CN101149991A - Simulated subassembly for fuel subassembly flow measurement - Google Patents
Simulated subassembly for fuel subassembly flow measurement Download PDFInfo
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- CN101149991A CN101149991A CNA2007101632136A CN200710163213A CN101149991A CN 101149991 A CN101149991 A CN 101149991A CN A2007101632136 A CNA2007101632136 A CN A2007101632136A CN 200710163213 A CN200710163213 A CN 200710163213A CN 101149991 A CN101149991 A CN 101149991A
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- fuel
- assembly
- flow measurement
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- 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
- Y02E30/30—Nuclear fission reactors
Abstract
The invention relates to a simulation test device for metering flow of a fuel assembly. The contour of the simulation test device is identical to that of the fuel assemble, the inner side of which is provided with a closed flow-path in which is provided with a positioning comb and a simulation fuel plate. The positioning com is a com-shape positioning plate with several side-by-side grooves and the simulation fuel plate is fitted in the grooves of the positioning com. The length of the simulation fuel plate is less than that of the practical fuel plate. At rear end of the simulation fuel plate and in the space of the closed flow path is provided in turn with a vortex flow meter and a resistance regulation plate which is a plate with through holes. The device avoids the error resulted by adopting pressure-guiding pipe to do metering. Advantage: raised precision and reduced cost.
Description
Technical field
The invention belongs to simulation test device, be specifically related to a kind of simulated assembly that is used for the fuel assembly flow measurement.
Background technology
When reactor core assignment of traffic simulation test, the accuracy of flow measurement is very important, is related to the safety of reactor.In order fully to understand the flow characteristics of water in nuclear reactor, the basic test data are provided for the design of reactor thermal-hydraulic and in-pile component, need carry out the whole hydraulic simulation test of nuclear reactor.When hydraulic simulation, must adopt the simulated fuel assembly of simplification to replace the prototype fuel assembly to carry out the research that assignment of traffic is tested, so that reach economic, practical purpose.
At home in the plate shape fuel assembly reactor core assignment of traffic experimental study of adopting first, the profile of simulated assembly and internal structure are similar substantially with fuel assembly, to satisfy Testing requirement, but because the inner space of plate shape fuel assembly is little, so the simulated assembly inner space is also little, the routine measurement instrument is difficult in its positioned inside, can only adopt this moment in the sheet separation and carry out flow measurement with the mode of many group pressure guiding pipes, its corresponding differential pressure measurement instrument can only be located at the outside of reactor core, but the differential pressure measurement of pressure guiding pipe and channel size with and the roughness on surface etc. relevant, when pressure reduction is converted into flow, be subjected to channel size with and the influence of these aspects of roughness on surface, cause the flow measurement precision lower, in addition, the flow measurement of an assembly needs the stack conversion of many group differential pressure measurements to obtain, this brings the error of stack can for the flow measurement of assembly, cause the precision of assembly flow measurement lower, and adopt many group measurement instruments to measure a flow parameter, increased experimentation cost.
Summary of the invention
The object of the present invention is to provide the high simulated assembly that is used for the fuel assembly flow measurement of a kind of measuring accuracy.
The present invention is achieved in that a kind of simulated assembly that is used for the fuel assembly flow measurement, its profile is consistent with fuel assembly, its inboard is made as the enclosed runner, in the enclosed runner, be provided with location comb and analog fuel plate, the location comb is for having the pectination location-plate of some grooves side by side, the analog fuel plate is located in the groove of location comb, the length of analog fuel plate is less than the length of natural fuel plate, also be provided with turbo flow meter and resistance adjustable plate successively in the rear end of analog fuel plate, enclosed flow channel space, the resistance adjustable plate is the plate that has through hole.
The length of analog fuel plate of the present invention is less than the length of natural fuel plate, therefore the inner space of simulated assembly increases, turbo flow meter can be put into simulated assembly and measure, the flow measurement distortion that brings is then regulated correction by the resistance adjustable plate because simulated assembly shortens.The present invention has avoided the error that adopts pressure guiding pipe to measure, and has therefore improved the precision of flow measurement.In addition, owing to do not need many group measurement instruments to measure, reduced experimentation cost.
Description of drawings
Fig. 1 is a kind of fuel assembly flow measurement simulated assembly front view provided by the present invention;
Fig. 2 is a kind of fuel assembly flow measurement simulated assembly vertical view provided by the present invention;
Fig. 3 is that the A-A of Fig. 1 is to view;
Among the figure: 1 bale handle, 2 location combs, 3 master plates, 4 times plugs, 5 analog fuel plates, 6 side plates, 7 resistance adjustable plates, 8 turbo flow meters, 9 pins, 10 recess channels.
Embodiment
As Fig. 1～shown in Figure 3, a kind of fuel assembly flow measurement simulated assembly, it comprises master plate 3, inferior lavatory plate 6, plug 4, location comb 2, analog fuel plate 5, pin 9, bale handle 1, turbo flow meter 8 and resistance adjustable plate 7 down.Location comb 2 is respectively equipped with time side plate 6 for having the pectination location-plate of some grooves side by side in the outermost groove near comb 2 two ends, location, be equipped with analog fuel plate 5 in the middle groove.Location comb 2, inferior side plate 6 and analog fuel plate 5 are connected and fixed by pin 9, sell 9 two ends and rivet or spot welding.Be provided with two blocks of master plates 3 on the vertical direction of inferior side plate 6, following plug 4 inserts from the rear end part of two master plates 3, and is connected by screw with two master plates 3, has a determining deviation between following plug 4 and the inferior side plate 6.
The profile of master plate 3 and time side plate 6 keeps consistent with prototype component, by being welded to form an enclosed runner.Master plate 3 is a platy structure, to the inboard bending of enclosed runner, and has projection cube structure in the outside of enclosed runner at front end.
The length of analog fuel plate 5 is less than the length of natural fuel plate, therefore can be in the enclosed runner that master plate 3 and time side plate 6 are formed, the rear end of analog fuel plate 5 is provided with turbo flow meter 8 and resistance adjustable plate 7 successively.The inner turbo flow meter 8 of installing of enclosed runner becomes one itself and assembly, and dependable flow all passes from turbo flow meter 8 is installed.The shell of turbo flow meter 8 adopts screw to be connected with twice side plate 6 with two master plates 3, and resistance adjustable plate 7 is for having the square plate of through hole, and the shape in hole can be circular, square or other shapes, is the slab of square-outside and round-inside in the present embodiment.Resistance adjustable plate 7 needs to determine by test of many times whether its perforate size is suitable.When regulating the perforate size of resistance adjustable plate, should guarantee that the both sides pressure reduction sum of analog fuel plate two ends pressure reduction, turbo flow meter two ends pressure reduction and resistance adjustable plate equals the pressure reduction of natural fuel plate.Resistance adjustable plate 7 also adopts screw to be connected with time side plate 6 with two master plates 3.Following plug 4 is the structures that the cross section is the trapezoidal transition rectangular channel, the passage that its inboard has fluid to flow through, and four sides, outside middle position is provided with fluid by recess channels 10.Following plug 4 main effects are that assembly is installed in the following Turbogrid plates of reactor core, and the effect of play the location, supporting guarantees assembly location and installation in reactor core.Bale handle 1 is the ad hoc lifting part when being used for the reactor installation component, is a cylindrical beam structure.Bale handle 1 need rivet or spot welding is connected the end of two master plates 3.
The present invention also goes for the enclosed assembly of other profile, such as circle, hexagon, octagon etc.As long as its profile is consistent with fuel assembly, its inboard is made as the enclosed runner, can be provided with turbo flow meter and resistance adjustable plate in the enclosed flow channel space, to improve the precision of fuel assembly flow measurement.
Claims (6)
1. simulated assembly that is used for the fuel assembly flow measurement, its profile is consistent with fuel assembly, its inboard is made as the enclosed runner, in the enclosed runner, be provided with location comb (2) and analog fuel plate (5), location comb (2) is for having the pectination location-plate of some grooves side by side, analog fuel plate (5) is located in the groove of location comb (2), it is characterized in that: the length of analog fuel plate (5) is less than the length of natural fuel plate, rear end in analog fuel plate (5), also be provided with turbo flow meter (8) and resistance adjustable plate (7) in the enclosed flow channel space successively, resistance adjustable plate (7) is for having the plate of through hole.
2. a kind of simulated assembly that is used for the fuel assembly flow measurement as claimed in claim 1, it is characterized in that: in outermost groove, be respectively equipped with time side plate (6) near comb (2) two ends, described location, be equipped with analog fuel plate (5) in the middle groove, be provided with two blocks of master plates (3) at the two ends of inferior side plate (6), master plate (3) and time side plate (6) are formed the enclosed runner.
3. a kind of simulated assembly that is used for the fuel assembly flow measurement as claimed in claim 2 is characterized in that: the rear end part of described two master plates (3) is connected with following plug (4).
4. a kind of fuel assembly flow measurement simulated assembly as claimed in claim 2 is characterized in that: location comb (2), inferior side plate (6) and analog fuel plate (5) are connected and fixed by pin (9).
5. a kind of simulated assembly that is used for the fuel assembly flow measurement as claimed in claim 2 is characterized in that: the shell of described turbo flow meter (8) adopts screw to be connected with twice side plate (6) and two master plates (3).
6. a kind of simulated assembly that is used for the fuel assembly flow measurement as claimed in claim 2 is characterized in that: the circumferential and master plate (3) of described resistance adjustable plate (7) is connected with time side plate (6).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2007101632136A CN101149991B (en) | 2007-10-19 | 2007-10-19 | Simulated subassembly for fuel subassembly flow measurement |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2007101632136A CN101149991B (en) | 2007-10-19 | 2007-10-19 | Simulated subassembly for fuel subassembly flow measurement |
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| Publication Number | Publication Date |
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| CN101149991A true CN101149991A (en) | 2008-03-26 |
| CN101149991B CN101149991B (en) | 2010-08-11 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN2007101632136A Active CN101149991B (en) | 2007-10-19 | 2007-10-19 | Simulated subassembly for fuel subassembly flow measurement |
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Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104078087A (en) * | 2014-06-24 | 2014-10-01 | 西安交通大学 | Rod bundle test piece for simulating supercritical water-cooled reactor fuel element |
| CN105719707A (en) * | 2014-12-01 | 2016-06-29 | 上海核工程研究设计院 | Differential pressure measuring point layout structure in pressurized water reactor integral hydraulic simulation test |
| CN106803431A (en) * | 2017-01-22 | 2017-06-06 | 中国核动力研究设计院 | The external that can accurately measure core flow declines chamber arrangement apparatus and measuring method |
| CN109841290A (en) * | 2019-03-11 | 2019-06-04 | 中国核动力研究设计院 | A kind of device and method suitable for the research of nuclear reactor natural circulation characteristic |
| CN110415843A (en) * | 2019-08-08 | 2019-11-05 | 中国核动力研究设计院 | The reactor enclosed fuel assembly hydraulics simulating device of resistance adjustment mechanism and its composition |
| CN111982213A (en) * | 2020-08-20 | 2020-11-24 | 中国核动力研究设计院 | Flow measurement method and system for nuclear reactor simulation fuel assembly |
| CN113393948A (en) * | 2021-06-15 | 2021-09-14 | 哈尔滨工程大学 | Visual experimental apparatus of large-space jet flow at outlet of plate-shaped fuel element |
-
2007
- 2007-10-19 CN CN2007101632136A patent/CN101149991B/en active Active
Cited By (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104078087A (en) * | 2014-06-24 | 2014-10-01 | 西安交通大学 | Rod bundle test piece for simulating supercritical water-cooled reactor fuel element |
| CN104078087B (en) * | 2014-06-24 | 2016-05-25 | 西安交通大学 | A kind of cluster testpieces of simulating Supercritical-Pressure Light Water Cooled Reactor fuel element |
| CN105719707A (en) * | 2014-12-01 | 2016-06-29 | 上海核工程研究设计院 | Differential pressure measuring point layout structure in pressurized water reactor integral hydraulic simulation test |
| CN106803431A (en) * | 2017-01-22 | 2017-06-06 | 中国核动力研究设计院 | The external that can accurately measure core flow declines chamber arrangement apparatus and measuring method |
| CN109841290A (en) * | 2019-03-11 | 2019-06-04 | 中国核动力研究设计院 | A kind of device and method suitable for the research of nuclear reactor natural circulation characteristic |
| CN110415843A (en) * | 2019-08-08 | 2019-11-05 | 中国核动力研究设计院 | The reactor enclosed fuel assembly hydraulics simulating device of resistance adjustment mechanism and its composition |
| CN110415843B (en) * | 2019-08-08 | 2021-01-26 | 中国核动力研究设计院 | Resistance adjusting mechanism and reactor closed fuel assembly hydraulics simulator who constitutes thereof |
| CN111982213A (en) * | 2020-08-20 | 2020-11-24 | 中国核动力研究设计院 | Flow measurement method and system for nuclear reactor simulation fuel assembly |
| CN111982213B (en) * | 2020-08-20 | 2022-02-11 | 中国核动力研究设计院 | Flow measurement method and system for nuclear reactor simulation fuel assembly |
| CN113393948A (en) * | 2021-06-15 | 2021-09-14 | 哈尔滨工程大学 | Visual experimental apparatus of large-space jet flow at outlet of plate-shaped fuel element |
| CN113393948B (en) * | 2021-06-15 | 2022-12-13 | 哈尔滨工程大学 | Visual experimental apparatus of big space efflux of tabular fuel element export |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101149991B (en) | 2010-08-11 |
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