joint block
91
and the joint block
92
are air-tightly connected to each other through an O-ring
93
by using a mechanical fastening member such as screws.
As shown in
FIG. 1
, an oil return passage
70
is provided for returning a lubrication oil separated in the gas-liquid separator
50
into the suction port of the compressor
10
. An inner heat exchanger
80
performs heat-exchange between low-pressure refrigerant to be sucked into the compressor
10
and high-pressure refrigerant from the gas cooler
20
.
Next, operation of the ejector cycle according to the first embodiment will be now described. In this embodiment, freon is used as the refrigerant. In this case, the pressure of high-pressure refrigerant discharged from the compressor
10
is lower than the critical pressure of the refrigerant. However, carbon dioxide can be used as the refrigerant. In this case, the pressure of high-pressure refrigerant discharged from the compressor
10
can be increased more than the critical pressure of the refrigerant.
When the compressor
10
starts its operation, gas refrigerant from the gas-liquid separator
50
is sucked into the compressor
10
, and the compressed refrigerant is discharged toward the gas cooler
20
. The refrigerant discharged from the compressor
10
is cooled in the gas cooler
20
, and the cooled refrigerant is expanded in the nozzle
41
of the ejector
40
. Refrigerant is sucked from the evaporator
30
to the mixing section
42
while refrigerant is jetted from the nozzle
41
. The refrigerant sucked from the evaporator
30
and the refrigerant jetted from the nozzle
41
are mixed in the mixing section
42
and is expanded in the diffuser
43
. Then, refrigerant is discharged from an outlet of the diffuser
43
of the ejector
40
into the gas-liquid separator
50
.
On the other hand, because refrigerant in the evaporator
30
is sucked into the ejector
40
, liquid refrigerant in the gas-liquid separator
50
is supplied into the evaporator
30
after passing through the throttle
60
. The supplied refrigerant evaporates in the evaporator
30
by absorbing heat from air to be blown into the passenger compartment.
As shown in
FIG. 3
, the refrigerant inlet
33
a
is provided in the lower header tank
33
. Therefore, refrigerant flows from the lower header tank
33
into the evaporator
30
upwardly, in this embodiment. Therefore, it is compared with a case where refrigerant flows from the upper refrigerant tank
33
into the evaporator
30
downwardly, the gas-liquid refrigerant distribution difference in the evaporator
30
due to the gravity difference between gas refrigerant and liquid refrigerant can be effectively restricted. Because refrigerant introduced into the lower header tank
33
from the refrigerant inlet
33
a
flows upwardly, it can restrict liquid refrigerant having relatively a large density from being readily introduced into the tubes
31
adjacent to the refrigerant inlet
33
a
, and gas refrigerant having relatively a small density from being readily introduced into the tubes
31
separated from the refrigerant inlet
33
a
. Thus, even if refrigerant flow speed from the gas-liquid separator
50
to the evaporator
30
is low in the ejector cycle, refrigerant can be uniformly distributed into the plural tubes
31
from the refrigerant inlet
33
a
, regardless its density difference between liquid refrigerant and gas refrigerant. As a result, in this embodiment, it can prevent high-density liquid refrigerant from mainly flowing into tubes
31
in vicinity of the refrigerant inlet
33
a
and low-density gas refrigerant from mainly flowing into tubes
31
separated from the refrigerant inlet
33
a
. Therefore, the surface temperature distribution of the evaporator
30
can be made uniform, and air temperature distribution can be made uniform.
In this ejector cycle, refrigerant is circulated from the gas-liquid separator
50
to the evaporator
30
by pumping operation of the ejector
40
. Therefore, it is compared with a expansion valve cycle where a compressor directly circulates refrigerant to the evaporator
30
, the amount of liquid refrigerant flowing into the evaporator
30
in this ejector cycle is larger. Therefore, refrigerant flow speed tends to be low in this ejector cycle, comparing with that of the expansion valve cycle. However, in the first embodiment, even when the refrigerant flow speed is low, the refrigerant distribution difference in the evaporator
30
and in an air temperature difference on the surface of the evaporator
30
can be can be made smaller.
FIG. 5B
shows a test result of the temperature distribution on the surface of the evaporator
30
when refrigerant flows from the refrigerant inlet of the upper header tank
33
into the evaporator
30
downwardly. In this case, the evaporator
30
has a wide temperature distribution difference, in particular on the right side of the surface adjacent to the refrigerant inlet. In this case, the highest air temperature on the surface of the evaporator is about 8.3° C., and maximum temperature deviation is about 2° C. comparing with the average temperature of the left side surface 5.35° C. On the contrary, according to the present invention of
FIG. 5A
, temperature distribution difference is reduced when refrigerant flows from the refrigerant inlet
33
a
of the lower header tank
33
into the evaporator
30
. As shown in
FIG. 5A
, the highest air temperature is about 5.8° C. on the surface, and maximum temperature deviation is less than 1° C. in the entire surface of the evaporator
30
. Thus, the air temperature (i.e., post-evaporator air temperature) of the evaporator
30
can be made uniform in the structure of the evaporator
30
in the first embodiment. In the experiments of
FIGS. 5A and 5B
, the air temperature introduced into the evaporator
30
is 27° C., the relative humidity of air introduced into the evaporator
30
is 50% RH, the air flow to be blown into the evaporator
30
is 450 m
3
/h, and the pressure of refrigerant flowing into the evaporator
30
from the refrigerant inlet
33
a
is 38.4 kgf/cm
2
G (3.7 Mpa).
As shown in
FIG. 2
, the throttle
60
is provided inside the passenger compartment so that refrigerant passage from the throttle
60
to the evaporator
30
is shortened. Therefore, it can restrict a part of liquid refrigerant from being evaporated before flowing into the evaporator
30
by absorbing heat from the atmosphere. Thus, a flow of gas-liquid two-phase refrigerant into the evaporator
30
can be avoided. Therefore, temperature deviation can be made small while cooling performance (heat-absorbing performance) of the evaporator
30
can be improved.
FIG. 6
shows a test result of a temperature distribution of air blown into different positions of the passenger compartment in a vehicle width direction, such as the center areas of the driver's and front-passenger's seats and the sides areas of the driver's and front-passenger's seats. Further,
FIG. 6
shows a temperature distribution of air immediately after passing through the evaporator
30
, when the throttle
60
is positioned in an engine compartment, and when the throttle
60
is positioned in the passenger compartment in the vicinity of the evaporator
30
.
As shown in
FIG. 6
, when the throttle
60
is positioned in the engine compartment, the highest temperature of air blown into the passenger compartment is about 21.1° C. and the lowest temperature of air blown into the passenger compartment is about 17.7° C. In this case, maximum temperature deviation is about 3.4° C. On the contrary, when the throttle
60
is disposed adjacent to the evaporator
30
to be separated from the evaporator
30
by about 0.1 m, the highest temperature of air blown into the passenger compartment is about 15.5° C., and the lowest temperature of air blown into the passenger compartment is about 14.0° C. In this case, maximum temperature deviation is about 1.5° C. Thus, temperature deviation of air blown toward different positions of the passenger compartment can be effectively decreased by positioning the throttle
60
in the vicinity of the evaporator
30
.
Further, as shown in
FIG. 6
, when the throttle
60
is provided in the engine compartment to be largely separated from the evaporator
30
, the highest air temperature (post-evaporator air temperature) after passing through the evaporator
30
is about 21.4° C., and the lowest post-evaporator air temperature is about 13.0° C. In this case, temperature deviation of the post-evaporator air temperature is about 8.4° C. On the contrary, when the throttle
60
is provided around the evaporator
30
, the highest post-evaporator air temperature is about 13.1° C., and the lowest post-evaporator air temperature is about 12.3° C. In this case, the temperature deviation of the post-evaporator air temperature is about 0.8° C. Accordingly, the temperature deviation in the post-evaporator air temperature can be effectively decreased by positioning the throttle
60
in the vicinity of the evaporator
30
. In
FIG. 6
, the post-evaporator air temperature is detected by a thermistor.
According to experiments by the inventors of the present invention, when the throttle
60
is disposed adjacent to the evaporator
30
in a case where the refrigerant inlet
33
a
and the refrigerant outlet
33
b
are positioned in the upper header tank
33
, the surface temperature distribution difference of the evaporator
30
can be reduced.
As shown in
FIG. 4
, the throttle
60
is constructed with the orifice
91
a
in a connection portion between an interior refrigerant pipe
90
and the evaporator
30
. Therefore, surface temperature of the evaporator
30
can be uniformed without increase of the part number of the ejector cycle.
(Second Embodiment)
In the second embodiment shown in
FIG. 7
, a heat exchanger
81
is provided to perform heat-exchange between refrigerant flowing from the gas-liquid separator
50
to the evaporator
30
and refrigerant sucked from the evaporator
30
into the ejector
40
. In this case, the throttle
60
is provided in a refrigerant outlet side of the heat exchanger
81
, at a position before being introduced into the evaporator
30
. According to the second embodiment of the present invention, refrigerant flowing from the gas-liquid separator
50
toward the evaporator
30
can be cooled by low-temperature refrigerant flowing from the evaporator
30
into the ejector
40
. Therefore, the refrigerant flowing into the evaporator
30
from the gas-liquid separator
50
can be approximated in a single-phase liquid refrigerant.
In the second embodiment, other parts are similar to those of the above-described first embodiment. Thus, temperature deviation can be made small while cooling capacity (heat-absorbing capacity) of the evaporator
30
can be improved.
(Third Embodiment)
In the third embodiment, as shown in
FIG. 8
, a throttle
60
is provided in a connecting portion between the interior refrigerant pipe
90
and an exterior refrigerant pipe
94
. The interior refrigerant pipe
90
is connected to the evaporator
30
, and is provided in the passenger compartment. On the other hand, the exterior refrigerant pipe
94
is connected to the gas-liquid separator
50
, and is provided in the engine compartment. In the third embodiment, the shape of the throttle
60
and the shape of the connection portion between the interior refrigerant pipe
90
and the exterior refrigerant pipe
94
can be suitably changed. Further, the throttle
60
is preferably provided in the passenger compartment or in a partition wall for partitioning the passenger compartment and the engine compartment. However, the throttle
60
can be provided in the engine compartment outside the passenger compartment at a position near the evaporator
30
.
Although the present invention has been fully described in connection with the preferred embodiments thereof with reference to the accompanying drawings, it is to be noted that various changes and modifications will become apparent to those skilled in the art.
For example, in the above embodiment, two core portions are provided serially with respect to the air flow direction, and the refrigerant outlet
33
b
is provided on the lower header tank
33
. However, the structure of the evaporator
30
is not limited to that of described above. For example, the evaporator
30
can have one core portion in the air flow direction. Besides, the evaporator
30
can have refrigerant outlet
33
b
on its upper side.
The throttle
60
is not limited to a fixed throttle such as an orifice and a capillary tube used in this embodiment. As the throttle
60
, a thermal expansion valve or a variable control valve can be used. The thermal expansion valve variably controls its throttle degree, so that a super heat degree of the refrigerant at an outlet of the evaporator
30
becomes a predetermined degree.
The nozzle
41
of the ejector
40
is not limited to the Laval nozzle adopted in this embodiment. For example, a tapered nozzle or the like can be used for the nozzle
41
of the ejector
40
.
Further, the ejector cycle of the present invention can be used for an apparatus other than the vehicle air conditioner.
Such changes and modifications are to be understood as being within the scope of the present invention as defined by the appended claims.
Claims
- 1. An ejector cycle comprising:a compressor for compressing refrigerant; a high-pressure heat exchanger disposed outside of a compartment, for radiating heat of high-pressure refrigerant discharged from the compressor; a low-pressure heat exchanger disposed in the compartment for evaporating low-pressure refrigerant after being decompressed; an ejector including a nozzle for decompressing and expanding high-pressure refrigerant flowing from the high-pressure heat exchanger, the ejector sucking gas refrigerant evaporated in the low-pressure heat exchanger by using a refrigerant flow jetted from the nozzle, and increasing a pressure of the refrigerant to be sucked to the compressor; a gas-liquid separator for separating refrigerant discharged from the ejector into gas refrigerant and liquid refrigerant, the gas-liquid separator having a gas refrigerant outlet connected to a suction port of the compressor, and a liquid refrigerant outlet connected with the low-pressure heat exchanger; and a throttle for decompressing refrigerant flowing from the gas-liquid separator into the low-pressure heat exchanger, wherein the throttle is provided in the compartment.
- 2. The ejector cycle according to claim 1, further comprising:an interior refrigerant pipe disposed in the compartment to be connected to the low-pressure heat exchanger; and an exterior refrigerant pipe disposed outside the compartment to be connected to the gas-liquid separator, wherein: the interior refrigerant pipe and exterior refrigerant pipe are connected to a connection portion; and the throttle is disposed in the connection portion.
- 3. The ejector cycle according to claim 2, wherein the throttle is an orifice provided in the connection portion.
- 4. The refrigerant cycle according to claim 1, further comprising:an interior refrigerant pipe that is connected to the low-pressure heat exchanger at a connection portion, wherein the throttle is provided in the connection portion between the interior refrigerant pipe and the low-pressure heat exchanger.
- 5. The ejector cycle according to claim 4, wherein the throttle is an orifice provided in the connection portion.
- 6. The ejector cycle according to claim 1, wherein:the low-pressure heat exchanger is connected to the gas-liquid separator through a refrigerant pipe; and the throttle is disposed in the refrigerant pipe adjacent to the low-pressure heat exchanger.
- 7. The ejector cycle according to claim 1, further comprisingan additional heat exchanger that is disposed to perform heat exchange between refrigerant flowing from the gas-liquid separator to the low-pressure heat exchanger and refrigerant to be sucked to the ejector from the low-pressure heat exchanger, wherein the throttle is disposed in a refrigerant passage through which liquid refrigerant is introduced from the gas-liquid separator to an inlet of the low-pressure heat exchanger, between an outlet of the additional heat exchanger and the inlet of the low-pressure heat exchanger.
- 8. The ejector cycle according to claim 1, wherein:the low-pressure heat exchanger includes a plurality of tubes extending substantially vertically, an upper header tank connected to upper ends of the tubes to communicate with the tubes, and a lower header tank connected to lower ends of the tubes to communicate with the tubes; the low-pressure heat exchanger has a refrigerant inlet from which refrigerant is introduced into the low-pressure heat exchanger; and the refrigerant inlet is provided in the lower header tank.
- 9. An ejector cycle comprising:a compressor for compressing refrigerant; a high-pressure heat exchanger disposed outside of a compartment, for radiating heat of high-pressure refrigerant discharged from the compressor; a low-pressure heat exchanger disposed in the compartment for evaporating low-pressure refrigerant after being decompressed; an ejector including a nozzle for decompressing and expanding high-pressure refrigerant flowing from the high-pressure heat exchanger, the ejector sucking gas refrigerant evaporated in the low-pressure heat exchanger by using a refrigerant flow jetted from the nozzle, and increasing a pressure of refrigerant to be sucked into the compressor; and a gas-liquid separator for separating refrigerant discharged from the ejector into gas refrigerant and liquid refrigerant, the gas-liquid separator having a gas refrigerant outlet connected to a suction port of the compressor, and a liquid refrigerant outlet connected with the low-pressure heat exchanger, wherein: the low-pressure heat exchanger includes a plurality of tubes extending substantially vertically, an upper header tank connected to upper ends of the tubes to communicate with the tubes, and a lower header tank connected to lower ends of the tubes to communicate with the tubes; the low-pressure heat exchanger has a refrigerant inlet from which refrigerant is introduced into the low-pressure heat exchanger; and the refrigerant inlet is provided in the lower header tank.
- 10. An arrangement structure of an ejector cycle in a vehicle having a passenger compartment and an engine compartment partitioned from each other, the arrangement structure comprising:a compressor disposed in the engine compartment, for compressing refrigerant; a high-pressure heat exchanger disposed in the engine compartment, for radiating heat of high-pressure refrigerant discharged from the compressor; a low-pressure heat exchanger disposed in the passenger compartment, for evaporating low-pressure refrigerant after being decompressed; an ejector disposed in the engine compartment, which includes a nozzle for decompressing and expanding high-pressure refrigerant flowing from the high-pressure heat exchanger, the ejector sucking gas refrigerant evaporated in the low-pressure heat exchanger by using a refrigerant flow jetted from the nozzle, and increasing a pressure of refrigerant to be sucked to the compressor; a gas-liquid separator disposed in the engine compartment, for separating refrigerant discharged from the ejector into gas refrigerant and liquid refrigerant, the gas-liquid separator having a gas refrigerant outlet connected to a suction port of the compressor, and a liquid refrigerant outlet connected with the low-pressure heat exchanger; and a throttle for decompressing refrigerant flowing from the gas-liquid separator into the low-pressure heat exchanger, wherein the throttle is provided in the passenger compartment.
- 11. The arrangement structure according to claim 10, further comprisingan interior refrigerant pipe that is connected to the low-pressure heat exchanger at a connection portion in the passenger compartment, wherein the throttle is provided in the connection portion between the interior refrigerant pipe and the low-pressure heat exchanger.
- 12. The ejector cycle according to claim 10, further comprising:an interior refrigerant pipe disposed in the passenger compartment to be connected to the low-pressure heat exchanger; and an exterior refrigerant pipe disposed in the engine compartment to be connected to the gas-liquid separator, wherein the interior refrigerant pipe and the exterior refrigerant pipe are connected to a connection portion in the passenger compartment, and the throttle is disposed in the connection portion.
Priority Claims (1)
Number |
Date |
Country |
Kind |
2002-275681 |
Sep 2002 |
JP |
|
US Referenced Citations (2)
Number |
Name |
Date |
Kind |
6044655 |
Ozaki et al. |
Apr 2000 |
A |
6550265 |
Takeuchi et al. |
Apr 2003 |
B2 |
Foreign Referenced Citations (1)
Number |
Date |
Country |
5-149652 |
Jun 1993 |
JP |