BACKGROUND OF THE INVENTION
Field of the Invention
[0001] The present invention relates to a cryocooler compressor.
Description of Related Art
[0002] In general, a cryocooler such as a Gifford-McMahon (GM) cryocooler includes a compressor
of a refrigerant gas to supply a high-pressure refrigerant gas to a cold head. The
compressor includes components such as a compressor main body, an oil separator, an
adsorber, a storage tank, and a control device (for example,
Japanese Unexamined Patent Publication No. 2001-74326).
SUMMARY OF THE INVENTION
[0003] In addition to the above-described components, the compressor for the cryocooler
is usually provided with a heat exchanger the cools the compressor. These components
of the compressor are accommodated in a compressor casing. In the existing design,
the heat exchanger occupies a relatively large footprint in the compressor casing.
Therefore, in aiming for miniaturization of the compressor, the heat exchanger may
be one of obstacles.
[0004] An exemplary object of one embodiment of the present invention is to propose heat
exchanger disposition that enables reduction in footprint of the heat exchanger in
the cryocooler compressor.
[0005] According to an aspect of the present invention, there is provided a cryocooler compressor
including a compressor casing and a double pipe-type heat exchanger that is accommodated
in the compressor casing and cools the compressor. The double pipe-type heat exchanger
includes a double pipe disposed along at least one surface of the compressor casing.
[0006] According to the present invention, it is possible to provide heat exchanger disposition
that enables reduction in footprint of the heat exchanger in the cryocooler compressor.
BRIEF DESCRIPTION OF THE DRAWINGS
[0007]
Fig. 1 is a diagram schematically showing a cryocooler according to an embodiment.
Fig. 2 is a schematic perspective view showing an appearance of a compressor according
to the embodiment.
Fig. 3 is a schematic perspective view showing disposition of devices inside the compressor
according to the embodiment.
Fig. 4 is a schematic front view of a heat exchanger according to the embodiment.
Fig. 5A is a schematic top view showing disposition of devices inside the compressor
according to the embodiment, and Fig. 5B is a schematic top view showing disposition
of devices inside a compressor according to a comparative example.
DETAILED DESCRIPTION OF THE INVENTION
[0008] Hereinafter, an embodiment for carrying out the present invention will be described
in detail with reference to the drawings. In the description and the drawings, the
same or equivalent components, members, and processes are denoted by the same reference
numerals, and overlapping description is omitted as appropriate. The scale and the
shape of each of parts shown in the drawings are set for convenience to make the description
easy to understand, and are not to be interpreted as limiting unless stated otherwise.
The embodiment is merely an example and does not limit the scope of the present invention.
All features described in the embodiment or combinations thereof are not necessarily
essential to the present invention.
[0009] Fig. 1 is a diagram schematically showing a cryocooler 10 according to the embodiment.
The cryocooler 10 is used to provide cryogenic cooling to an object or a medium. For
example, the cryocooler 10 may be used as a cooling source for a superconducting magnet
device. The superconducting magnet device is mounted on, for example, a high magnetic
field using device as a magnetic field source of an accelerator such as a single crystal
pulling device, a nuclear magnetic resonance (NMR) system, a magnetic resonance imaging
(MRI) system, and a cyclotron, a high energy physical system such as a nuclear fusion
system, or other high magnetic field using devices (not shown) and can generate a
high magnetic field required for the devices.
[0010] The cryocooler 10 includes a compressor 12 and a cold head 14. The compressor 12
is configured to collect a refrigerant gas of the cryocooler 10 from the cold head
14, to pressurize the collected refrigerant gas, and to supply the refrigerant gas
to the cold head 14 again. The compressor 12 is also referred to as a compressor unit.
The cold head 14 is also referred to as an expander and includes a room temperature
section 14a and a low-temperature section 14b which is also referred to as a cooling
stage. The refrigerant gas is also referred to as a working gas, and other suitable
gases may be used although a helium gas is typically used. The compressor 12 and the
cold head 14 constitute a refrigeration cycle of the cryocooler 10, whereby the low-temperature
section 14b is cooled to a desired cryogenic temperature. The low-temperature section
14b can cool an object to be cooled such as a superconducting magnet.
[0011] Although the cryocooler 10 is, for example, a single-stage or two-stage Gifford-McMahon
(GM) cryocooler, the cryocooler 10 may be a pulse tube cryocooler, a Stirling cryocooler,
or other types of cryocoolers. Although the cold head 14 has a different configuration
depending on the type of the cryocooler 10, the compressor 12 can use a configuration
described below regardless of the type of the cryocooler 10.
[0012] In general, both a pressure of a refrigerant gas supplied from the compressor 12
to the cold head 14 and a pressure of a refrigerant gas collected from the cold head
14 to the compressor 12 are considerably higher than the atmospheric pressure, and
can be called a first high pressure and a second high pressure, respectively. For
convenience of description, the first high pressure and the second high pressure are
also simply called a high pressure and a low pressure, respectively. Typically, the
high pressure is, for example, 2 to 3 MPa. The low pressure is, for example, 0.5 to
1.5 MPa and is, for example, about 0.8 MPa.
[0013] The compressor 12 is an oil-lubricated cryocooler compressor, and includes a compressor
main body 16, a refrigerant gas line 18, and an oil circulation line 20. In Fig. 1,
in order to facilitate understanding, the refrigerant gas line 18 is shown by a solid
line, and the oil circulation line 20 is shown by a broken line. In addition, the
compressor 12 includes a compressor casing 24 that accommodates each component of
the compressor 12, such as the compressor main body 16, the refrigerant gas line 18,
and the oil circulation line 20.
[0014] The compressor main body 16 is configured to internally compress a refrigerant gas
sucked from a suction port of the compressor main body 16 and to discharge the refrigerant
gas from a discharge port. An oil is used in the compressor main body 16 for the sake
of cooling and lubrication, and the sucked refrigerant gas is directly exposed to
the oil in the compressor main body 16. Accordingly, the refrigerant gas is delivered
from the discharge port in a state where the oil is slightly mixed.
[0015] The compressor main body 16 may be, for example, a scroll type pump, a rotary type
pump, or other pumps that pressurize a refrigerant gas. The compressor main body 16
may be configured to discharge the refrigerant gas at a fixed and constant flow rate.
Alternatively, the compressor main body 16 may be configured to vary the flow rate
of the refrigerant gas to be discharged. The compressor main body 16 may be called
a compression capsule.
[0016] The refrigerant gas line 18 includes a discharge port 30, a suction port 31, a discharge
flow path 32, and a suction flow path 33. The discharge port 30 is an outlet of a
refrigerant gas that is installed in the compressor casing 24 in order to deliver
the refrigerant gas, which is pressurized to a high pressure by the compressor main
body 16, from the compressor 12, and the suction port 31 is an inlet of the refrigerant
gas that is installed in the compressor casing 24 in order for the compressor 12 to
receive a low-pressure refrigerant gas. The compressor casing 24 accommodates the
discharge flow path 32 and the suction flow path 33. The discharge port of the compressor
main body 16 is connected to the discharge port 30 by the discharge flow path 32,
and the suction port 31 is connected to the suction port of the compressor main body
16 by the suction flow path 33.
[0017] The refrigerant gas line 18 is connected to the cold head 14. A high-pressure port
40 and a low-pressure port 41 are provided in the room temperature section 14a of
the cold head 14. The high-pressure port 40 is connected to the discharge port 30
by a high-pressure pipe 42, and the low-pressure port 41 is connected to the suction
port 31 by a low-pressure pipe 43.
[0018] The oil separator 34 and the adsorber 35 are provided in the discharge flow path
32. The oil separator 34 is provided in order to separate an oil, which is mixed in
a refrigerant gas as passing through the compressor main body 16, out from the refrigerant
gas. The adsorber 35 is provided in order to remove, for example, a vaporized oil
and other contaminants remaining in the refrigerant gas from the refrigerant gas through
adsorption. The oil separator 34 and the adsorber 35 are connected in series. In the
discharge flow path 32, the oil separator 34 is disposed on the compressor main body
16 side, and the adsorber 35 is disposed on the discharge port 30 side.
[0019] An oil return line 21 that connects the oil separator 34 to the compressor main body
16 is provided. An oil collected by the oil separator 34 can be returned to the compressor
main body 16 through the oil return line 21. In the middle of the oil return line
21, a filter that removes dust included in the oil separated out by the oil separator
34 and an orifice that controls the amount of the oil returning to the compressor
main body 16 may be provided.
[0020] On the other hand, a storage tank 36 is provided at the suction flow path 33. The
storage tank 36 is provided as a volume for removing pulsation included in a low-pressure
refrigerant gas returning from the cold head 14 to the compressor 12.
[0021] In addition, a bypass valve 38 that connects the discharge flow path 32 to the suction
flow path 33 to bypass the compressor main body 16 is provided at the refrigerant
gas line 18. For example, the bypass valve 38 branches off from the discharge flow
path 32 between the oil separator 34 and the adsorber 35 and is connected to the suction
flow path 33 between the compressor main body 16 and the storage tank 36. The bypass
valve 38 is provided in order to control a flow rate of a refrigerant gas and/or in
order to equalize the discharge flow path 32 and the suction flow path 33 when the
compressor 12 is stopped.
[0022] The oil circulation line 20 connects an oil outlet to an oil inlet of the compressor
main body 16 in order to return the oil flowing out from the compressor main body
16 to the compressor main body 16 again. The oil circulation line 20 may be provided
with an orifice that controls a flow rate of an oil flowing therein. In addition,
a filter that removes dust included in the oil may be provided at the oil circulation
line 20.
[0023] In addition, the compressor 12 further includes a heat exchanger 22 that is accommodated
in the compressor casing 24 and cools the compressor 12. The heat exchanger 22 includes
a refrigerant gas cooler 22a that cools the refrigerant gas line 18 through heat exchange
between the refrigerant gas and a cooling medium, and an oil cooler 22b that cools
the oil circulation line 20 through heat exchange between the oil and the cooling
medium.
[0024] The refrigerant gas cooler 22a is disposed between the compressor main body 16 and
the oil separator 34 in the discharge flow path 32, and cools a high-pressure refrigerant
gas heated by compression heat generated with the compression of the refrigerant gas
in the compressor main body 16. The refrigerant gas cooler 22a cools the refrigerant
gas through heat exchange between the refrigerant gas and the cooling medium. The
cooled refrigerant gas is purified by the oil separator 34 and the adsorber 35. In
addition, the oil cooler 22b cools the oil through heat exchange between the oil flowing
out from the oil outlet of the compressor main body 16 to the oil circulation line
20 and the cooling medium. The cooled oil is returned into the compressor main body
16 from the oil inlet of the compressor main body 16. The cooling medium is supplied
from the outside to the compressor 12 through a cooling medium intake 44, and is discharged
to the outside of the compressor 12 from a cooling medium discharge port 45 via the
refrigerant gas cooler 22a and the oil cooler 22b. The cooling medium may be a coolant,
for example, water. In this manner, compression heat generated by the compressor main
body 16 is removed to the outside of the compressor 12 together with the cooling medium.
The cooling medium may be cooled by, for example, a chiller (not shown) and may be
supplied again.
[0025] In this embodiment, the heat exchanger 22 is a double pipe-type heat exchanger. Therefore,
the heat exchanger 22 includes an outer tube and an inner tube inserted into the outer
tube. The cooling medium is supplied to one of the outer tube and the inner tube,
a fluid to be cooled is supplied to the other. Accordingly, heat exchange between
the cooling medium and the target fluid is performed, and the fluid can be cooled.
For example, in the refrigerant gas cooler 22a, cooling water may be supplied to the
outer tube, and the refrigerant gas may be supplied to the inner tube. In the oil
cooler 22b, cooling water may be supplied to the outer tube, and oil may be supplied
to the inner tube.
[0026] In addition, the compressor casing 24 may accommodate a control device 50 for controlling
the cryocooler 10. The control device 50 may include a control circuit configured
to receive an output from various sensors provided in the cryocooler 10 and to control
various devices of the cryocooler 10 based on the sensor output. The sensor may include,
for example, a refrigerant gas temperature sensor and a refrigerant gas pressure sensor
provided in the refrigerant gas line 18, an oil temperature sensor provided in the
oil circulation line 20, or a cooling temperature sensor provided in the low-temperature
section 14b of the cold head 14. The device controlled based on the sensor output
may include, for example, a compressor motor that drives the compressor main body
16, the bypass valve 38, and a cold head motor that drives the cold head 14. The control
device 50 may include a compressor inverter for controlling a rotation speed of the
compressor motor and/or a cold head inverter for controlling a rotation speed of the
cold head motor.
[0027] During an operation of the cryocooler 10, a refrigerant gas is supplied from the
compressor 12 to the cold head 14, a refrigeration cycle (for example, a GM cycle)
is configured by a periodic volume fluctuation of an expansion space of the refrigerant
gas in the cold head 14 and a pressure fluctuation of the refrigerant gas in the expansion
space synchronized with the periodic volume fluctuation, and the low-temperature section
14b of the cold head 14 is cooled to a desired cryogenic temperature. In a case where
the cold head 14 is, for example, a two-stage type, a first-stage cooling stage is
cooled to a first cooling temperature in a range of, for example, about 30 K to about
80 K, and a second-stage cooling stage is cooled to a second cooling temperature lower
than the first cooling temperature, for example, 1 K to 20 K. The second cooling temperature
may be a liquid helium temperature of about 4.2 K or a temperature lower than the
liquid helium temperature.
[0028] A refrigerant gas collected from the cold head 14 to the compressor 12 flows into
the suction port 31 of the compressor 12 from the low-pressure port 41 through the
low-pressure pipe 43. The refrigerant gas is collected to the suction port of the
compressor main body 16 via the storage tank 36 on the suction flow path 33. The refrigerant
gas is compressed and pressurized by the compressor main body 16. In this case, a
temperature of the refrigerant gas is raised by compression heat. The refrigerant
gas delivered from the discharge port of the compressor main body 16 is cooled by
the refrigerant gas cooler 22a of the heat exchanger 22, and exits the compressor
12 from the discharge port 30 via the oil separator 34 and the adsorber 35. The refrigerant
gas is supplied into the cold head 14 via the high-pressure pipe 42 and the high-pressure
port 40.
[0029] Fig. 2 is a schematic perspective view showing an appearance of the compressor 12
according to the embodiment. Fig. 4 is a schematic perspective view showing the disposition
of the devices inside the compressor 12 according to the embodiment. Figs. 2 and 3
each show a perspective view of the compressor 12 seen from a rear side. Fig. 3 shows
a state in which some panels of the compressor casing 24 are removed in order to show
the disposition of the internal devices of the compressor 12.
[0030] As shown in Fig. 2, the compressor casing 24 of the compressor 12 has a rectangular
parallelepiped shape having six surfaces, and includes a front panel 24a, a back panel
24b, an upper panel 24c, a bottom panel 24d, and two side panels 24e and 24f on left
and right sides. The back panel 24b faces an opposite side of the front panel 24a.
Between the front panel 24a and the back panel 24b, the upper panel 24c is disposed
above, the bottom panel 24d is disposed below, and the side panels 24e and 24f are
disposed on the left and right sides.
[0031] The front panel 24a may be configured to provide a user interface and a pipe connection.
Accordingly, an operation panel 25 for receiving an input for controlling the cryocooler
10 from a user of the cryocooler 10 and/or for displaying information regarding the
cryocooler 10 may be provided on a front surface of the front panel 24a. The control
device 50 may be mounted on the front panel 24a. For example, the control device 50
may be attached to a back surface of the front panel 24a. In addition, the front panel
24a may be provided with the discharge port 30, the suction port 31, the cooling medium
intake 44, and the cooling medium discharge port 45 although the discharge port 30,
the suction port 31, the cooling medium intake 44, and the cooling medium discharge
port 45 are not shown in Figs. 2 and 3 because they are oriented in the opposite direction.
[0032] Casters 52 may be attached to the bottom panel 24d in order to facilitate the movement
and the transportation of the compressor 12.
[0033] As shown in Fig. 3, the compressor casing 24 includes a frame structure 26 that supports
the above-described panels and is responsible for structural strength. The panels
are removably attached to the frame structure 26. In a state where the panels are
attached to the frame structure 26, the devices inside the compressor 12 are covered
and hidden by the panels as shown in Fig. 2. The panels may be attached to the frame
structure 26 by an appropriate method such as screwing. In a state where the panels
are removed from the frame structure 26, the user or the worker can easily access
the devices inside the compressor 12 from an opening portion of the frame structure
26, and can efficiently perform maintenance work or manufacturing work of the compressor
12.
[0034] For example, on a back surface of the compressor casing 24, a rectangular back outer
frame 26a that is provided to surround the back surface and that configures a part
of the frame structure 26 is provided. Each of four sides of the rectangular shape
of the back panel 24b is removably attached to the back outer frame 26a. Both ends
of an upper part of the back outer frame 26a are connected to both ends of an upper
edge of the front panel 24a by two side frames 26b, and a lower part of the back outer
frame 26a is connected to a rear edge of the bottom panel 24d. In addition, a lower
edge of the front panel 24a is connected to a front edge of the bottom panel 24d.
Four sides of the upper panel 24c are removably attached to upper parts of the back
outer frame 26a and the front panel 24a and the two side frames 26b. Four sides of
the side panels 24e and 24f are removably attached to side portions of the back outer
frame 26a and the front panel 24a, the side frame 26b, and the bottom panel 24d.
[0035] As described above, the main components of the compressor 12, such as the compressor
main body 16, the heat exchanger 22, the oil separator 34, the adsorber 35, the storage
tank 36, and the control device 50, are accommodated in the compressor casing 24.
The oil separator 34, the adsorber 35, and the storage tank 36 are installed on the
bottom panel 24d close to one side panel 24e, and are disposed in the compressor casing
24. The adsorber 35, the storage tank 36, and the oil separator 34 are arranged in
this order from the front panel 24a toward the back panel 24b. In addition, the compressor
main body 16 and the control device 50 are disposed in the compressor casing 24 close
to the other side panel 24f. As described above, the control device 50 may be attached
to the front panel 24a, and the compressor main body 16 may be installed on the bottom
panel 24d between the control device 50 and the back panel 24b.
[0036] The heat exchanger 22 includes a double pipe 28 disposed along at least one surface
of the compressor casing 24, in this embodiment, along the back surface of the compressor
casing 24. The double pipe 28 is supported by the back outer frame 26a. When the back
panel 24b is attached to the back outer frame 26a, the heat exchanger 22 is covered
and hidden by the back panel 24b.
[0037] Fig. 4 is a schematic front view of the heat exchanger 22 according to the embodiment.
Fig. 4 shows a state in which the heat exchanger 22 and the back outer frame 26a are
viewed from the inside of the compressor 12 (that is, from inside the compressor casing
24) in a state where the back panel 24b is removed.
[0038] As shown in Figs. 3 and 4, the double pipe 28 includes a first portion 28a and a
second portion 28b. The first portion 28a of the double pipe 28 functions as the refrigerant
gas cooler 22a of the heat exchanger 22 shown in Fig. 1, and the second portion 28b
functions as the oil cooler 22b.
[0039] As shown in Fig. 4, a refrigerant gas inlet 54a and a first cooling medium outlet
56b are provided at one end of the first portion 28a of the double pipe 28, and a
refrigerant gas outlet 54b and a first cooling medium inlet 56a are provided at the
other end. As shown in Fig. 1, the refrigerant gas inlet 54a is connected to the discharge
port of the compressor main body 16, and the high-temperature and high-pressure refrigerant
gas pressurized by the compressor main body 16 flows into the refrigerant gas cooler
22a (that is, the first portion 28a) through the refrigerant gas inlet 54a. The cooling
medium (for example, cooling water as described above) supplied to the compressor
12 from the cooling medium intake 44 flows into the refrigerant gas cooler 22a from
the first cooling medium inlet 56a, cools the refrigerant gas through heat exchange,
and flows out from the first cooling medium outlet 56b. The refrigerant gas outlet
54b is connected to the oil separator 34, and the cooled high-pressure refrigerant
gas is supplied to the oil separator through the first cooling medium outlet 56b.
[0040] The first portion 28a of the double pipe 28 is bent along at least two adjacent sides
of the back surface of the compressor casing 24, in this embodiment, along three adjacent
sides. As shown in Figs. 3 and 4, the first portion 28a is bent in a substantially
C-shape along an upper side and a lateral side of the back outer frame 26a and along
a rear edge of the bottom panel 24d. In this way, the first portion 28a is disposed
to leave a space at a center portion of the back surface of the compressor casing
24.
[0041] In addition, an oil inlet 58a and a second cooling medium outlet 60b are provided
at one end of the second portion 28b of the double pipe 28, and an oil outlet 58b
and a second cooling medium inlet 60a are provided at the other end. As shown in Fig.
1, the oil inlet 58a is connected to the oil outlet of the compressor main body 16,
and the oil flowing out from the compressor main body 16 flows into the oil cooler
22b (that is, the second portion 28b) through the oil inlet 58a. As shown in Fig.
4, the second cooling medium inlet 60a is connected to the first cooling medium outlet
56b, and the cooling medium flows into the second portion 28b from the first portion
28a, cools the oil through heat exchange, and flows out from the second cooling medium
outlet 60b. As shown in Fig. 1, the second cooling medium outlet 60b is connected
to the cooling medium discharge port 45, and the cooling medium used for cooling the
refrigerant gas and the oil is discharged from the compressor 12 through the cooling
medium discharge port 45. The oil outlet 58b is connected to the oil inlet of the
compressor main body 16, and the cooled oil is returned to the compressor main body
16.
[0042] The second portion 28b of the double pipe 28 is bent in a spiral shape along the
back surface of the compressor casing 24. The second portion 28b is disposed inside
the first portion 28a on the back surface of the compressor casing 24. In this way,
the second portion 28b is disposed to leave a space at the center portion of the back
surface of the compressor casing 24. An opening portion 62 in which the double pipe
28 is not disposed is formed inside the second portion 28b, that is, in the center
portion of the back surface of the compressor casing 24.
[0043] The double pipe 28 is supported by the back outer frame 26a. As an example, as shown
in Fig. 4, the double pipe 28 may be fixed to the back outer frame 26a by using a
support material 64. In this example, two support materials 64 are attached to each
of left and right lateral sides of the back outer frame 26a. One end of the support
material 64 is attached to the back outer frame 26a by an appropriate method such
as screwing, and the other end extends horizontally toward the opening portion 62.
A hole into which the double pipe 28 is inserted is formed in the support material
64, and the double pipe 28 is inserted into the hole of the support material 64 and
attached to the support material 64 by an appropriate method such as soldering.
[0044] Fig. 5A is a schematic top view showing disposition of devices inside the compressor
12 according to the embodiment, and Fig. 5B is a schematic top view showing disposition
of devices inside a compressor 112 according to a comparative example. Figs. 5A and
5B show a state in which the upper panel 24c is removed from the compressor casing
24. In addition, for the sake of simplicity, the illustration of the pipe connecting
the components of the compressor 12 or 112 to each other is omitted in each drawing.
[0045] As described above, the compressor 12 includes the compressor main body 16, the heat
exchanger 22, the oil separator 34, the adsorber 35, the storage tank 36, and the
control device 50. As shown in Fig. 5A, the compressor main body 16 and the control
device 50 are disposed in a half area between the front panel 24a and the back panel
24b of the compressor casing 24, and the oil separator 34, the adsorber 35, and the
storage tank 36 are disposed in the remaining half area. The heat exchanger 22 is
disposed along the back panel 24b.
[0046] On the other hand, in the compressor 112 of the existing design shown in Fig. 5B,
the compressor main body 16, a heat exchanger 122, and the control device 50 are disposed
in a half area between the front panel 24a and the back panel 24b of the compressor
casing 24, and the oil separator 34, the adsorber 35, and the storage tank 36 are
disposed in the remaining half area. The heat exchanger 122 is disposed between the
compressor main body 16 and the control device 50, and may be, for example, a plate
type heat exchanger.
[0047] In the disposition of the devices of the compressor 112 shown in Fig. 5B, the heat
exchanger 122 occupies a relatively large footprint between the compressor main body
16 and the control device 50 in order to provide a desired cooling performance. Therefore,
as can be understood from the comparison between Figs. 5A and 5B, the footprint allowed
for the compressor main body 16 and the control device 50 is restricted.
[0048] On the other hand, according to the embodiment, as shown in Fig. 5A, the heat exchanger
22 is disposed along at least one surface of the compressor casing 24, for example,
along the back surface. A space adjacent to a surface of the compressor casing 24
is a dead space and is not used in the existing design. By using this space to house
the heat exchanger 22, a footprint for other devices such as the compressor main body
16 and the control device 50 can be expanded. Therefore, a degree of freedom in the
disposition of the devices in the compressor 12 is increased, which is advantageous.
In addition, in recent years, there is a tendency to require a large-sized control
device 50 to be mounted on the compressor 12 in order to implement advanced control.
According to the embodiment, in response to such a requirement, it is easy and advantageous
to secure sufficient space for installation of the control device 50.
[0049] In addition, according to the embodiment, the double pipe 28 of the heat exchanger
22 is bent along an outer periphery of the surface of the compressor casing 24. For
example, as described above, the first portion 28a is bent along at least two adjacent
sides of the back surface of the compressor casing 24, and the second portion 28b
is bent in a spiral shape along the back surface of the compressor casing 24. By using
the bent pipe having such a shape, the total length of the heat exchanger 22 can be
easily increased while suppressing an increase in the footprint of the heat exchanger
22. In particular, compared to the plate type heat exchanger that can be mounted on
the existing compressor, the heat exchanger 22 according to the embodiment can reduce
the footprint. As described above, suppressing the increase in the footprint is useful
in improving the degree of freedom in the disposition of other devices inside the
compressor 12. Increasing the total length of the heat exchanger 22 is helpful in
improving the cooling performance of the double pipe-type heat exchanger 22.
[0050] According to the embodiment, the heat exchanger 22 is disposed so as to leave a space
at the center portion of the surface of the compressor casing 24 in which the double
pipe 28 is disposed. Accordingly, the opening portion 62 in which the double pipe
28 is not disposed is formed at the center portion of the surface of the compressor
casing 24. In the manufacturing process of the compressor 12 or in maintenance work
of the compressor 12 at a site where the compressor 12 is used, the worker can easily
access the devices inside the compressor 12 from the opening portion 62. For example,
the manufacturing work such as pipe welding and joint fastening and various kinds
of maintenance work (for example, replacement of consumables such as filters and replacement
and repair of devices such as failed sensors) can be performed through the opening
portion 62. In this way, the disposition of the double pipe 28 having a vacant center
portion is useful in improving the efficiency of the manufacturing and maintenance
of the compressor 12.
[0051] In the existing compressor, a design is adopted in which a panel itself forming each
surface of the compressor casing is responsible for structural strength, so that a
plate thickness of the panel is large, and a weight thereof tends to be large. Therefore,
the work of attaching the panel in the manufacturing process or the work of removing
the panel in the maintenance work is not easy, which is one of causes of a decrease
in workability for the worker.
[0052] On the other hand, according to the embodiment, the compressor casing 24 includes
the frame structure 26 that is responsible for structural strength, so that each panel
such as the back panel 24b attached to the frame structure 26 can be thinned and weight-saved.
Such a casing structure is also useful in improving workability. In addition, the
thinning of the panel is also useful in securing a housing space for the heat exchanger
22.
[0053] The present invention has been described above based on the examples. It will be
understood by those skilled in the art that the present invention is not limited to
the embodiment, various modification examples are possible, and such modification
examples are also within the scope of the present invention. Various features described
concerning a certain embodiment are also applicable to other embodiments. A new embodiment
resulting from combinations also has the effects of each of the combined embodiments.
[0054] In the above-described embodiment, the heat exchanger 22 is disposed along the back
surface of the compressor casing 24. However, this is an example, and the present
invention is not limited thereto. The heat exchanger 22 may be disposed along another
surface (for example, an upper surface or a side surface) of the compressor casing
24.
[0055] In addition, in the above-described embodiment, a case where the heat exchanger 22
is disposed along only a single surface (that is, a back surface) of the compressor
casing 24 has been described as an example, but the heat exchanger 22 can be disposed
in other manners. For example, the heat exchanger 22 may be disposed along at least
two adjacent surfaces (for example, a back surface and an upper surface, or a back
surface and a side surface) of the compressor casing 24.
[0056] The bending shape of the double pipe 28 is not limited to the spiral shape. For example,
the double pipe 28 may be bent in a meandering shape along the surface of the compressor
casing 24.
[0057] Although the present invention has been described using specific words and phrases
based on the embodiment, the embodiment merely shows one aspect of the principle and
application of the present invention, and various modifications and improvements can
be made within the scope of the present invention described in claims.
Brief Description of the Reference Symbols
[0058]
- 10
- cryocooler
- 12
- compressor
- 22
- heat exchanger
- 24
- compressor casing
- 24b
- back panel
- 26a
- back outer frame
- 28
- double pipe