CN102435769A - Method and device for spreading trace particles in supersonic PIV (Particle Image Velocimetry) flow field testing experiment - Google Patents
Method and device for spreading trace particles in supersonic PIV (Particle Image Velocimetry) flow field testing experiment Download PDFInfo
- Publication number
- CN102435769A CN102435769A CN2011103720528A CN201110372052A CN102435769A CN 102435769 A CN102435769 A CN 102435769A CN 2011103720528 A CN2011103720528 A CN 2011103720528A CN 201110372052 A CN201110372052 A CN 201110372052A CN 102435769 A CN102435769 A CN 102435769A
- Authority
- CN
- China
- Prior art keywords
- particle
- flow
- piv
- trace
- generator
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Pending
Links
Images
Landscapes
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
The invention relates to a method and a device for spreading trace particles in a supersonic PIV (Particle Image Velocimetry) flow field testing experiment. The trace particles are charged by using vacuum suction in a supersonic wind tunnel high-pressure high-temperature large-flow flow field environment, the trace particles are stored in a particle generator before the experiment, after a gas flow is injected, the gas flow and the trace particles are sufficiently mixed, pass through a high-pressure pipeline, are spread by a particle spreader and then enter a wind tunnel pipeline, the trace particles are uniformly spread under the condition of a high-Mach-number flow, and the trace particles are tested through a particle image velocity-measuring system. Compared with the prior art, the method and the device provided by the invention realize that the PIV trace particles are charged and uniformly spread in a high-pressure high-temperature large-flow flow field ambient condition, the probable agglomeration phenomenon of the trace particles in the injection process is effectively avoided, precise sequence control between a PIV system and wind tunnel operation is guaranteed, and the testing scheme corresponding to the spreading concentration satisfying the PIV operation requirement is determined.
Description
Technical field
The present invention relates to the wind tunnel technique of aerospace field, especially relate to the method and the device that dispense trace particle in the experiment of supersonic speed PIV flow-field test.
Background technology
Along with space technology and hypersonic weaponry technology rapid development; Ultra/hypersonic compressible mobile research and relevant experiment test technology are paid attention to greatly and are developed, particularly the measuring technology of the quantification velocity field of high-accuracy high-resolution distribution.
Particle image velocimetry technology (PIV) application facet that tests the speed in the flow field has had significant progress in recent years; It breaks through traditional spot measurement restriction; Velocity distribution in can instantaneous noncontacting measurement flow field on cross section; And higher measuring accuracy is arranged, flow such as supersonic jet, shear layer, stream and adhere in the hypersonic flow field measurements such as shock wave and cylinder detached shock wave such as corner flow, wedge and to have obtained good measurement result in the ultra-combustion ramjet.
Ultra/as hypersonicly to flow that to be different from the low speed distinguishing feature that flows be shock wave phenomena.Shock wave can cause forming the zone that a flow velocity is a significant slowdown at model surface; Boundary layer and shear layer are relatively very thin, and the compressible mobile velocity field of PIV technical testing high speed has been brought challenge: guarantee in the measurement face that trace particle concentration evenly and satisfy the PIV test request.Therefore the selected particle homogeneity scheme of dispensing preferably is that PIV using ultrasound speed flows the key issue of research as one of supersonic speed PIV measuring technology development key technology, how to realize that trace particle evenly dispenses and concentration satisfies the concern that the PIV trace particle technology of dispensing that the PIV Flame Image Process requires obtains numerous researchers under study for action.
Summary of the invention
The object of the invention is exactly for the defective that overcomes above-mentioned prior art existence method and the device that dispenses trace particle in a kind of supersonic speed PIV experiment to be provided; But make supersonic speed PIV trace particle dispense system's manual control or Long-distance Control and real-time response; Dispense and to avoid and to reduce trace particle in the process and gather a phenomenon; And can obtain the good image of distribution of particles effect, computing can obtain comparatively desirable flow field vector distribution plan through PIV.
The object of the invention can be realized through following technical scheme:
Dispense the method for trace particle in the supersonic speed PIV experiment; Under the environment of the big flow of supersonic wind tunnel HTHP flow field, utilize vacuum to suck and realize the trace particle filling; It is characterized in that; This method may further comprise the steps: trace particle is stored in the particle generator before the experiment; Air-flow and trace particle fully mix through pressure duct and dispense device through particle and dispense the laggard wind-tunnel pipeline of going into after open injecting air-flow, and trace particle dispenses evenly under the high Mach number inlet flow conditions, and system tests trace particle through particle image velocimetry.
Injection air-flow in the described particle generator adopts annular high pressure finedraw spray mode, make the air-flow spray evenly and the trace particle powder that is easy to carry about with one go out generator.
Regulate the array mode that particle generator injects the air flow meter flow value and changes the shut-off valve assemblies on the particle generator, the trace particle that obtains suitable PIV Flame Image Process under different air flow rates and the pressure condition dispenses concentration and flow.
Air pressure is to closing on vacuum state between the preceding need of unlatching wind-tunnel balance test section, stable section and vacuum sphere.Open valve made particle generator also reach and closed on vacuum state this moment.The trace particle powder that when opening duct valve and closing the pressure duct valve, is contained in the particle jar can be inhaled in the generator tank body fast, and the particle volt is waited for the experiment beginning in the particle generator tank base behind the closure catheter for closing valve.Propose and realization vacuum suction particle dosing method, can significantly reduce trace particle and contact the phenomenon that group is gathered in the back with humid air, and can reduce the number of times of dismounting particle generator port, obviously improved the trace particle injection efficiency.
Dispense the device of trace particle in the supersonic speed PIV experiment, comprising:
Particle generator: store trace particle, be connected with the particle jar through airtight pipeline;
Particle dispenses device: be arranged between the wind-tunnel stable section upper reaches and the well heater downstream, be connected with particle generator through airtight pipeline.
Described particle generator injects airflow pipeline by lower port and high pressure and is connected, and stop valve and two flowmeters are installed on the pipeline, and flowmeter group scalable high pressure draught flow is closed in the circulation of stop valve control high pressure gas.Trace particle stores in the particle jar before the experiment, utilizes the vacuum inhalation method to get into particle generator through conduit, stop valve and port then, and a jar internal pressure reads through tensimeter.Particle generator is fixed by stent support.During experiment stop valve is opened, high pressure draught carry well-mixed trace particle through pressure duct, dispense pipe and particle and dispense device and inject wind-tunnel, and with the even blending of wind-tunnel main flow and do not influence each flow parameter of wind-tunnel.
Utilize the vacuum tightness after particle generator and the wind-tunnel stable section balance that trace particle is sucked in the particle generator.High pressure injects air-flow and gets into particle generator by lower port; Pipeline is by mode spray in the form of a ring between fastening group of guiding in lower end guiding, guide housing; From bottom to top impact the trace particle powder be positioned at the bottom of the generator jar, and powder is injected wind-tunnel through the generator port uniformly.Lower port realizes high pressure sealing through port pressure cap and inner sealing device, can the high pressure of anti-20MPa.
Particle generator dispense the pipe in air current spray nozzle be supersonic nozzle, high pressure draught through nozzle, dispense a mouthful entering wind-tunnel pipeline.Dispensing mouthful diameter is 1mm.Dispense tube material and select SS321 for use, can the high pressure of anti-16MPa.
The pipe endpiece that dispenses that described particle dispenses in the device adopts supersonic nozzle, and opening direction is parallel to the wind-tunnel main flow and comes flow path direction.
This device can realize that the switching of manual control or Long-distance Control also can real-time response.
Compared with prior art, the present invention dispenses flow and concentration through the trace particle that strength and the valve member array mode of regulating trace particle and injecting air-flow obtained to adapt to different incoming flow Mach numbers and different flow; Propose to utilize the vacuum tightness after particle generation tank and the wind-tunnel stable section balance that trace particle is sucked into the particle method for implanting in the generator jar, effectively avoided trace particle contingent phenomenon of gathering in injection process; Through selected experiment test flow process sequential, guaranteed accurate sequential control between PIV system and the wind tunnel operation; Through compare test particle generator injection pressure particle is dispensed the influence of concentration, that has confirmed to satisfy PIV computing requirement dispenses the pairing testing scheme of concentration.
Description of drawings
Fig. 1 is the arrangement synoptic diagram of this device;
Fig. 2 is the structural representation of this device;
Fig. 3 is a particle generator lower port structural representation;
Fig. 4 dispenses the tubular construction synoptic diagram for particle generator.
Embodiment
Below in conjunction with accompanying drawing and specific embodiment the present invention is elaborated.
Embodiment
The on-the-spot arrangement of supersonic speed PIV is shown in Figure 1 as illustrating among the present invention; A is the Laboratory Module of supersonic wind tunnel among the figure; B is the PIV system; C is the wind-tunnel stable section, is respectively trace particle shown in D, F, the G and dispenses particle in the system and dispense device (comprising that particle dispenses pipeline), particle generator and generator and inject airflow pipeline, and E is a wind-tunnel main flow pipeline.Particle dispenses device D and is arranged between the wind-tunnel stable section upper reaches and the well heater downstream, and particle generator F is used for trace particle and high pressure and injects that air-flow G mixes and carry entering wind-tunnel main flow pipeline by its impact.
The device that dispenses trace particle among the present invention in the supersonic speed PIV experiment is as shown in Figure 2; Particle generator 5 injects airflow pipeline 1-1 by lower port 4 and high pressure and is connected; Stop valve 2-1 and two flowmeter 3-1, flowmeter 3-2 are installed on the pipeline; Flowmeter group scalable high pressure draught flow is closed in the circulation of stop valve control high pressure gas.Trace particle stores in particle jar 9 before the experiment, utilizes the vacuum inhalation method to get into particle generator 5 through conduit 1-2, stop valve 2-2 and port 6 then, and a jar internal pressure reads through tensimeter 8.Particle generator 5 is by support 7 support fixation.During experiment stop valve 2-3, stop valve 2-4 are opened; High pressure draught carry well-mixed trace particle through pressure duct 1-3, pressure duct 1-4, dispense pipe 10-1, dispense pipe 10-2 and dispense device 11 and inject wind-tunnel, and with the even blending of wind-tunnel main flow and do not influence each flow parameter of wind-tunnel.
Particle generator lower port structure among the present invention is as shown in Figure 3; High pressure injects air-flow and gets into particle generator by lower port 31; Pipeline is by fastening group of 35 the mode sprays in the form of a ring of leading in lower end guiding 33, guide housing 34; From bottom to top impact the trace particle powder be positioned at the bottom of the generator jar, and powder is injected wind-tunnel through the generator port uniformly.Lower port realizes high pressure sealing through port pressure cap 32 and inner sealing device, can the high pressure of anti-20MPa.
It is as shown in Figure 4 that particle generator among the present invention dispenses tubular construction, dispenses that air current spray nozzle 42 is supersonic nozzle in the pipe, high pressure draught through nozzle, dispense mouthfuls 41 and get into wind-tunnel pipelines.Dispensing mouthful diameter is 1mm.Dispense tube material and select SS321 for use, can the high pressure of anti-16MPa.
Air pressure is to closing on vacuum state between the preceding need of unlatching wind-tunnel balance test section, stable section and vacuum sphere.Open stop valve 2-3, stop valve 2-4 this moment, makes particle generator also reach and close on vacuum state.The trace particle powder that when opening catheter cutoff valve 2-2 and closing pressure duct stop valve 2-3, stop valve 2-4, is contained in the particle jar can be inhaled in the generator tank body fast; The particle volt is waited for the experiment beginning in the particle generator tank base behind the closure catheter for closing stop valve 2-2.Propose and realization vacuum suction particle dosing method, can significantly reduce trace particle and contact the phenomenon that group is gathered in the back with humid air, and can reduce the number of times of dismounting particle generator port, obviously improved the trace particle injection efficiency.
According to the wind tunnel operation parameter, table 1 has provided selected injection pressure and pairing trace particle flow and wind-tunnel main flow flow under Mach number 4.0 and 7.0 experiment conditions.Utilize PIV software to the image gathered to carrying out computing cross-correlation, the flow field vector is evenly distributed and can fully reflects the shock wave structure characteristic.When particle flow is 0.01kg/s and main flow flow when being 3.1kg/s, can estimate that according to particle density and incoming flow flow velocity the particle concentration that obtains in the experimental section is 100,000/mm
3, therefore can satisfy each interpretation sub-district has 10 particles to exist, and meets the requirement of PIV computing cross-correlation.
Table 1 trace particle injection pressure and flow parameter
Dispense the method for trace particle in the supersonic speed PIV experiment; Under the environment of the big flow of supersonic wind tunnel HTHP flow field, utilize vacuum to suck and realize the trace particle filling; Trace particle is stored in the particle generator before the experiment; Air-flow and trace particle fully mix through pressure duct and dispense device through particle and dispense the laggard wind-tunnel pipeline of going into after open injecting air-flow, and trace particle dispenses evenly under the high Mach number inlet flow conditions, and system tests trace particle through particle image velocimetry.
Injection air-flow in the particle generator adopts annular high pressure finedraw spray mode, make the air-flow spray evenly and the trace particle powder that is easy to carry about with one go out generator.Regulate the array mode that particle generator injects the air flow meter flow value and changes the shut-off valve assemblies on the particle generator, the trace particle that obtains suitable PIV Flame Image Process under different air flow rates and the pressure condition dispenses concentration and flow.
Air pressure is to closing on vacuum state between the preceding need of unlatching wind-tunnel balance test section, stable section and vacuum sphere.Open valve made particle generator also reach and closed on vacuum state this moment.The trace particle powder that when opening duct valve and closing the pressure duct valve, is contained in the particle jar can be inhaled in the generator tank body fast, and the particle volt is waited for the experiment beginning in the particle generator tank base behind the closure catheter for closing valve.Propose and realization vacuum suction particle dosing method, can significantly reduce trace particle and contact the phenomenon that group is gathered in the back with humid air, and can reduce the number of times of dismounting particle generator port, obviously improved the trace particle injection efficiency.
Claims (9)
1. dispense the method for trace particle in the experiment of supersonic speed PIV flow-field test; Under the environment of the big flow of supersonic wind tunnel HTHP flow field, utilize vacuum to suck and realize the trace particle filling; It is characterized in that; This method may further comprise the steps: trace particle is stored in the particle generator before the experiment; Air-flow and trace particle fully mix through pressure duct and dispense device through particle and dispense the laggard wind-tunnel pipeline of going into after open injecting air-flow, and trace particle dispenses evenly under the high Mach number inlet flow conditions, and system tests trace particle through particle image velocimetry.
2. dispense the method for trace particle in the supersonic speed PIV flow-field test experiment according to claim 1; It is characterized in that; Injection air-flow in the described particle generator adopts annular high pressure finedraw spray mode, make the air-flow spray evenly and the trace particle powder that is easy to carry about with one go out generator.
3. dispense the method for trace particle in the supersonic speed PIV flow-field test experiment according to claim 1; It is characterized in that; Regulate the array mode that particle generator injects the air flow meter flow value and changes the shut-off valve assemblies on the particle generator, the trace particle that obtains suitable PIV Flame Image Process under different air flow rates and the pressure condition dispenses concentration and flow.
4. dispense the method for trace particle in the supersonic speed PIV flow-field test experiment according to claim 1; It is characterized in that; Need before the test that air pressure utilizes the vacuum state in particle generator this moment from the particle jar, to suck in the particle generator trace particle subsequent use fast to closing on vacuum state between equilibrium particle generator, experimental section, stable section and vacuum sphere.
5. dispense the device of trace particle in the experiment of supersonic speed PIV flow-field test, it is characterized in that this device comprises:
Particle generator: store trace particle, be connected with the particle jar through airtight pipeline;
Particle dispenses device: be arranged between the wind-tunnel stable section upper reaches and the well heater downstream, be connected with particle generator through airtight pipeline.
6. dispense the device of trace particle in the supersonic speed PIV flow-field test experiment according to claim 5; It is characterized in that; Described particle generator is provided with stop valve, tensimeter and flowmeter, through regulating the flow that stop valve and flowmeter control trace particle injects air-flow.
7. dispense the device of trace particle in the supersonic speed PIV flow-field test according to claim 5 experiment, it is characterized in that, utilize the vacuum tightness after particle generator and the wind-tunnel stable section balance that trace particle is sucked in the particle generator.
8. dispense the device of trace particle in the supersonic speed PIV flow-field test experiment according to claim 5, it is characterized in that, the pipe endpiece that dispenses that described particle dispenses in the device adopts supersonic nozzle, and opening direction is parallel to the wind-tunnel main flow and comes flow path direction.
9. dispense the device of trace particle in the supersonic speed PIV flow-field test experiment according to claim 5, it is characterized in that, this device can realize that the switching of manual control or Long-distance Control also can real-time response.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011103720528A CN102435769A (en) | 2011-11-21 | 2011-11-21 | Method and device for spreading trace particles in supersonic PIV (Particle Image Velocimetry) flow field testing experiment |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2011103720528A CN102435769A (en) | 2011-11-21 | 2011-11-21 | Method and device for spreading trace particles in supersonic PIV (Particle Image Velocimetry) flow field testing experiment |
Publications (1)
Publication Number | Publication Date |
---|---|
CN102435769A true CN102435769A (en) | 2012-05-02 |
Family
ID=45983930
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2011103720528A Pending CN102435769A (en) | 2011-11-21 | 2011-11-21 | Method and device for spreading trace particles in supersonic PIV (Particle Image Velocimetry) flow field testing experiment |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN102435769A (en) |
Cited By (35)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103698553A (en) * | 2013-12-26 | 2014-04-02 | 天津大学 | Novel surface flow field velocity measurement system and velocity measurement method on basis of infrared image pickup |
CN103940573A (en) * | 2014-05-06 | 2014-07-23 | 大连理工大学 | Tracer particle dispensing device and dispensing method for small-size PIV flow field testing experiment |
CN104730286A (en) * | 2015-03-17 | 2015-06-24 | 北京理工大学 | Venting cavity inside particle dispensing device based on PIV |
CN105588700A (en) * | 2015-12-16 | 2016-05-18 | 西安交通大学 | Evaluation device and method for complex flow regime and heat transfer effect of swirling impinging jet |
CN105664744A (en) * | 2016-03-29 | 2016-06-15 | 江苏大学 | Particle dispenser for dispensing fine solid particles into airflow |
CN105891539A (en) * | 2015-12-17 | 2016-08-24 | 北京理工大学 | Particle dispensing device for PIV based internal flow field measurement of ventilated cavity |
CN106405145A (en) * | 2016-09-14 | 2017-02-15 | 昆明理工大学 | Device and method for measuring free settling velocity of coarse-particle solid |
CN106563584A (en) * | 2016-10-09 | 2017-04-19 | 上海交通大学 | Quick response concentration-controllable high-flow nano-particle spreader |
CN106895951A (en) * | 2017-02-22 | 2017-06-27 | 中国科学技术大学 | Hypersonic interior rotatable air intake duct and distance piece flow field chromatograph display methods, system |
CN107748053A (en) * | 2017-09-29 | 2018-03-02 | 中国空气动力研究与发展中心低速空气动力研究所 | Trace displaying particle generator |
CN107818197A (en) * | 2017-09-15 | 2018-03-20 | 南京航空航天大学 | A kind of force measuring method and device of the supersonic profile based on PIV technologies |
CN108519213A (en) * | 2018-06-06 | 2018-09-11 | 湖南云顶智能科技有限公司 | A kind of multipurpose trace particle broadcasts sowing fluidizer |
CN108627673A (en) * | 2018-04-24 | 2018-10-09 | 中国船舶科学研究中心(中国船舶重工集团公司第七0二研究所) | A kind of PIV trace particles wall surface sowing apparatus |
CN108760219A (en) * | 2018-05-23 | 2018-11-06 | 中国航空工业集团公司沈阳空气动力研究所 | A kind of adjustable-flow particle generator |
CN109084914A (en) * | 2018-09-17 | 2018-12-25 | 上海交通大学 | A kind of measurement of full field system and method for high temperature and high speed turbulence flux |
CN110095247A (en) * | 2019-06-04 | 2019-08-06 | 中国人民解放军国防科技大学 | Tracer particle scattering device, tracer particle scattering system and wind tunnel test system |
CN110763422A (en) * | 2019-09-29 | 2020-02-07 | 哈尔滨工程大学 | Comprehensive wind tunnel test system |
CN111238766A (en) * | 2020-01-16 | 2020-06-05 | 南方科技大学 | Tracer particle generator |
CN111623952A (en) * | 2020-04-29 | 2020-09-04 | 中国航天空气动力技术研究院 | Three-dimensional space flow field measuring device and method in sub-span wind tunnel |
CN112197934A (en) * | 2020-09-30 | 2021-01-08 | 中国空气动力研究与发展中心高速空气动力研究所 | Tracer particle concentration control method for large-scale high-speed wind tunnel PIV test |
CN112229597A (en) * | 2020-09-30 | 2021-01-15 | 中国空气动力研究与发展中心高速空气动力研究所 | Tracer particle generator for large-scale high-speed wind tunnel PIV test |
CN113041933A (en) * | 2021-03-09 | 2021-06-29 | 西南石油大学 | Device and method for keeping particle concentration stable in proppant velocity measurement experiment |
CN113281533A (en) * | 2021-05-19 | 2021-08-20 | 上海交通大学 | Solid-state tracer particle scattering device based on hourglass filling and multi-stage filtering |
CN113376401A (en) * | 2021-04-28 | 2021-09-10 | 西安交通大学 | Flow-controllable tracer molecule adding device and adding method thereof |
CN113484534A (en) * | 2021-07-05 | 2021-10-08 | 中国人民解放军国防科技大学 | Supersonic flow field characteristic testing system and method based on image processing |
CN113484533A (en) * | 2021-07-05 | 2021-10-08 | 中国人民解放军国防科技大学 | Visible light-infrared light coupling flow field measurement system based on image processing |
CN113640543A (en) * | 2021-06-29 | 2021-11-12 | 河海大学 | Automatic putting device and putting control method for tracer particles in unsteady flow |
CN113959676A (en) * | 2021-10-11 | 2022-01-21 | 南京航空航天大学 | Hypersonic flow display device and method based on Rayleigh scattering |
CN113970445A (en) * | 2021-10-14 | 2022-01-25 | 上海交通大学 | Entropy-sound test platform and test method thereof |
CN114252648A (en) * | 2021-12-22 | 2022-03-29 | 北京航空航天大学 | Tracer particle generator system and control method thereof |
CN114487474A (en) * | 2021-12-27 | 2022-05-13 | 北京理工大学 | Device for controlling supply of tracer particles |
US20220214245A1 (en) * | 2019-08-29 | 2022-07-07 | Zhejiang University | Tracer Particle Spreading Device for a Boundary Layer Flow Visualization Experiment Based on a Flat Plate |
CN115046730A (en) * | 2022-06-21 | 2022-09-13 | 中国科学院工程热物理研究所 | Self-drying solid tracer particle generating device, system and method |
CN115824560A (en) * | 2023-02-21 | 2023-03-21 | 中国空气动力研究与发展中心空天技术研究所 | Planar cascade wind tunnel PIV experiment slit tracer particle distribution device and distribution method |
CN117433738A (en) * | 2023-12-18 | 2024-01-23 | 中国空气动力研究与发展中心计算空气动力研究所 | Hypersonic wind tunnel |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1519565A (en) * | 2003-01-23 | 2004-08-11 | 申功� | Pressure type particle generator |
CN2852136Y (en) * | 2005-08-19 | 2006-12-27 | 北京航空航天大学 | Trace displaying particle generator |
US20110188622A1 (en) * | 2008-07-31 | 2011-08-04 | Jiddtek Pty Ltd | Neutral Particle Generator |
CN202158945U (en) * | 2011-05-11 | 2012-03-07 | 魏润杰 | Solid-state particle generator |
-
2011
- 2011-11-21 CN CN2011103720528A patent/CN102435769A/en active Pending
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1519565A (en) * | 2003-01-23 | 2004-08-11 | 申功� | Pressure type particle generator |
CN2852136Y (en) * | 2005-08-19 | 2006-12-27 | 北京航空航天大学 | Trace displaying particle generator |
US20110188622A1 (en) * | 2008-07-31 | 2011-08-04 | Jiddtek Pty Ltd | Neutral Particle Generator |
CN202158945U (en) * | 2011-05-11 | 2012-03-07 | 魏润杰 | Solid-state particle generator |
Non-Patent Citations (4)
Title |
---|
付甲尧: "石墨化填料的真空吸送", 《碳素》, 31 December 1982 (1982-12-31), pages 17 - 21 * |
代钦: "超音速喷流DPIV瞬时速度场实验测量", 《北京航空航天大学学报》, vol. 27, no. 6, 31 December 2001 (2001-12-31), pages 665 - 669 * |
单根立等: "气动真空上料机", 《液压与气动》, no. 4, 31 December 2006 (2006-12-31), pages 54 * |
蒋观沅: "物料的真空吸送及应用", 《真空》, no. 2, 31 December 1988 (1988-12-31), pages 30 - 33 * |
Cited By (52)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103698553A (en) * | 2013-12-26 | 2014-04-02 | 天津大学 | Novel surface flow field velocity measurement system and velocity measurement method on basis of infrared image pickup |
CN103940573A (en) * | 2014-05-06 | 2014-07-23 | 大连理工大学 | Tracer particle dispensing device and dispensing method for small-size PIV flow field testing experiment |
CN104730286B (en) * | 2015-03-17 | 2017-08-25 | 北京理工大学 | A kind of ventilation hole internal particle dispensing device based on PIV |
CN104730286A (en) * | 2015-03-17 | 2015-06-24 | 北京理工大学 | Venting cavity inside particle dispensing device based on PIV |
CN105588700A (en) * | 2015-12-16 | 2016-05-18 | 西安交通大学 | Evaluation device and method for complex flow regime and heat transfer effect of swirling impinging jet |
CN105588700B (en) * | 2015-12-16 | 2018-04-17 | 西安交通大学 | A kind of evaluating apparatus and method of rotary impact jet stream Complex Flow Status and heat transfer effect |
CN105891539B (en) * | 2015-12-17 | 2019-05-17 | 北京理工大学 | Particle sowing apparatus based on PIV ventilation hole interior flow field measurement |
CN105891539A (en) * | 2015-12-17 | 2016-08-24 | 北京理工大学 | Particle dispensing device for PIV based internal flow field measurement of ventilated cavity |
CN105664744A (en) * | 2016-03-29 | 2016-06-15 | 江苏大学 | Particle dispenser for dispensing fine solid particles into airflow |
CN105664744B (en) * | 2016-03-29 | 2018-08-21 | 江苏大学 | A kind of particle dispenser broadcasted sowing micro-solid particle in air-flow |
CN106405145B (en) * | 2016-09-14 | 2022-12-23 | 昆明理工大学 | Device and method for measuring free settling velocity of coarse particle solid |
CN106405145A (en) * | 2016-09-14 | 2017-02-15 | 昆明理工大学 | Device and method for measuring free settling velocity of coarse-particle solid |
CN106563584A (en) * | 2016-10-09 | 2017-04-19 | 上海交通大学 | Quick response concentration-controllable high-flow nano-particle spreader |
CN106895951A (en) * | 2017-02-22 | 2017-06-27 | 中国科学技术大学 | Hypersonic interior rotatable air intake duct and distance piece flow field chromatograph display methods, system |
CN107818197A (en) * | 2017-09-15 | 2018-03-20 | 南京航空航天大学 | A kind of force measuring method and device of the supersonic profile based on PIV technologies |
CN107818197B (en) * | 2017-09-15 | 2021-05-25 | 南京航空航天大学 | Supersonic airfoil force measuring method and device based on PIV technology |
CN107748053A (en) * | 2017-09-29 | 2018-03-02 | 中国空气动力研究与发展中心低速空气动力研究所 | Trace displaying particle generator |
CN108627673B (en) * | 2018-04-24 | 2021-03-16 | 中国船舶科学研究中心(中国船舶重工集团公司第七0二研究所) | PIV trace particle wall surface scattering device |
CN108627673A (en) * | 2018-04-24 | 2018-10-09 | 中国船舶科学研究中心(中国船舶重工集团公司第七0二研究所) | A kind of PIV trace particles wall surface sowing apparatus |
CN108760219A (en) * | 2018-05-23 | 2018-11-06 | 中国航空工业集团公司沈阳空气动力研究所 | A kind of adjustable-flow particle generator |
CN108519213A (en) * | 2018-06-06 | 2018-09-11 | 湖南云顶智能科技有限公司 | A kind of multipurpose trace particle broadcasts sowing fluidizer |
CN109084914A (en) * | 2018-09-17 | 2018-12-25 | 上海交通大学 | A kind of measurement of full field system and method for high temperature and high speed turbulence flux |
CN110095247A (en) * | 2019-06-04 | 2019-08-06 | 中国人民解放军国防科技大学 | Tracer particle scattering device, tracer particle scattering system and wind tunnel test system |
US20220214245A1 (en) * | 2019-08-29 | 2022-07-07 | Zhejiang University | Tracer Particle Spreading Device for a Boundary Layer Flow Visualization Experiment Based on a Flat Plate |
US11953405B2 (en) * | 2019-08-29 | 2024-04-09 | Zhejiang University | Tracer particle spreading device for a boundary layer flow visualization experiment based on a flat plate |
CN110763422A (en) * | 2019-09-29 | 2020-02-07 | 哈尔滨工程大学 | Comprehensive wind tunnel test system |
CN111238766B (en) * | 2020-01-16 | 2022-02-08 | 南方科技大学 | Tracer particle generator |
CN111238766A (en) * | 2020-01-16 | 2020-06-05 | 南方科技大学 | Tracer particle generator |
CN111623952A (en) * | 2020-04-29 | 2020-09-04 | 中国航天空气动力技术研究院 | Three-dimensional space flow field measuring device and method in sub-span wind tunnel |
CN112229597A (en) * | 2020-09-30 | 2021-01-15 | 中国空气动力研究与发展中心高速空气动力研究所 | Tracer particle generator for large-scale high-speed wind tunnel PIV test |
CN112229597B (en) * | 2020-09-30 | 2022-07-19 | 中国空气动力研究与发展中心高速空气动力研究所 | Tracer particle generator for large-scale high-speed wind tunnel PIV test |
CN112197934A (en) * | 2020-09-30 | 2021-01-08 | 中国空气动力研究与发展中心高速空气动力研究所 | Tracer particle concentration control method for large-scale high-speed wind tunnel PIV test |
CN113041933A (en) * | 2021-03-09 | 2021-06-29 | 西南石油大学 | Device and method for keeping particle concentration stable in proppant velocity measurement experiment |
CN113376401A (en) * | 2021-04-28 | 2021-09-10 | 西安交通大学 | Flow-controllable tracer molecule adding device and adding method thereof |
CN113281533A (en) * | 2021-05-19 | 2021-08-20 | 上海交通大学 | Solid-state tracer particle scattering device based on hourglass filling and multi-stage filtering |
CN113281533B (en) * | 2021-05-19 | 2022-11-01 | 上海交通大学 | Solid-state tracer particle scattering device based on hourglass filling and multi-stage filtering |
CN113640543A (en) * | 2021-06-29 | 2021-11-12 | 河海大学 | Automatic putting device and putting control method for tracer particles in unsteady flow |
CN113484533B (en) * | 2021-07-05 | 2024-02-27 | 中国人民解放军国防科技大学 | Visible light-infrared light coupling flow field measurement system based on image processing |
CN113484534A (en) * | 2021-07-05 | 2021-10-08 | 中国人民解放军国防科技大学 | Supersonic flow field characteristic testing system and method based on image processing |
CN113484533A (en) * | 2021-07-05 | 2021-10-08 | 中国人民解放军国防科技大学 | Visible light-infrared light coupling flow field measurement system based on image processing |
CN113484534B (en) * | 2021-07-05 | 2024-04-09 | 中国人民解放军国防科技大学 | Supersonic flow field characteristic test system and method based on image processing |
CN113959676A (en) * | 2021-10-11 | 2022-01-21 | 南京航空航天大学 | Hypersonic flow display device and method based on Rayleigh scattering |
CN113970445A (en) * | 2021-10-14 | 2022-01-25 | 上海交通大学 | Entropy-sound test platform and test method thereof |
CN113970445B (en) * | 2021-10-14 | 2023-02-10 | 上海交通大学 | Entropy-sound test platform and test method thereof |
CN114252648A (en) * | 2021-12-22 | 2022-03-29 | 北京航空航天大学 | Tracer particle generator system and control method thereof |
CN114487474B (en) * | 2021-12-27 | 2023-02-03 | 北京理工大学 | Device for controlling supply of tracer particles |
CN114487474A (en) * | 2021-12-27 | 2022-05-13 | 北京理工大学 | Device for controlling supply of tracer particles |
CN115046730A (en) * | 2022-06-21 | 2022-09-13 | 中国科学院工程热物理研究所 | Self-drying solid tracer particle generating device, system and method |
CN115046730B (en) * | 2022-06-21 | 2024-07-09 | 中国科学院工程热物理研究所 | Self-drying solid trace particle generating device, system and method |
CN115824560B (en) * | 2023-02-21 | 2023-04-14 | 中国空气动力研究与发展中心空天技术研究所 | Planar cascade wind tunnel PIV experiment slit tracer particle distribution device and distribution method |
CN115824560A (en) * | 2023-02-21 | 2023-03-21 | 中国空气动力研究与发展中心空天技术研究所 | Planar cascade wind tunnel PIV experiment slit tracer particle distribution device and distribution method |
CN117433738A (en) * | 2023-12-18 | 2024-01-23 | 中国空气动力研究与发展中心计算空气动力研究所 | Hypersonic wind tunnel |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN102435769A (en) | Method and device for spreading trace particles in supersonic PIV (Particle Image Velocimetry) flow field testing experiment | |
CN202158945U (en) | Solid-state particle generator | |
CN204649518U (en) | A kind of dynamically aerosol diluter | |
CN206192621U (en) | Experimental high -efficient jumbo size of intake duct is drawn and is penetrated piping installation | |
US20220214245A1 (en) | Tracer Particle Spreading Device for a Boundary Layer Flow Visualization Experiment Based on a Flat Plate | |
CN109506744A (en) | A kind of aero-engine overall test Venturi nozzle air mass flow calibration method | |
CN104535795B (en) | Low-pressure space jet flow particle picture speed measurement experiment device | |
CN203824731U (en) | A tracer particle scattering apparatus used in a small-size PIV flow field testing experiment | |
CN108627673B (en) | PIV trace particle wall surface scattering device | |
CN110095247B (en) | Tracer particle scattering device, tracer particle scattering system and wind tunnel test system | |
CN205538610U (en) | A dust and sand feed arrangement for sand and dust test chamber | |
CN105890871A (en) | Tracer particle putting device used for liquid flow field particle image velocimeter (PIV) measurement | |
CN106153816A (en) | Cyclone fluidized bed solids generator | |
CN106441781B (en) | A kind of measurable air intake duct throttling set of flow | |
CN102680220B (en) | Method and device for measuring hydraulic characteristic of trickle irrigation emitter | |
CN106949989A (en) | A kind of hemispherical head steady temperature force combination probe for measuring low speed three-dimensional flow field | |
CN106000707B (en) | A kind of rain controller | |
CN202033227U (en) | Constant speed gas distribution sampling device for atmosphere particulate matter monitoring instrument | |
CN110763265B (en) | System and method for testing atomization spraying effect of natural gas drag reducer | |
CN202133528U (en) | Active flow control experimental device for high-speed wind tunnel air intake duct | |
CN208026450U (en) | Gas driven generator blowing experiment device | |
CN208297087U (en) | A kind of Flow Field outside test test segment structure | |
CN204287224U (en) | A kind of low-voltage space jet PIV tests the speed experimental provision | |
CN209952617U (en) | Real-time liquid preparation device for mixing two liquids | |
CN205157480U (en) | Measure device that CO2 drove extraction liquid well head throttling effect coefficient |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C12 | Rejection of a patent application after its publication | ||
RJ01 | Rejection of invention patent application after publication |
Application publication date: 20120502 |