CN113035380A - Pop-up divertor probe system for magnetic confinement nuclear fusion device - Google Patents
Pop-up divertor probe system for magnetic confinement nuclear fusion device Download PDFInfo
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- CN113035380A CN113035380A CN202110213748.XA CN202110213748A CN113035380A CN 113035380 A CN113035380 A CN 113035380A CN 202110213748 A CN202110213748 A CN 202110213748A CN 113035380 A CN113035380 A CN 113035380A
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- divertor
- probe assembly
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- 239000000523 sample Substances 0.000 title claims abstract description 116
- 230000004927 fusion Effects 0.000 title claims abstract description 24
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 claims abstract description 20
- 229910002804 graphite Inorganic materials 0.000 claims abstract description 20
- 239000010439 graphite Substances 0.000 claims abstract description 20
- 239000000919 ceramic Substances 0.000 claims description 23
- 238000005192 partition Methods 0.000 claims description 11
- 229910010293 ceramic material Inorganic materials 0.000 claims description 4
- 125000006850 spacer group Chemical group 0.000 claims 1
- 238000004804 winding Methods 0.000 abstract description 6
- 230000007246 mechanism Effects 0.000 abstract description 5
- 238000003745 diagnosis Methods 0.000 abstract description 2
- 230000009347 mechanical transmission Effects 0.000 abstract description 2
- 210000002381 plasma Anatomy 0.000 abstract 1
- 239000000463 material Substances 0.000 description 5
- 230000008878 coupling Effects 0.000 description 4
- 238000010168 coupling process Methods 0.000 description 4
- 238000005859 coupling reaction Methods 0.000 description 4
- 238000005259 measurement Methods 0.000 description 3
- PNEYBMLMFCGWSK-UHFFFAOYSA-N Alumina Chemical compound [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 2
- 229920000049 Carbon (fiber) Polymers 0.000 description 2
- 230000005540 biological transmission Effects 0.000 description 2
- 239000004917 carbon fiber Substances 0.000 description 2
- 239000002131 composite material Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 2
- 229910052721 tungsten Inorganic materials 0.000 description 2
- 239000010937 tungsten Substances 0.000 description 2
- 229910052582 BN Inorganic materials 0.000 description 1
- PZNSFCLAULLKQX-UHFFFAOYSA-N Boron nitride Chemical compound N#B PZNSFCLAULLKQX-UHFFFAOYSA-N 0.000 description 1
- QZLJNVMRJXHARQ-UHFFFAOYSA-N [Zr].[Cr].[Cu] Chemical compound [Zr].[Cr].[Cu] QZLJNVMRJXHARQ-UHFFFAOYSA-N 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- SBYXRAKIOMOBFF-UHFFFAOYSA-N copper tungsten Chemical compound [Cu].[W] SBYXRAKIOMOBFF-UHFFFAOYSA-N 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 230000001050 lubricating effect Effects 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
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- 229910001220 stainless steel Inorganic materials 0.000 description 1
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Images
Classifications
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- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21B—FUSION REACTORS
- G21B1/00—Thermonuclear fusion reactors
- G21B1/11—Details
- G21B1/23—Optical systems, e.g. for irradiating targets, for heating plasma or for plasma diagnostics
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- G—PHYSICS
- G21—NUCLEAR PHYSICS; NUCLEAR ENGINEERING
- G21B—FUSION REACTORS
- G21B1/00—Thermonuclear fusion reactors
- G21B1/25—Maintenance, e.g. repair or remote inspection
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R1/00—Details of instruments or arrangements of the types included in groups G01R5/00 - G01R13/00 and G01R31/00
- G01R1/02—General constructional details
- G01R1/06—Measuring leads; Measuring probes
- G01R1/067—Measuring probes
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E30/00—Energy generation of nuclear origin
- Y02E30/10—Nuclear fusion reactors
Abstract
The invention belongs to the field of diagnosis of high-temperature plasmas of a magnetic confinement nuclear fusion device, and discloses a pop-up divertor probe system for the magnetic confinement nuclear fusion device, which comprises a supporting base, wherein a probe assembly module loaded with a rectangular graphite probe is arranged on the supporting base; the driving support module is arranged on the support base and used for driving the probe assembly module to move, so that the probe assembly module can be ejected or recovered; the coil box component module is rotatably arranged on the supporting base and is connected with the driving supporting module through a universal connecting shaft component; the basic principle that an electrified winding coil can generate electromagnetic torque under the condition of a magnetic field is adopted, a parallelogram framework is adopted as a driving mechanism, a universal connecting shaft assembly is adopted as a connecting mechanism, and accurate mechanical transmission is realized.
Description
Technical Field
The utility model belongs to the field of diagnosis of high-temperature plasma of a magnetic confinement nuclear fusion device, and particularly relates to a pop-up divertor probe system for a magnetic confinement nuclear fusion device.
Background
At present, divertor probes on Tokamak devices at home and abroad are basically installed on a divertor target plate in an embedded mode. Patent ZL201410437565.6 proposes a target plate probe system suitable for use in the full tungsten divertor of EAST tokamak apparatus, which is capable of measuring plasma parameters well in the EAST tungsten divertor region and is verified in the course of several experiments in EAST. ZL201711393247.4 has mentioned an integrated modularization probe system suitable for tungsten copper target plate, adopts integrated modular structure, and make full use of target plate space can wholly the dismouting, does not have the welded fastening structure, has independent water-cooling structure, probe simple structure. However, the two types of probes are embedded on the divertor target plate, and the plasma in the divertor target plate area is measured for a long time, and once the probes are installed, the probes are exposed in the plasma for a long time, so that the probes can be quickly ablated and damaged by high heat flow particle flow, the later measurement is affected, meanwhile, some unnecessary data can be measured in the actual measurement process, and the service life of the probes is wasted.
Disclosure of Invention
Aiming at the defects of the prior art, the purpose of the disclosure is to provide a pop-up divertor probe system for a magnetic confinement nuclear fusion device, which can be used in a high-intensity magnetic field high-temperature environment of the magnetic confinement nuclear fusion device, and has simple structure and stable and reliable transmission mechanism.
The purpose of the disclosure can be realized by the following technical scheme:
a pop-up divertor probe system for a magnetically confined nuclear fusion device comprises a support base, wherein a probe assembly module loaded with a rectangular graphite probe is arranged on the support base;
the driving support module is arranged on the support base and used for driving the probe assembly module to move, so that the probe assembly module can be ejected or recovered;
the coil box component module loaded with a coil is installed at the lower end of the supporting base, the coil box component module is rotatably installed on the supporting base, and the coil box component module is connected with the driving supporting module through a universal connecting shaft component.
Further, the drive support module comprises a drive connecting rod, a driven connecting rod and a probe assembly shaft, cylindrical holes are formed in two ends of the drive connecting rod and two ends of the driven connecting rod respectively, the probe assembly module and the support base which are close to two ends of each accommodating hole are provided with the probe assembly shaft, and the probe assembly shaft penetrates through the cylindrical holes in two ends of the drive connecting rod and two ends of the driven connecting rod.
Furthermore, the probe assembly module comprises a plurality of probe assembly units which are mutually attached and linearly arranged.
Furthermore, the probe unit comprises a rectangular graphite probe, a ceramic partition plate, a wiring screw and a wire, wherein a first groove is formed in one surface of the ceramic partition plate, the rectangular graphite probe is embedded in the first groove, the top end of the rectangular graphite probe protrudes out of the first groove, a threaded hole is formed in the bottom of the rectangular graphite probe and is in threaded connection with the wiring screw, and the wiring screw is in clamping connection with the wire.
Furthermore, the tail ends of the probe assembly units which are mutually attached and linearly arranged are attached with a ceramic baffle plate, and the side surfaces of the probe assembly units and the ceramic baffle plate are wrapped by a first fixing frame, a second fixing frame, a first top plate and a second top plate;
the probe assembly shaft is arranged between the first fixing frame and the second fixing frame of the probe assembly module, and two ends of the probe assembly shaft are fixedly connected with the first fixing frame and the second fixing frame.
Furthermore, a rectangular second groove is formed between the first fixing frame and the second fixing frame, and the ceramic partition plates of all the probe assembly units are clamped in the second groove.
Further, the ceramic partition and the ceramic baffle are made of an insulating ceramic material.
Further, the coil box component module comprises a coil, the coil is wound on a winding drum, and a cylindrical through hole is formed in the middle of the winding drum;
the front surface of the coil box is provided with a square groove, the middle of the coil box is provided with a cylinder, the cylinder just passes through a cylinder hole in the middle of the winding drum so as to fix the winding drum, and the side surface of the coil box is provided with a rectangular groove for the coil to penetrate out and be connected with a power supply;
the coil box cover is matched with the coil box;
one end of the coil box is provided with a cylindrical through hole;
the coil box shaft just passes through the cylindrical through hole at one end of the coil box.
Further, the coil box shaft of the coil box assembly module is perpendicular to the rotating shaft of the driving connecting rod in the driving support module.
The beneficial effect of this disclosure:
the present disclosure uses the basic principle that an electrified winding coil can generate electromagnetic torque under a magnetic field condition, uses a parallelogram structure as a driving mechanism, and uses a universal connecting shaft assembly as a connecting mechanism, thereby realizing precise mechanical transmission.
Drawings
In order to more clearly illustrate the embodiments or technical solutions in the prior art of the present disclosure, the drawings used in the description of the embodiments or prior art will be briefly described below, and it is obvious for those skilled in the art that other drawings can be obtained based on these drawings without creative efforts.
FIG. 1 is an isometric view of a pop-up divertor probe system of a magnetically confined nuclear fusion device in this embodiment;
FIG. 2 is an exploded view of a probe assembly of the pop-up divertor probe system of the magnetically confined nuclear fusion device in this embodiment;
FIG. 3 is a front view of a pop-up divertor probe system of the magnetically confined nuclear fusion device in this embodiment;
FIG. 4 is a side view of a pop-up divertor probe system of a magnetically confined nuclear fusion device in this embodiment;
FIG. 5 is an exploded view of the coil box assembly of the pop-up divertor probe system of the magnetically confined nuclear fusion device in this embodiment.
Detailed Description
The technical solutions in the embodiments of the present disclosure will be clearly and completely described below with reference to the drawings in the embodiments of the present disclosure, and it is obvious that the described embodiments are only a part of the embodiments of the present disclosure, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments disclosed herein without making any creative effort, shall fall within the protection scope of the present disclosure.
As shown in fig. 1 to 5, a pop-up divertor probe system for a magnetic confinement nuclear fusion device comprises a support base 1, wherein a probe assembly module 30 loaded with a rectangular graphite probe 3 is arranged on the support base 1;
the driving support module 40 is installed on the support base 1, and the driving support module 40 is used for driving the probe assembly module 30 to move, so that the probe assembly module 30 can be ejected or recovered;
the coil box assembly module 8 loaded with the coil 803 is installed at the lower end of the supporting base 1, the coil box assembly module 8 is rotatably installed on the supporting base 1, and the coil box assembly module 8 is connected with the driving supporting module 40 through the universal connecting shaft assembly 7.
During the use, coil 803 in the coil box subassembly module 8 is circular telegram, circular telegram coil 803 can produce electromagnetic torque's basic principle under the magnetic field condition, make coil box subassembly module 8 do in the magnetic field around the connecting axle of being connected with support base 1 and rotate, pivoted coil box subassembly module 8 drives drive support module 40 through universal connecting axle coupling assembling and moves, drive support module 40 drives probe subassembly module 30 and accomodates or expose in accomodating the hole, the realization has stably controlled the rectangle graphite probe 3 in the probe subassembly module 30 and has popped out and withdraw, and the loss that has reduced rectangle graphite probe 3 to the at utmost, improve the life of probe.
In this embodiment, the driving support module 40 includes a driving connecting rod 4, a driven connecting rod 5 and a probe assembly shaft 19, two ends of the driving connecting rod 4 and the driven connecting rod 5 are respectively provided with a cylindrical hole, the probe assembly module 30 and the support base 1 near two ends of the accommodating hole are both provided with the probe assembly shaft 19, the probe assembly shaft 19 passes through the cylindrical holes at two ends of the driving connecting rod 4 and the driven connecting rod 5, that is, the driving connecting rod 4, the driven connecting rod 5, the probe assembly module 30 and the support base 1 form a parallelogram framework, so that the driving connecting rod 4 and the driven connecting rod 5 synchronously rotate, and the probe assembly module 30 is stably ejected or retracted; in some disclosures, as shown in the figures, the probe assembly shaft 19 is provided with threaded holes at both ends, and is fixed at both ends of the probe assembly module 30 and the support base 1 by screws 12.
In this embodiment, the probe assembly module 30 includes a plurality of probe assembly units which are attached to each other and arranged in a straight line, each probe assembly unit includes a rectangular graphite probe 3, a ceramic partition plate 15, a wiring screw 14 and a wire 6, a first groove is formed on one surface of the ceramic partition plate 15, the rectangular graphite probe 3 is embedded in the first groove, the top end of the rectangular graphite probe 3 protrudes out of the first groove, a threaded hole is formed in the bottom of the rectangular graphite probe 3 and is in threaded connection with the wiring screw 14, and the wiring screw 14 is in clamping connection with the wire 6.
The tail ends of the probe assembly units which are mutually attached and linearly arranged are attached with the ceramic baffle plate 16, and the side surfaces of the probe assembly units and the ceramic baffle plate 16 are wrapped by the first fixing frame 2, the second fixing frame 9, the first top plate 17 and the second top plate 18;
the probe assembly shaft 19 is installed between the first fixing frame 2 and the second fixing frame 9 of the probe assembly module 30, and both ends of the probe assembly shaft 19 are fixedly connected with the first fixing frame 2 and the second fixing frame 9, including but not limited to a fixing manner by using screws 12 as shown in the figure.
In some embodiments, the first fixing frame 2, the second fixing frame 9, the first top plate 17 and the second top plate 18 are fixedly connected through four screws 12, so that the first fixing frame 2, the second fixing frame 9, the first top plate 17 and the second top plate 18 are mutually stabilized, and the first fixing frame 2, the second fixing frame 9, the first top plate 17 and the second top plate 18 are mutually detachable; of course, in other embodiments, the first fixing frame 2, the second fixing frame 9, the first top plate 17 and the second top plate 18 may be integrally formed.
A rectangular second groove is formed between the first fixing frame 2 and the second fixing frame 9, and the ceramic partition plates 15 of all the probe assembly units can be just clamped in the second groove; the probe assembly module 30 is compact and easy to assemble.
In this embodiment, the ceramic partition 15 and the ceramic baffle 16 are made of insulating ceramic materials, such as high-temperature sintered alumina ceramic, so that all the rectangular graphite probes 3 are wrapped by the ceramic partition 15 and the ceramic baffle 16, thereby achieving a good insulating effect and ensuring the measurement accuracy of the rectangular graphite probes 3.
The coil box assembly module 8 comprises a coil 803, the coil 803 is wound on a bobbin 802, and a cylindrical through hole is arranged in the middle of the bobbin 802; the front surface of the coil box 801 is provided with a square groove, the middle of the coil box 801 is provided with a cylinder, the cylinder just passes through a cylinder hole in the middle of the bobbin 802 to fix the coil box, and the side surface of the coil box 801 is provided with a rectangular groove for the coil 803 to penetrate out to be connected with a power supply; the coil box cover 804 is matched with the coil box 801 and fixed by screws 12; one end of the coil box 801 is provided with a cylindrical through hole; two ends of the coil box shaft 21 are provided with threaded holes and are screwed and fixed on the support base 1 by screws 12; the coil box shaft 21 just passes through the cylindrical through hole at one end of the coil box 801 to realize the rotation of the coil box assembly module 8.
The coil box shaft 21 of the coil box component module 8 is perpendicular to the rotating shaft of the driving connecting rod 4 in the driving support module 40, which is determined by the magnetic field direction of a divertor area and the polar direction distribution direction of a pop-up divertor probe, so the coil box component module 8 is connected with the driving connecting rod 4 in the driving support module 40 through a universal connecting shaft component 7, the universal connecting shaft component 7 is composed of two universal couplings and a connecting rod, the connecting rod is fixedly connected between one joint of the two universal couplings, the other joints of the two universal couplings are respectively welded and fixed on the driving connecting rod 4 and the coil box component module 8, the universal connecting shaft component 7 is adopted for connection, accurate motion transmission can be realized, and the position accuracy of the pop-up and the recovery of the probe is improved.
In some embodiments, the probe assembly shaft 19 and the coil box shaft 21 are made of composite carbon fiber material, and can perform a lubricating function to reduce friction resistance while satisfying the requirement of rotational connection.
In some embodiments, the supporting base 1, the first fixing frame 2, the second fixing frame 9, the first top plate 17, the second top plate 18, the driving connecting rod 4, the driven connecting rod 5, the coil box 801 and the coil box cover 804 may be formed by processing 316L stainless steel and a chromium zirconium copper material, and may also be formed by processing a composite carbon fiber material with better service performance; the bobbin 802 is fabricated from an insulating ceramic material, such as boron nitride, alumina ceramic, or the like.
In the present embodiment, although the screws 12 in different parts are marked with the same mark "12", the limitation between the screws 12 cannot be regarded as such, such as the limitation only to a single type of screw 12, and in some scenarios, the screws 12 in different parts in the present disclosure may be replaced according to actual needs, so that the types of the screws 12 in one or more different parts are different from each other.
In some disclosures, the pop-up divertor probe system disclosed in this embodiment is an integrated structure, independent of the divertor target plate 10, that can be integrally mounted and dismounted; a rectangular hole with the width of 2cm is formed in the divertor target plate 10, and the pop-up divertor probe system penetrates through the rectangular hole and is fixedly arranged on the divertor target plate 10 or a rear-end supporting structure; the integrated structure can make the pop-up divertor probe system easy to install and dismantle, and the maintenance is more convenient.
In the description herein, references to the description of "one embodiment," "an example," "a specific example," etc., mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the disclosure. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.
The foregoing illustrates and describes the general principles, principal features, and advantages of the present disclosure. It will be understood by those skilled in the art that the present disclosure is not limited to the embodiments described above, which are presented solely for purposes of illustrating the principles of the disclosure, and that various changes and modifications may be made to the disclosure without departing from the spirit and scope of the disclosure, which is intended to be covered by the claims.
Claims (9)
1. A pop-up divertor probe system for a magnetically confined nuclear fusion device, comprising a support base (1), characterized in that a probe assembly module (30) loaded with rectangular graphite probes (3) is arranged on the support base (1);
the supporting base (1) is provided with a driving supporting module (40), and the driving supporting module (40) is used for driving the probe assembly module (30) to move, so that the probe assembly module (30) can be ejected or recovered;
the coil box assembly module (8) loaded with the coil (803) is installed at the lower end of the supporting base (1), the coil box assembly module (8) is rotatably installed on the supporting base (1), and the coil box assembly module (8) is connected with the driving supporting module (40) through a universal connecting shaft assembly (7).
2. The pop-up divertor probe system for a magnetically confined nuclear fusion device according to claim 1, wherein the driving support module (40) comprises a driving connecting rod (4), a driven connecting rod (5) and a probe assembly shaft (19), wherein cylindrical holes are respectively formed at both ends of the driving connecting rod (4) and the driven connecting rod (5), the probe assembly shaft (19) is installed at both the probe assembly module (30) and the support base (1) which are close to both ends of the receiving hole, and the probe assembly shaft (19) passes through the cylindrical holes at both ends of the driving connecting rod (4) and the driven connecting rod (5).
3. The pop-up divertor probe system for a magnetically confined nuclear fusion device of claim 2, wherein said probe assembly module (30) comprises a plurality of probe assembly units in line with each other.
4. The pop-up divertor probe system for a magnetically confined nuclear fusion device according to claim 3, wherein the probe unit comprises a rectangular graphite probe (3), a ceramic partition (15), a wiring screw (14), and a wire (6), wherein a first groove is formed on one surface of the ceramic partition (15), the rectangular graphite probe (3) is embedded in the first groove, the top end of the rectangular graphite probe (3) protrudes out of the first groove, a threaded hole is formed in the bottom of the rectangular graphite probe (3) and is in threaded connection with the wiring screw (14), and the wiring screw (14) is in clamping connection with the wire (6).
5. The pop-up divertor probe system for a magnetically confined nuclear fusion device of claim 4, wherein the ends of a plurality of said probe assembly units attached to each other in a linear arrangement are attached with a ceramic baffle (16), and the side faces of the probe assembly units and the ceramic baffle (16) as a whole are wrapped by a first fixing frame (2), a second fixing frame (9), a first top plate (17) and a second top plate (18);
the probe assembly shaft (19) is arranged between the first fixing frame (2) and the second fixing frame (9) of the probe assembly module (30), and two ends of the probe assembly shaft (19) are fixedly connected with the first fixing frame (2) and the second fixing frame (9).
6. The pop-up divertor probe system for a magnetically confined nuclear fusion device of claim 5, wherein a second rectangular recess is opened between said first holder (2) and said second holder (9), and ceramic spacers (15) of all probe assembly units are captured in the second recess.
7. A pop-up divertor probe system for a magnetically confined nuclear fusion device according to claim 6, wherein said ceramic baffles (15, 16) and ceramic baffles are made of an insulating ceramic material.
8. A pop-up divertor probe system for a magnetically confined nuclear fusion device according to claim 7, wherein said coil box assembly module (8) comprises a coil (803), said coil (803) being wound on a bobbin (802), a cylindrical through hole being provided in the middle of the bobbin (802);
the front surface of the coil box (801) is provided with a square groove, the middle of the coil box is provided with a cylinder, the cylinder just penetrates through a cylinder hole in the middle of the bobbin (802) to fix the bobbin, and the side surface of the coil box (801) is provided with a rectangular groove for the coil (803) to penetrate out to be connected with a power supply;
the coil box cover (804) is matched with the coil box (801);
one end of the coil box (801) is provided with a cylindrical through hole;
the coil box shaft (21) just penetrates through the cylindrical through hole at one end of the coil box (801).
9. The pop-up divertor probe system for a magnetically confined nuclear fusion device of claim 8, wherein the coil box axis (21) of the coil box assembly module (8) is perpendicular to the axis of rotation of the drive connection rod (4) in the drive support module (40).
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110213748.XA CN113035380B (en) | 2021-02-25 | 2021-02-25 | Pop-up divertor probe system for magnetically confined nuclear fusion device |
| LU500014A LU500014B1 (en) | 2021-02-25 | 2021-04-08 | Pop-up divertor probe system for magnetic confinement nuclear fusion device |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202110213748.XA CN113035380B (en) | 2021-02-25 | 2021-02-25 | Pop-up divertor probe system for magnetically confined nuclear fusion device |
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| CN113035380A true CN113035380A (en) | 2021-06-25 |
| CN113035380B CN113035380B (en) | 2024-01-26 |
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Citations (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4149931A (en) * | 1973-07-16 | 1979-04-17 | The United States Of America As Represented By The United States Department Of Energy | Divertor for use in fusion reactors |
| EP0180013A1 (en) * | 1984-09-21 | 1986-05-07 | International Business Machines Corporation | Test probe system |
| US4624400A (en) * | 1983-10-21 | 1986-11-25 | Westinghouse Electric Corp. | Electromagnetic probe drive apparatus |
| US4667148A (en) * | 1985-06-26 | 1987-05-19 | General Electric Company | Generator air-gap flux probe for detecting shorted rotor turns |
| US20020153877A1 (en) * | 2000-05-03 | 2002-10-24 | Harris Daniel L. | Indexing rotatable chuck for a probe station |
| CN1538929A (en) * | 2001-06-07 | 2004-10-20 | ���Ͽع�����˾ | Reciprocating device for winding yarn in form of reel |
| CN101263397A (en) * | 2005-08-05 | 2008-09-10 | 凡利安股份有限公司 | Axially constrained NMR RF probe coil |
| CN102109547A (en) * | 2009-12-24 | 2011-06-29 | 核工业西南物理研究院 | Scanning probe system on high field side of Tokamak device |
| CN102163481A (en) * | 2011-02-16 | 2011-08-24 | 中国科学院等离子体物理研究所 | Supporting leg structure of superconducting Tokamak longitudinal field coil |
| CN104332184A (en) * | 2014-08-30 | 2015-02-04 | 中国科学院等离子体物理研究所 | Target-plate probe system applicable to full-tungsten divertor of EAST tokamak device |
| CN205210293U (en) * | 2015-11-27 | 2016-05-04 | 沈阳工业大学 | Novel electric equipment surperficial magnetic characteristic test probe unshakable in one's determination |
| CN105607019A (en) * | 2014-09-15 | 2016-05-25 | 艾斯拜克特Ai有限公司 | NMR extractable probe cassette means and methods thereof |
| CN107301882A (en) * | 2017-06-12 | 2017-10-27 | 孙旭阳 | A kind of dumbbell structure controllable nuclear fusion apparatus |
| US20170336360A1 (en) * | 2016-03-14 | 2017-11-23 | Board Of Trustees Of Michigan State University | Rotating Current Excitation with Array Magnetic Sensors Nondestructive Testing Probe For Tube Inspection |
| CN206945761U (en) * | 2017-05-11 | 2018-01-30 | 中芯国际集成电路制造（天津）有限公司 | Probe card and test system |
| CN108040415A (en) * | 2017-12-21 | 2018-05-15 | 中国科学院合肥物质科学研究院 | Suitable for the integrated modular probe system of tungsten copper target plate |
| CN109061531A (en) * | 2018-08-24 | 2018-12-21 | 河北工业大学 | Consider the big print rotary magnetic characteristic test system and method for vortes interference |
| CN109425840A (en) * | 2017-08-30 | 2019-03-05 | 河北工业大学 | A kind of nanocrystalline rotary magnetic characteristic test system and measurement method |
| CN111403056A (en) * | 2020-03-31 | 2020-07-10 | 中国科学院合肥物质科学研究院 | Fast electronic measurement probe system suitable for magnetic confinement plasma |
-
2021
- 2021-02-25 CN CN202110213748.XA patent/CN113035380B/en active Active
- 2021-04-08 LU LU500014A patent/LU500014B1/en active IP Right Grant
Patent Citations (19)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4149931A (en) * | 1973-07-16 | 1979-04-17 | The United States Of America As Represented By The United States Department Of Energy | Divertor for use in fusion reactors |
| US4624400A (en) * | 1983-10-21 | 1986-11-25 | Westinghouse Electric Corp. | Electromagnetic probe drive apparatus |
| EP0180013A1 (en) * | 1984-09-21 | 1986-05-07 | International Business Machines Corporation | Test probe system |
| US4667148A (en) * | 1985-06-26 | 1987-05-19 | General Electric Company | Generator air-gap flux probe for detecting shorted rotor turns |
| US20020153877A1 (en) * | 2000-05-03 | 2002-10-24 | Harris Daniel L. | Indexing rotatable chuck for a probe station |
| CN1538929A (en) * | 2001-06-07 | 2004-10-20 | ���Ͽع�����˾ | Reciprocating device for winding yarn in form of reel |
| CN101263397A (en) * | 2005-08-05 | 2008-09-10 | 凡利安股份有限公司 | Axially constrained NMR RF probe coil |
| CN102109547A (en) * | 2009-12-24 | 2011-06-29 | 核工业西南物理研究院 | Scanning probe system on high field side of Tokamak device |
| CN102163481A (en) * | 2011-02-16 | 2011-08-24 | 中国科学院等离子体物理研究所 | Supporting leg structure of superconducting Tokamak longitudinal field coil |
| CN104332184A (en) * | 2014-08-30 | 2015-02-04 | 中国科学院等离子体物理研究所 | Target-plate probe system applicable to full-tungsten divertor of EAST tokamak device |
| CN105607019A (en) * | 2014-09-15 | 2016-05-25 | 艾斯拜克特Ai有限公司 | NMR extractable probe cassette means and methods thereof |
| CN205210293U (en) * | 2015-11-27 | 2016-05-04 | 沈阳工业大学 | Novel electric equipment surperficial magnetic characteristic test probe unshakable in one's determination |
| US20170336360A1 (en) * | 2016-03-14 | 2017-11-23 | Board Of Trustees Of Michigan State University | Rotating Current Excitation with Array Magnetic Sensors Nondestructive Testing Probe For Tube Inspection |
| CN206945761U (en) * | 2017-05-11 | 2018-01-30 | 中芯国际集成电路制造（天津）有限公司 | Probe card and test system |
| CN107301882A (en) * | 2017-06-12 | 2017-10-27 | 孙旭阳 | A kind of dumbbell structure controllable nuclear fusion apparatus |
| CN109425840A (en) * | 2017-08-30 | 2019-03-05 | 河北工业大学 | A kind of nanocrystalline rotary magnetic characteristic test system and measurement method |
| CN108040415A (en) * | 2017-12-21 | 2018-05-15 | 中国科学院合肥物质科学研究院 | Suitable for the integrated modular probe system of tungsten copper target plate |
| CN109061531A (en) * | 2018-08-24 | 2018-12-21 | 河北工业大学 | Consider the big print rotary magnetic characteristic test system and method for vortes interference |
| CN111403056A (en) * | 2020-03-31 | 2020-07-10 | 中国科学院合肥物质科学研究院 | Fast electronic measurement probe system suitable for magnetic confinement plasma |
Non-Patent Citations (4)
| Title |
|---|
| J.C.XU: "Upgrade Design of Lower Divertor Langmuir Probe Diagnostic System in the EAST Tokamak", 《IEEE》, pages 1 - 7 * |
| JILEI HOU: "Deuterium pellet fueling in type-III ELMy H-mode plasmas on EAST superconducting tokamak", 《ELSEVIER》, pages 79 - 86 * |
| 谭胜均 等: "EAST 上由垂直不稳定性引发破裂的分析与预测", 《核聚变与等离子体物理》, vol. 39, no. 2, pages 104 - 111 * |
| 钟武律: "托卡马克高约束模边缘等离子体不稳定性研究", 《原子核物理评论》, vol. 37, no. 3, pages 462 - 469 * |
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| LU500014B1 (en) | 2022-08-25 |
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