Embodiments of the present invention relate to a charged particle acceleration device and a method for adjusting a charged particle acceleration device.
In an accelerator, in order to control a beam trajectory of charged particles, a plurality of devices such as a bending electromagnet, a quadrupole electromagnet, and a screen monitor are installed along the beam trajectory. These control devices are required to be installed with high accuracy with respect to the beam trajectory. Thus, when these control devices are installed, alignment adjustment is performed to position these control devices with reference to the fixed point of the building. However, the accelerator also includes devices that are installed only during the adjustment and removed during normal operation as exemplified by an emittance monitor to be used only for adjusting an injector.
In construction of the accelerator as described above, a lot of time is spent because it is necessary to repeatedly perform precise alignment of the control devices every time the adjustment stage is switched to the normal state.
In view of the above-described circumstances, an object of embodiments of the present invention is to provide a charged particle acceleration device and a method for adjusting it, each of which eliminates the need for repeating alignment adjustment even in the case of repeating installation of the control devices.
Hereinafter, embodiments of the present invention will be described by referring to the accompanying drawings.
The charged particle acceleration device 10A (10) includes: controllers 15 (15a, 15b, 15c) configured to control a beam trajectory 12 of charged particles, which pass through ducts 11, and also configured such that the ducts 11 are inserted through the controllers 15; and stages 20 that are supported by a frame 16 fixed to a base (not shown) and reversibly move the controllers 15 in a direction of intersecting the beam trajectory 12.
In the charged particle acceleration device 10A (10), the beam trajectory 12 is formed by interconnecting a plurality of ducts 11 at the joint portions at both ends thereof. In detail, the joint portions (flange plates) of the adjacent ducts 11 facing each other are made to abut and fastened with screws or the like such that the plurality of ducts 11 are connected, and consequently, the beam trajectory 12 of moving charged particles is formed.
The plurality of controllers 15 (15a, 15b, 15c) such as a bending electromagnet, a quadrupole electromagnet, and a screen monitor are installed along the beam trajectory 12, and the trajectory of the charged particles moving in the internal space of the ducts 11 is controlled. Note that the controllers 15 are not limited to them.
Although the charged particle acceleration device 10A (10) is heavy, the frame 16 is a structure configured to support the charged particle acceleration device 10A (10) along the beam trajectory 12 and is built on a concrete-cast base (not shown). Although the frame 16 in the figure is exemplified as an H-steel coordinated horizontally in the longitudinal direction, its aspect is not particularly limited to it. The frame 16 can also be coordinated vertically or diagonally depending on the installation position of the controllers 15.
Each stage 20 includes: a fixing plate 22 to be fixed to the frame 16; a moving plate 21 to which controllers 15 are fixed; and a linear-motion driver (linear-motion mechanism) 23, wherein the moving plate 21 moves relative to the fixing plate 22 and the linear motion driver 23 axially rotates so as to move the moving plate 21 with respect to the fixing plate 22.
The bottom face of the moving plate 21 abuts on the top face of the fixing plate 22 so as to slide. While being restricted from moving along the beam trajectory 12, the moving plate 21 can move in the direction intersecting the beam trajectory 12 with a stroke width with which the controllers 15 do not interfere with the beam trajectory 12. Although it is not illustrated, the moving plate 21 positioned on the top face of the fixing plate 22 can be fixed at that position by using fastening members so as not to move with respect to the fixing plate 22.
The controllers 15 (15a, 15b, 15c) such as a bending electromagnet, a quadrupole electromagnet, and a screen monitor are installed on the moving plate 21 together with the duct 11 so as to penetrate the center of the trajectory through which the charged particles pass. The moving plate 21 on which these controllers 15 are installed is positioned on the top face of the fixing plate 22 and fixed with fastening members. The assembly of these controllers 15, each duct 11, and each stage 20 is performed at a location different from the installation location of the charged particle acceleration device 10A (10), and after being integrally assembled, it is transported to the installation location.
At the installation location of the charged particle acceleration device 10A (10), each stage 20 in which the controllers 15 and the duct 11 are integrally assembled is connected to the upper portion of the frame 16 with the use of a height-adjustable coupling member 28. Although a widely used combination of screws and nuts can be used as the coupling member 28, any member capable of stably fixing a high-gravity object and adjusting its height can be appropriately used as the coupling member 28.
These controllers 15 are required to be installed with high accuracy with respect to the beam trajectory 12. Thus, when each stage 20 in which these controllers 15 are installed is installed on the frame 16, alignment adjustment for positioning is performed with reference to the fixed point of the building while adjusting the height of the coupling member 28.
As shown in
Since the linear-motion driver 23 is configured as described above, the integrated structure of the duct 11 and the moving plate 21 can be evacuated to the side of the beam trajectory 12 from the position determined by the positioning and can be returned to the original position determined by the positioning with satisfactory reproducibility.
Although the storage space of the linear-motion driver 23 is provided in a groove shape on the top face of the fixing plate 22 in the drawing, the storage space may be a through hole in which the thick portion is perforated in parallel with the main face of the moving plate 21. The linear-motion driver 23 is not an essential component, and the integrated structure of the controllers 15, the duct 11 and the moving plate 21 may be moved by another method, for example, manually.
Thereafter, an adjuster 17 such as an emittance measurement device is disposed on the beam trajectory 12 after the controllers 15 are evacuated. This adjuster 17 is disposed on the beam trajectory 12 with adjustment ducts 18 at both ends. As shown in
When the adjustment stage of the charged particle acceleration device 10A (10) is completed, the adjuster 17 is removed from the frame 16 and the evacuated controllers 15 are returned to the beam trajectory 12. The controllers 15 return to the position of the original beam trajectory 12 with high reproducibility, and thus, realignment adjustment for the controllers 15 is unnecessary.
Next, the second embodiment of the present invention will be described by referring to
In the charged particle acceleration device 10B of the second embodiment, the stage 20 has the regulator 30 that regulates the movement of the moving plate 21 with respect to the fixing plate 22. As shown in
After attaching the controllers 15 and each stage 20 to the frame 16, until the alignment adjustment is completed, the regulator 30 is required to be fixed to the fixing plate 22 in the state where the abutting portion 31 is in contact with the moving plate 21. Since the regulator 30 is provided in this manner, at the time of returning the controllers 15 evacuated in the adjustment stage to the beam trajectory 12, the controllers 15 can be accurately returned to the original position by simply bringing the moving plate 21 into contact with the regulator 30.
Next, the third embodiment of the present invention will be described by referring to
In addition to the stage 20a where the controllers 15 (15a, 15b, 15c) are installed, the charged particle acceleration device 10C of the third embodiment further includes another stage 20b that reversibly moves the adjuster 17 to be operated in the adjustment stage in the direction of intersecting the beam trajectory 12. As a result, in the adjustment stage, the work of alternately replacing the controllers 15 and the adjuster 17 for positioning the controllers 15 with respect to the beam trajectory 12 can be performed without realignment adjustment. Further, the stage 20b on which the adjuster 17 is installed can be removed as shown in
As shown in
Each fixing plate 22 is provided with a pair of dividing boundaries 35a at symmetrical positions centered on the beam trajectory 12. Each fixing plate 22 is configured to be trisected into three divisions by the pair of dividing boundaries 35a, and the three divisions are integrated at least in the adjustment stage. Similarly, each moving plate 21 is provided with a pair of dividing boundaries 35b at symmetrical positions centered on the beam trajectory 12. Each moving plate 21 is configured to be trisected into three divisions by the pair of dividing boundaries 35b, and the three divisions are integrated at least in the adjustment stage. Since those components are configured as described above, after the adjustment stage is completed, unnecessary areas of the fixing plates 22 and the moving plates 21 can be removed, and the surrounding space of the charged particle acceleration device 10 can be secured.
An adjustment method of the charged particle acceleration device according to each embodiment will be described on the basis of the flowchart of
First, in the step S11, as shown in
In the step S12, alignment adjustment for the beam trajectory 12 is performed.
Next, the beam adjustment process is started.
In the step S13, the stage 20 is moved such that the controllers 15 are evacuated from the beam trajectory 12 as shown in
In the step S14, the adjuster 17 is disposed at the beam trajectory 12.
After making such a state, in the step S15, charged particles are emitted from an injector (not shown) and incident conditions of the charged particles are adjusted.
After the adjustment of the incident conditions of the charged particles is completed, the adjuster 17 is evacuated from the beam trajectory 12 in the step S16, and the stage 20 is moved to return the controllers 15 to the beam trajectory 12 in the step S17. The steps S13 to S17 are repeated until the beam adjustment process is completed (step S18 No Yes, END).
According to the charged particle acceleration device of at least one embodiment described above, the stage for reversibly moving the controller(s) in the direction intersecting the beam trajectory is provided, which eliminates the need for repeating the alignment adjustment even in the case of repeating installation of the controller(s).
While certain embodiments have been described, these embodiments have been presented by way of example only, and are not intended to limit the scope of the inventions. These embodiments may be embodied in a variety of other forms, and various omissions, substitutions, and changes may be made without departing from the spirit of the inventions. These embodiments and their modifications are included in the accompanying claims and their equivalents as well as included in the scope and gist of the inventions.
Number | Date | Country | Kind |
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2019-085396 | Apr 2019 | JP | national |
This application is a Continuation Application of No. PCT/JP2020/017066, filed on Apr. 20, 2020, and the PCT application is based upon and claims the benefit of priority from Japanese Patent Application No. 2019-085396, filed on Apr. 26, 2019, the entire contents of which are incorporated herein by reference.
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Number | Date | Country | |
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Number | Date | Country | |
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Parent | PCT/JP2020/017066 | Apr 2020 | US |
Child | 17447342 | US |