ACCELERATOR AND CYCLOTRON

Information

  • Patent Application
  • 20110291484
  • Publication Number
    20110291484
  • Date Filed
    May 23, 2011
    13 years ago
  • Date Published
    December 01, 2011
    12 years ago
Abstract
An accelerator includes an inflector through which a beam entering from an ion source passes and which introduces the beam to an acceleration orbit. The inflector includes a beam convergence unit that converges the beam passing through the inflector. A cyclotron, which accelerates a beam in a convoluted acceleration orbit, includes magnetic poles, D-electrodes, and an inflector. The magnetic poles generate a magnetic field in a direction perpendicular to the acceleration orbit. The D-electrodes generate a potential difference, which accelerates the beam, in the acceleration orbit. A beam, which enters in an incident direction perpendicular to the acceleration orbit, passes through the inflector, and the inflector bends the beam so as to introduce the beam to the acceleration orbit. The inflector includes a beam convergence unit that converges the beam passing through the inflector.
Description
RELATED APPLICATION

Priority is claimed to Japanese Patent Application No. 2010-120716, filed May 26, 2010, the entire content of which is incorporated herein by reference.


BACKGROUND

1. Technical Field


The present invention relates to a cyclotron and an accelerator including an inflector that introduces a beam to an acceleration orbit.


2. Description of the Related Art


In the past, a cyclotron has been known as a technique in this field. The cyclotron accelerates a beam in a convoluted acceleration orbit by the actions of magnetic poles and D-electrodes in an acceleration space, and outputs the beam. The beam enters the cyclotron in the incident direction perpendicular to the acceleration orbit. Further, the cyclotron can make the beam go into the acceleration orbit in the acceleration space by bending the beam, which is emitted from a beam source, at an angle of 90° by an inflector.


SUMMARY

According to an embodiment of the invention, there is provided an accelerator including an inflector through which a beam entering from an ion source passes and which introduces the beam to an acceleration orbit. The inflector includes a beam convergence unit that converges the beam passing through the inflector.


Further, according to another embodiment of the invention, there is provided a cyclotron that accelerates a beam in a convoluted acceleration orbit. The cyclotron includes magnetic poles that generate a magnetic field in a direction perpendicular to the acceleration orbit; D-electrodes generating a potential difference, which accelerates the beam, in the acceleration orbit; and an inflector through which a beam entering in an incident direction perpendicular to the acceleration orbit passes and which bends the beam so as to introduce the beam to the acceleration orbit. The inflector includes a beam convergence unit that converges the beam passing through the inflector.





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a perspective view of an accelerator (cyclotron) according to an embodiment of the invention.



FIG. 2 is a perspective view of a spiral inflector of the cyclotron shown in FIG. 1



FIGS. 3A, 3B, and 3C are views schematically showing the cross-sectional shape of a positive electrode and a negative electrode.



FIG. 4 is a perspective view showing an inflector similar to the spiral inflector shown in FIG. 2.



FIG. 5 is a graph showing the result of a simulation that is performed by the inventors.



FIG. 6 is a graph showing the result of a simulation that is performed by the inventors.



FIG. 7 is a schematic cross-sectional view showing the cross-section of another example of the inflector that that is perpendicular to a passing orbit.



FIG. 8 is a plan view showing the vicinity of a beam outlet of still another example of the inflector as seen from above.





DETAILED DESCRIPTION

In this kind of accelerator, the beam to be introduced to the acceleration orbit is diffused, so that a part of the beam collides with inner walls partitioning the acceleration space and disappears. A ratio of a beam, which is finally output from the accelerator, is decreased by the loss of the beam. Accordingly, in order to increase the ratio of the beam, which is finally obtained, in this kind of accelerator, there is a demand for the suppression of the diffusion of the beam to be introduced to the acceleration orbit in order to reduce a beam colliding with the inner walls of the acceleration space.


Accordingly, it is desirable to provide a cyclotron and an accelerator that can suppress the diffusion of a beam to be introduced to an acceleration orbit.


In the accelerator, the inflector includes the beam convergence unit. Accordingly, the beam entering from the ion source is converged by the beam convergence unit of the inflector and introduced to the acceleration orbit, so that it may be possible to suppress the diffusion of the beam to be introduced to the acceleration orbit.


Specifically, the beam convergence unit may generate a distorted quadrupole-component electric field in a beam passing area through which the beam passes. In this case, the beam passing through the inflector is converged by the distorted quadrupole-component electric field generated by the beam convergence unit. Accordingly, the diffusion of the beam to be introduced to the acceleration orbit is suppressed.


Further, the inflector may include positive and negative electrodes facing each other with a gap, which forms the beam passing area, therebetween. The positive and negative electrodes may be formed so that the width of the gap is not constant in a cross-section perpendicular to a traveling direction of the beam.


In this case, an electric field, which is caused by the positive and negative electrodes, is generated in the beam passing area the inflector. Further, since the gap between the positive and negative electrodes is not constant in the cross-section perpendicular to the traveling direction of the beam, the beam is affected by an electric field corresponding to the passing position of the cross-section and is bent according to the passing position. Accordingly, it may be possible to converge the beam that passes through the beam passing area.


Specifically, the acceleration orbit may have a convoluted shape, and the width of the gap may be increased toward a position corresponding to the outer side of the acceleration orbit, which has the convoluted shape, in the cross-section perpendicular to the traveling direction of the beam.


Moreover, the acceleration orbit may have a convoluted shape; the beam convergence unit may generate an electric field in a beam passing area through which the beam passes; and the intensity of the electric field may become weak toward a position corresponding to the outer side of the acceleration orbit, which has the convoluted shape, in a cross-section perpendicular to a traveling direction of the beam.


In the cyclotron, the inflector includes the beam convergence unit. Accordingly, the beam entering from the ion source is converged by the beam convergence unit of the inflector and introduced to the acceleration orbit, so that it may be possible to suppress the diffusion of the beam to be introduced to the acceleration orbit.


According to the accelerator and the cyclotron of the embodiments of the invention, it may be possible to suppress the diffusion of the beam to be introduced to the acceleration orbit.


A cyclotron and an accelerator according to preferred embodiments of the invention will be described below in detail with reference to the drawings.


A cyclotron 1 shown in FIG. 1 is an accelerator that accelerates an ion particle beam B entering from an ion source 11 and outputs the beam. The cyclotron 1 has an acceleration space 5 which has a circular shape in plan view and through which the beam B passes and is accelerated. Here, the cyclotron 1 is installed so that the acceleration space 5 extends horizontally. When used in the following description, words including the concepts of “upper” and “lower” correspond to the upper and lower sides of the cyclotron 1 that is in a state shown in FIG. 1. Further, when necessary, an xyz coordinate system, which uses a z-axis as a vertical axis and uses an x-y plane as a horizontal plane, may be set as shown in FIG. 1 and x, y, and z may be used for descriptive purposes.


The cyclotron 1 includes magnetic poles 7 that are provided above and below the acceleration space 5. Meanwhile, the magnetic pole 7 provided above the acceleration space 5 is not shown. The magnetic poles 7 generate a vertical magnetic field in the acceleration space 5. Further, the cyclotron 1 includes a plurality of D-electrodes 9 that has fan shape in plan view. The D-electrode 9 has a cavity that passes through the D-electrode in a circumferential direction, and the cavity forms a part of the acceleration space 5. When alternating current is supplied to the plurality of D-electrodes 9, the D-electrodes 9 generate a potential difference in the circumferential direction in the acceleration space 5. Accordingly, a beam B is accelerated by the potential difference. A beam B, which is introduced substantially to the center of the acceleration space 5, is accelerated by the actions of the magnetic field generated by the magnetic poles 7 and the electric field generated by the D-electrodes 9 while forming an acceleration orbit T, which has a convoluted shape on the horizontal plane, in the acceleration space 5. The accelerated beam B is finally output in the tangential direction of the acceleration orbit T. Since the above-mentioned structure of the cyclotron 1 is well-known, more detailed description thereof will be omitted.


The ion beam B is generated by the ion source 11 provided below the cyclotron 1, and enters the cyclotron 1 in an incident direction, which is directed vertically upward, through two solenoids 13. Meanwhile, the solenoids 13 function to prevent the beam B from being diffused. The beam B, which enters in the vertical direction, needs to be bent to the horizontal direction in the cyclotron 1 so that the beam B is introduced to the acceleration orbit T. Accordingly, the cyclotron 1 includes a spiral inflector 21 that is provided at the center of the acceleration space 5. The inflector 21 bends the beam B entering from below, and emits the beam in the horizontal direction substantially at the center of the acceleration space 5. The emitted beam B is introduced to the above-mentioned acceleration orbit T and accelerated.


As shown in FIG. 2, the inflector 21 includes positive and negative electrodes 23 and 27 that are formed of metal blocks (for example, copper blocks) and face each other. The positive and negative electrodes 23 and 27 are connected to different constant-voltage power sources (not shown), respectively. A positive electrode surface 23a, which forms a curved surface having the shape of a twisted strip, is formed on the surface of the positive electrode 23, and a negative electrode surface 27a, which forms a curved surface having the shape of a twisted strip, is formed on the surface of the negative electrode 27. The positive and negative electrode surfaces 23a and 27a are positioned so as to face each other with a predetermined gap therebetween. An electric field, which is generated by the potential difference between the positive and negative electrodes 23 and 27, is formed in the spiral space that is formed of the gap. Meanwhile, the polarities of the electrodes 23 and 27 may be reversed according to the polarity (positive and negative) of ions that form the ion beam B.


The beam B, which is directed vertically upward, enters from a gap between the positive and negative electrode surfaces 23a and 27a at the lower portion of the inflector 21. The beam B, which has entered the gap, is affected by the electric field, which is generated by the potential difference between the positive and negative electrodes 23 and 27, and the magnetic field that is generated by the magnetic poles 7. Accordingly, the beam travels while being spirally bent along the gap. Further, the beam B is horizontally emitted from the gap between the positive and negative electrode surfaces 23a and 27a at the upper portion of the inflector 21. After being emitted from the inflector 21, the beam B goes into the acceleration orbit T while being convoluted counterclockwise as seen from above. Meanwhile, an ideal passing orbit of a beam in the inflector 21 is denoted by reference character “S”. As described above, the spiral space, which is formed of the gap, serves as a beam passing area 25 through which a beam passes.


Subsequently, the width of the gap between the positive and negative electrodes 23 and 27 will be described.



FIG. 3 includes schematic cross-sectional views showing the cross-section, which is perpendicular to the passing orbit S, of the vicinity of the beam passing area 25. FIG. 3A shows the cross-section of the beam passing area at the position of the lower end surface of the inflector 21, FIG. 3B shows the cross-section of the beam passing area at an arbitrary position in the inflector 21, and FIG. 3C shows the cross-section of the beam passing area at an arbitrary position on the passing orbit S on the front side (downstream side) of the position of FIG. 3B. FIGS. 3a, 3b, and 3c are cross-sectional views as seen in a direction where the beam B on the passing orbit S travels to the front side from the back side of the plane of each drawing.


As shown in FIG. 3A, on the lower end surface of the inflector 21, the positive and negative electrode surfaces 23a and 27a are parallel to each other and the width g of the gap is constant. When an arbitrary cross-section is taken as shown in FIGS. 3B and 3C, the width g of the gap between the positive and negative electrodes 23 and 27 is not constant in the cross-section and is increased toward the left side in FIGS. 3B and 3C. Meanwhile, the left side in FIG. 3 corresponds to the outer side of the convoluted acceleration orbit T and the right side in FIG. 3 corresponds to the inner side of the convoluted acceleration orbit T.


In other words, when an arbitrary cross-section perpendicular to the passing orbit S is taken, the positive and negative electrodes 23 and 27 are formed so that the profiles of the positive and negative electrode surfaces 23a and 27a form a V shape. Further, FIG. 3C shows the cross-section of the beam passing area at the position on the passing orbit S on the front side (downstream side) of the position of FIG. 3B. As understood from the comparison of FIGS. 3B and 3C, the positive and negative electrodes 23 and 27 are formed in a three-dimensional shape where the difference between the widths g of the right and left portions of the gap is increased toward the front side on the gassing orbit S.


According to the setting of the width g of the gap described above, the distribution of an electric field, which is generated by the electrodes 23 and 27 and becomes weak toward the positron corresponding to the outer side of the acceleration orbit T (the left side in FIG. 3) and becomes strong toward the position corresponding to the inner side of the acceleration orbit T, is formed in the beam passing area 25. That is, as the passing position of the beam B is deviated to the left side in FIG. 3, a so-called distorted quadrupole-component electric field is generated in the beam passing area 25 so that a force applied to the beam B in a downward direction (or an upward direction) in FIG. 3 by the electric field is reduced. The structure of the electrodes 23 and 27, which generate the distorted quadrupole-component electric field, has a function as a beam convergence unit that converges the beam B passing through the inflector 21, particularly, in the vertical direction.


Accordingly, when a beam B passes through the beam passing area 25 where the distorted quadrupole-component electric field exists, the beam B introduced to the acceleration orbit T is converged, particularly, in the vertical direction (z-axis direction), so that the diffusion of the beam B in the vertical direction is suppressed. Further, since the diffusion of the beam B in the vertical direction is suppressed, the beams colliding with the inner walls the D-electrode 9 decreased in the acceleration space 5. As a result, it may be possible to increase the ratio of the beam B that is finally output from the cyclotron 1 (which may be referred to as the transmittance of the cyclotron).


If the width g of the gap is expressed by a specific expression as a specific example that obtains the above-mentioned width g of the gap, the following expression (1) is obtained.









g
=



g
o



1
+


k
′2



sin
2


b






(

1
-

η


w

W
/
2



sin





b


)






[

Expression





1

]







g: the width of a gap at a predetermined position


go: the width of a gap at an inflector inlet


k′: tilt parameter


b: b=s/A


s: a distance between the inflector inlet and the predetermined position measured along a passing orbit S


A: the height of the inflector


η: the intensity of a distorted quadrupole-component electric field


W: the width of the inflector


w: the position of the predetermined position in the width (W) direction


Meanwhile, the height A of the inflector means a length between an inflector inlet of the beam B and an inflector outlet of the beam B that is measured in the vertical direction. The inlet of the beam B is a theoretical position where the application of an electric field generated by the electrodes 23 and 27 to the beam B starts, and is positioned slightly below the lower end surface of the inflector 21. Further, the outlet of the beam B is a theoretical position where the application of an electric field generated by the electrodes 23 and 27 to the beam B is terminated, and is positioned slightly in front of the positions of the upper ends of the positive and negative electrode surfaces 23a and 27a in the traveling direction of the beam B. The tilt parameter k′ is a parameter that represents the tilt of the beam passing area 25 in the plane perpendicular to the passing orbit S. Further, the width W of the inflector means the width of the beam passing area 25. At the inflector inlet, “b=0” is satisfied and the positive and negative electrode surfaces 23a and 27a are parallel to each other. Furthermore, “b=π/2” is satisfied at the inflector outlet. As understood from Expression (1), the width g of the gap depends on w.


Meanwhile, for the purpose of comparison, another type of spiral inflector (hereinafter, referred to as a “similar inflector”) 121 similar to the inflector 21 is shown in FIG. 4. In this similar inflector 121, a gap between positive and negative electrodes 123 and 127 is constant in all the cross-sections perpendicular to a passing orbit S′ of a beam B. That is, the positive and negative electrodes 123 and 127 are formed so that the profiles of positive and negative electrode surfaces 123a and 127a appearing in all the cross-sections perpendicular to the passing orbit S′ are parallel to each other. In the similar inflector 121, only bipolar components of an electric field of a beam passing area 125 are generated. For this reason, the advantage of converging a beam as in the inflector 21 is not obtained.


Subsequently, a simulation, which is performed by the inventors for confirmation of the advantage of the inflector 21, will be described.


Here, a simulation where 5000 ion particles of a beam pass through the inflector 21 is performed. z values and z′ values of the ion particles at the outlet of the inflector 21 are plotted, and the distribution thereof is shown in FIG. 5. The z value represents the passing position (mm) of the ion particle in the vertical direction, and the z′ value represents the traveling direction of the particle by an angle (mrad) from the horizontal plane. Further, for the purpose of comparison, the same simulation as described above is performed on the similar inflector 121 and the results are shown in FIG. 6.


From the comparison of FIGS. 5 and 6, it is found that the variations of the z values are small. This means that the upper and lower positions of the ion particles passing through the inflector 21 are uniform as compared to the similar inflector 121. Further, from comparison of FIGS. 5 and 6, it is found that the variations of the z′ values are small and have angles close to zero mrad. This means that the ion particles passing through the inflector 21 have a strong tendency to be emitted at an angle close to the horizontally as compared to the similar inflector 121. Accordingly, according to the inflector 21, it is confirmed that an advantage of converging a beam B in the vertical direction is obtained as compared to the similar inflector 121.


The invention is not limited to the above-mentioned embodiment. For example, in the embodiment, the cyclotron 1 has been installed so that the acceleration space 5 extends horizontally. However, the invention may also be applied to an accelerator of which an acceleration space is disposed along a vertical plane. Further, the invention is not limited to a cyclotron and may also be applied to a synchrocyclotron (accelerator).


Furthermore, the above-mentioned gap may be formed by using a pair of plate-like electrodes, which is twisted and has a uniform thickness, instead of the electrodes 23 and 27 formed of metal blocks, and disposing the electrodes so that a V-shaped cross-section is formed. Moreover, in order to form the structure where the width g of the gap depends on w, for example, a metal member 129 having a triangular cross-section may be bonded to the negative electrode surface 127a of the similar inflector 121 as shown in FIG. 7. Further, in order to form a distorted quadrupole-component electric field in the beam passing area 25, distorted quadrupole magnets may be installed in front of the beam outlet of the similar inflector 121. Furthermore, in order to form a distorted quadrupole-component electric field in the beam passing area 25, the lengths of the electrodes 127 and 123 of the similar inflector 121 seen from above may be set to be long up to a position corresponding to the inner side of the acceleration orbit T in the traveling direction of a beam as shown in FIG. 8.


It should be understood that the invention is not limited to the above-described embodiment, but may be modified into various forms on the basis of the spirit of the invention. Additionally, the modifications are included in the scope of the invention.

Claims
  • 1. A working machine comprising: a working motor which is driven by an operator's operation;a DC busbar which is connected to the working motor via a first inverter circuit;a storage battery which is connected to the DC busbar via a DC voltage converter and a switch;a control unit which controls the first inverter circuit, the DC voltage converter, and the switch;a cooling motor which drives a cooling fan and/or a cooling liquid circulating pump used for cooling at least one of the first inverter circuit, the DC voltage converter, and the control unit; anda cooling motor driving circuit which is connected between the cooling motor and the DC busbar and is controlled by the control unit to drive the cooling motor,wherein the control unit includes a busbar voltage lowering mode decreasing a voltage of the DC busbar when the operation of the working machine is stopped, and decreases the voltage of the DC busbar in a manner such that the cooling motor driving circuit is operated after the switch enters a disconnection state to consume electricity in the cooling motor in the busbar voltage lowering mode.
  • 2. The working machine according to claim 1, wherein the control unit stops the operation of the cooling motor driving circuit when the voltage of the DC busbar becomes a predetermined value or less in the busbar voltage lowering mode.
  • 3. The working machine according to claim 1, wherein the control unit charges the storage battery by driving the DC voltage converter before the switch enters a disconnection state when the voltage of the DC busbar is higher than that of the storage battery upon starting the busbar voltage lowering mode.
  • 4. The working machine according to claim 1, wherein the control unit starts the busbar voltage lowering mode whenever the operation of the working machine is stopped.
  • 5. The working machine according to claim 1, wherein the control unit starts the busbar voltage lowering mode when there is an input from the operator while the operation of the working machine is stopped.
  • 6. The working machine according to claim 1, further comprising: an internal combustion engine;a first cooling liquid circulating system which includes a first heat exchanger cooling the internal combustion engine; anda second cooling liquid circulating system which includes a second heat exchanger provided separately from the first cooling liquid circulating system to cool the first inverter circuit and the DC voltage converter.
  • 7. The working machine according to claim 6, wherein the DC voltage converter includes a reactor, andwherein the second cooling liquid circulating system cools the reactor.
  • 8. The working machine according to claim 1, further comprising: a plurality of driver units which includes an inverter unit having the first inverter circuit with an intelligent power module and a step-up/step-down converter unit having the DC voltage converter with an intelligent power module,wherein the plurality of driver units includes a second temperature sensor which is provided outside the intelligent power module to detect the temperature of the intelligent power module in addition to a first temperature sensor built in the intelligent power module, andwherein when a temperature detection result obtained by the second temperature sensor is higher than a predetermined first threshold value lower than a temperature where an overheat protection function of the intelligent power module is operated by the first temperature sensor, the control unit decreases a maximum driving current to the working motor when the driver unit is the inverter unit and decreases a maximum discharging current from the storage battery and/or a maximum charging current to the storage battery when the driver unit is the step-up/step-down converter unit.
  • 9. The working machine according to claim 8, wherein the plurality of driver units each includes a casing accommodating the first inverter circuit or the DC voltage converter and is disposed in parallel along a predetermined direction, andwherein the casings of the adjacent driver units are fixed to each other by a fastening tool.
  • 10. The working machine according to claim 8, further comprising: a control unit which serves as the control unit,wherein the control unit includes a casing which has a sealing structure, a plurality of CPUs which is provided inside the casing and controls the DC voltage converters and the inverter circuits of the plurality of driver units, and a cooling pipe which is thermally coupled to the plurality of CPUs and cools the plurality of CPUs by introducing a cooling liquid from the outside of the casing.
  • 11. The working machine according to claim 8, further comprising: a casing which fixes the inverter unit and the step-up/step-down converter unit,wherein an input terminal of the inverter unit and an input terminal of the step-up/step-down converter unit are connected to a DC bus formed as a busbar.
  • 12. The working machine according to claim 1, further comprising: a cooling device which cools the first inverter circuit; anda temperature detection means which detects the temperature of a refrigerant in the cooling device,wherein the first inverter circuit includes a mechanism which stops a supply of current for driving the working motor when detecting that the temperature of the first inverter circuit becomes a predetermined operation stop temperature or higher,wherein when the temperature of the refrigerant obtained from the temperature detection means is higher than a predetermined output suppressing temperature, the control unit compares the state with the case where the temperature of the refrigerant is the output suppressing temperature or lower and controls the first inverter circuit to decrease an upper limit value of a current supplied to the working motor, andwherein the output suppressing temperature is lower than the operation stop temperature.
  • 13. The working machine according to claim 2, wherein the control unit charges the storage battery by driving the DC voltage converter before the switch enters a disconnection state when the voltage of the DC busbar is higher than that of the storage battery upon starting the busbar voltage lowering mode.
  • 14. The working machine according to claim 2, wherein the control unit starts the busbar voltage lowering mode whenever the operation of the working machine is stopped.
  • 15. The working machine according to claim 2, wherein the control unit starts the busbar voltage lowering mode when there is an input from the operator while the operation of the working machine is stopped.
  • 16. The working machine according to claim 6, further comprising: a plurality of driver units which includes an inverter unit having the first inverter circuit with an intelligent power module and a step-up/step-down converter unit having the DC voltage converter with an intelligent power module,wherein the plurality of driver units includes a second temperature sensor which is provided outside the intelligent power module to detect the temperature of the intelligent power module in addition to a first temperature sensor built in the intelligent power module, andwherein when a temperature detection result obtained by the second temperature sensor is higher than a predetermined first threshold value lower than a temperature where an overheat protection function of the intelligent power module is operated by the first temperature sensor, the control unit decreases a maximum driving current to the working motor when the driver unit is the inverter unit and decreases a maximum discharging current from the storage battery and/or a maximum charging current to the storage battery when the driver unit is the step-up/step-down converter unit.
  • 17. The working machine according to claim 16, wherein the DC voltage converter includes a reactor, andwherein the second cooling liquid circulating system cools the reactor.
  • 18. The working machine according to claim 9, further comprising: a control unit which serves as the control unit,wherein the control unit includes a casing which has a sealing structure, a plurality of CPUs which is provided inside the casing and controls the DC voltage converters and the inverter circuits of the plurality of driver units, and a cooling pipe which is thermally coupled to the plurality of CPUs and cools the plurality of CPUs by introducing a cooling liquid from the outside of the casing.
  • 19. The working machine according to claim 9, further comprising: a casing which fixes the inverter unit and the step-up/step-down converter unit,wherein an input terminal of the inverter unit and an input terminal of the step-up/step-down converter unit are connected to a DC bus formed as a busbar.
  • 20. The working machine according to claim 19, further comprising: a control unit which serves as the control unit,wherein the control unit includes a casing which has a sealing structure, a plurality of CPUs which is provided inside the casing and controls the DC voltage converters and the inverter circuits of the plurality of driver units, and a cooling pipe which is thermally coupled to the plurality of CPUs and cools the plurality of CPUs by introducing a cooling liquid from the outside of the casing.
Priority Claims (1)
Number Date Country Kind
2010-120716 May 2010 JP national