CN111272947A - Visual combustion test device with sound excitation system - Google Patents
Visual combustion test device with sound excitation system Download PDFInfo
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- CN111272947A CN111272947A CN202010201827.4A CN202010201827A CN111272947A CN 111272947 A CN111272947 A CN 111272947A CN 202010201827 A CN202010201827 A CN 202010201827A CN 111272947 A CN111272947 A CN 111272947A
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- 238000002485 combustion reaction Methods 0.000 title claims abstract description 79
- 230000000007 visual effect Effects 0.000 title claims abstract description 61
- 238000012360 testing method Methods 0.000 title claims abstract description 19
- 230000005284 excitation Effects 0.000 title claims abstract description 18
- 239000011148 porous material Substances 0.000 claims abstract description 8
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 7
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 7
- 239000011888 foil Substances 0.000 claims abstract description 7
- 238000007789 sealing Methods 0.000 claims description 15
- 238000003466 welding Methods 0.000 claims description 6
- 239000004809 Teflon Substances 0.000 claims description 4
- 229920006362 Teflon® Polymers 0.000 claims description 4
- 239000003292 glue Substances 0.000 claims description 3
- 239000010453 quartz Substances 0.000 claims description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicon dioxide Inorganic materials O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 claims description 3
- 230000000638 stimulation Effects 0.000 claims 9
- 238000002474 experimental method Methods 0.000 abstract description 10
- 239000010410 layer Substances 0.000 description 12
- 239000007789 gas Substances 0.000 description 11
- 230000000694 effects Effects 0.000 description 9
- 239000000446 fuel Substances 0.000 description 6
- 238000011160 research Methods 0.000 description 6
- 238000013461 design Methods 0.000 description 4
- 238000006243 chemical reaction Methods 0.000 description 3
- 238000011161 development Methods 0.000 description 3
- 238000003745 diagnosis Methods 0.000 description 3
- 239000002737 fuel gas Substances 0.000 description 3
- 238000005259 measurement Methods 0.000 description 3
- 239000005030 aluminium foil Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000008569 process Effects 0.000 description 2
- 238000012545 processing Methods 0.000 description 2
- 230000004044 response Effects 0.000 description 2
- 239000002356 single layer Substances 0.000 description 2
- UGFAIRIUMAVXCW-UHFFFAOYSA-N Carbon monoxide Chemical compound [O+]#[C-] UGFAIRIUMAVXCW-UHFFFAOYSA-N 0.000 description 1
- YCKRFDGAMUMZLT-UHFFFAOYSA-N Fluorine atom Chemical compound [F] YCKRFDGAMUMZLT-UHFFFAOYSA-N 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 229910002091 carbon monoxide Inorganic materials 0.000 description 1
- 239000006185 dispersion Substances 0.000 description 1
- 229910052731 fluorine Inorganic materials 0.000 description 1
- 239000011737 fluorine Substances 0.000 description 1
- 229910052739 hydrogen Inorganic materials 0.000 description 1
- 239000001257 hydrogen Substances 0.000 description 1
- 125000004435 hydrogen atom Chemical class [H]* 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012806 monitoring device Methods 0.000 description 1
- 230000010355 oscillation Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N31/00—Investigating or analysing non-biological materials by the use of the chemical methods specified in the subgroup; Apparatus specially adapted for such methods
- G01N31/12—Investigating or analysing non-biological materials by the use of the chemical methods specified in the subgroup; Apparatus specially adapted for such methods using combustion
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- Combustion & Propulsion (AREA)
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- Engineering & Computer Science (AREA)
- Analytical Chemistry (AREA)
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- General Health & Medical Sciences (AREA)
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Abstract
The invention relates to a visual combustion test device with a sound excitation system, which comprises a visual cylindrical combustion chamber, wherein an outer pipe swirl passage and an inner pipe swirl passage are positioned below the visual cylindrical combustion chamber, the visual cylindrical combustion chamber and the outer pipe swirl passage are both connected with a visual combustion chamber base, the center of the inner pipe swirl passage is connected with a central pipeline, and the bottom of the inner pipe is provided with an aluminum foil honeycomb pore plate; the outer pipe air inlet pipe is connected with the outer pipe; the inner pipe base and the outer pipe base are hermetically connected with the chamber; the central pipeline is hermetically connected with the central air inlet pipe; a central air inlet duct passes through the chamber; the cavity air inlet pipe is communicated with the cavity; the chamber is connected with the chamber base; the chamber porous plate is connected with a special loudspeaker; the special loudspeaker is connected with the chamber base; the special power amplifier is connected with the special loudspeaker through a signal line, and the waveform generator is connected with the special power amplifier through a data line. The invention provides a reference combustor for domestic experiments of sound-excited turbulent combustion.
Description
Technical Field
The invention relates to a visual combustion test device with a sound excitation system, which can be widely applied to the development of experimental research on combustion states in various combustion modes, various gas mixing combustion and various sound excitations.
Background
In the current research on turbulent flame characteristics, the premixing degree of fuel gas and air and the complex interaction problem between the turbulent flow and the flame have very important influence on the characteristics of a combustion device, and accurate experimental measurement research on the characteristics is urgently needed. The experiment research on turbulent flow rotating part premixed flame under sound excitation in China is not enough, and particularly, a standard combustion test bed device with complete functions and accurate and controllable is lacked.
Disclosure of Invention
The invention aims to provide a visual combustion test device with an acoustic excitation system.
The invention realizes the purpose through the following technical scheme: a visual combustion test device with a sound excitation system comprises a visual cylindrical combustion chamber, wherein the visual cylindrical combustion chamber is made of quartz tubes, an outer tube cyclone channel and an inner tube cyclone channel are positioned below the visual cylindrical combustion chamber, the visual cylindrical combustion chamber and the outer tube cyclone channel are both connected with a visual combustion chamber base, the visual cylindrical combustion chamber and the visual combustion chamber base are directly compressed, and the outer tube cyclone channel is in threaded connection with the visual combustion chamber base; the center of the inner pipe rotational flow channel is connected with a central pipeline, and an aluminum foil honeycomb pore plate is arranged at the bottom of the inner pipe; the first outer pipe air inlet pipe and the second outer pipe air inlet pipe are connected with the outer pipe through a pagoda head in a welding mode; the inner pipe base and the outer pipe base are hermetically connected with the chamber through mortise and tenon joints and bolts; the central pipeline and the central air inlet pipe are hermetically connected through a Teflon elbow with conical threads; the central air inlet pipeline penetrates through the chamber, and the joint of the chamber and the central air inlet pipeline is sealed by the thread sealing device; the first chamber air inlet pipe and the second chamber air inlet pipe are communicated with the chamber through welding of a pagoda head; the chamber is connected with the chamber base through a bolt; the chamber porous plate is connected with the special loudspeaker through a bolt; the special loudspeaker is connected with the chamber base through a bolt; the special power amplifier is connected with the special loudspeaker through a signal line, and the waveform generator is connected with the special power amplifier through a data line.
Further, the chamber is a large chamber with the bottom diameter of 146 mm.
Further, the length of the inner pipe and the outer pipe is 300 mm.
Further, the outer pipe swirl passage is machined with external tapered threads, the outer pipe is machined with internal tapered threads, and the corresponding threads are matched with each other.
Further, the inner tube swirl passage is machined with external tapered threads, the inner tube is machined with internal tapered threads, and the corresponding threads are matched with each other.
Furthermore, the outer pipe and the inner pipe are both provided with external conical threads, the bases of the inner pipe and the outer pipe are provided with corresponding internal conical threads, and the corresponding threads are matched with each other.
Furthermore, the contact positions of the inner pipe base and the outer pipe base with the chamber are step-shaped connectors and are connected through sealing glue and bolts.
Furthermore, the outer pipe swirl channel and the inner pipe swirl channel are slightly higher than the bottom of the visual cylindrical combustion chamber.
Furthermore, the aluminum foil honeycomb pore plate is welded between the inner pipe and the central pipeline through a pagoda head.
Further, the diameter of the special loudspeaker corresponds to the diameter of the chamber perforated plate.
Compared with the prior art, the visual combustion test device with the sound excitation system has the beneficial effects that: the design of a three-layer circular tube structure is adopted, the structures of the middle layer and the outer layer are very similar, the middle layer (namely an inner tube) and the inner layer (namely a central pipeline) are mutually related through small holes, different premixing effects are achieved by adjusting the positions of the holes, a single-layer or double-layer flame experiment can be designed according to actual requirements, a mixing combustion experiment of various fuel gases can be carried out according to requirements, an ideal partial premixing/non-premixing and swirling flow effect is achieved, and meanwhile, the device can be well matched with other measuring and detecting instruments for use; the device is characterized in that the large cavity below the device is designed, so that the full premixing effect of gas is met, sufficient space is provided for good resonance reaction of excitation generated by the loudspeaker, the measurement requirements of flame combustion parameters under different self-excitation states can be met, the device is novel in design, convenient to process and reliable in work. In addition, the rotational flow channel is printed and processed by 3D, the geometric accuracy is high, the cost is reasonable, parts with different specifications are easy to disassemble and replace, and the application is wide. And corresponding parameter changes can be carried out according to the specific experimental requirements, great help is provided for the research of turbulent flow rotary combustion, and a reference combustor is provided for the domestic development of the experiment of sound excitation turbulent flow combustion.
Drawings
Fig. 1 is a schematic sectional structure of the present invention.
Fig. 2 is a schematic structural view of the swirling passage of the outer tube.
Fig. 3 is a schematic structural view of the swirling passage of the inner tube.
Fig. 4 is a schematic structural view of the chamber.
In the figure, 1, visual cylindrical combustion chamber, 2, outer tube whirl passageway, 3, inner tube whirl passageway, 4, central authorities 'pipeline, 5, the outer tube, 6, the inner tube, 7, first outer tube intake pipe, 8, second outer tube intake pipe, 9, aluminium foil honeycomb orifice plate, 10, interior outer tube base, 11, the cavity, 12, special fluorine dragon return bend, 13, central authorities' intake pipe, 14, thread sealing device, 15, first cavity intake pipe, 16, second cavity intake pipe, 17, the cavity base, 18, the cavity perforated plate, 19, special speaker, 20, special power amplifier, 21, waveform generator, 22, visual combustion chamber base, 23, the signal line, 24, the data line.
Detailed Description
Referring to fig. 1 to 4, a visual combustion test device with a sound excitation system includes a visual cylindrical combustion chamber 1, the visual cylindrical combustion chamber 1 is made of a quartz tube, an outer tube swirling channel 2 and an inner tube swirling channel 3 are located below the visual cylindrical combustion chamber 1, the visual cylindrical combustion chamber 1 and the outer tube swirling channel 2 are both connected with a visual combustion chamber base 22, the visual cylindrical combustion chamber 1 and the visual combustion chamber base 22 are directly compressed to ensure sealing, and the outer tube swirling channel 2 and the visual combustion chamber base 22 are in threaded connection; the center of the inner pipe rotational flow channel 3 is connected with a central pipeline 4, the outer pipe rotational flow channel 2 is connected with an outer pipe 5 through conical threads, and the inner pipe rotational flow channel 3 is connected with an inner pipe 6 through the conical threads; the outer pipe 5 and the inner pipe 6 are both connected with the inner pipe base and the outer pipe base 10 through conical threads; the bottom of the inner pipe 6 is provided with an aluminum foil honeycomb pore plate 9; the first outer tube air inlet pipe 7 and the second outer tube air inlet pipe 8 are connected with the outer tube 5 through welding of pagoda heads; the inner pipe base 10 and the outer pipe base 10 are hermetically connected with the chamber 11 through mortise and tenon joints and bolts; the central pipeline 4 and the central air inlet pipe 13 are hermetically connected through a Teflon elbow 12 with conical threads; the central air inlet pipe 13 passes through the chamber 11, and the threaded sealing device 14 seals the joint of the chamber 11 and the central air inlet pipe 13; the first chamber air inlet pipe 15 and the second chamber air inlet pipe 16 are communicated with the chamber 11 through welding of a pagoda head; the chamber 11 is connected with the chamber base 17 through bolts; the chamber porous plate 18 is connected with a special loudspeaker 19 through a bolt; the special speaker 19 is connected with the chamber base 17 through bolts; the special power amplifier 20 is connected with the special loudspeaker 19 through a signal line 23, and the waveform generator 21 is connected with the special power amplifier 20 through a data line 24.
The cavity 11 is a large cavity with the bottom diameter of 146mm, so that the air flow can be ensured to reach a fully mixed state, and meanwhile, enough space is ensured to perform a good resonance reaction on the excitation generated by the loudspeaker, and stable oscillation is formed.
The length of the inner pipe 5 and the outer pipe 6 is 300mm, which can ensure that the air flow can reach a fully developed turbulent flow state.
The first outer tube inlet pipe 7 and the second outer tube inlet pipe 8 are supplied with a fixed flow of fuel and air to ensure that the premixed fuel meets the ignition and experimental requirements.
The first chamber intake 15 and the second chamber intake 16 enter a fixed flow of fuel and air to ensure that the premixed fuel meets ignition and experimental requirements.
Outer tube whirl passageway 2 processing has outside awl screw thread, and outer tube 5 processing has inside awl screw thread, and corresponding screw thread cooperates each other, and furthest's assurance leakproofness.
The inner pipe rotational flow channel 3 is processed with external conical threads, the inner pipe 6 is processed with internal conical threads, corresponding threads are matched with each other, and the sealing performance is guaranteed to the maximum extent.
The outer pipe 5 and the inner pipe 6 are both provided with external conical threads, the inner pipe base 10 and the outer pipe base are provided with corresponding internal conical threads, the corresponding threads are matched with each other, and the sealing performance is guaranteed to the maximum extent.
When the inner pipe base 10 and the outer pipe base 10 are designed in a printing mode, step-shaped connectors are designed at positions where the inner pipe base and the outer pipe base are in contact with the cavity 11 and are connected through sealing glue and bolts, and sealing performance is guaranteed.
The outer tube cyclone channel 2 and the inner tube cyclone channel 3 are slightly higher than the bottom of the visual cylindrical combustion chamber, so that light paths can enter the visual cylindrical combustion chamber conveniently and laser diagnosis experiments can be performed conveniently.
The visual cylindrical combustion chamber 1 and the visual combustion chamber base 22 are directly compressed to ensure sealing; the outer pipe swirl channel 2 is in threaded connection with the visual combustion chamber base 22.
The aluminium foil honeycomb pore plate 9 is welded between the inner pipe 6 and the central pipe 4 through a pagoda head, ensuring that a sufficient dispersion effect is generated for the air flow.
The central pipeline 4 and the central air inlet pipe 13 are processed with external conical threads, the two ends of the Teflon elbow 12 are processed with internal conical threads, and the corresponding threads are matched with each other to ensure the sealing property.
The chamber 11 and the chamber base 17 are processed with 8 corresponding bolt holes, the chamber base 17 and the special loudspeaker 19 are processed with 8 corresponding bolt holes, and 16 bolt connections are formed in total to ensure sealing.
The diameter of the special loudspeaker 19 corresponds to that of the chamber porous plate 18, so that good response of airflow to sound wave excitation is ensured; the special power amplifier 20 is communicated with the special loudspeaker 19 through a signal line 23, and the waveform generator 21 is connected with the special power amplifier 20 through a data line 24, so that the instruction of the pc end is stably and accurately transmitted.
The working principle of the invention is as follows:
the waveform generator 21 causes the loudspeaker 19 to produce a sound shock wave of a specific frequency, waveform and amplitude through the dedicated power amplifier 20, exerting a "self-excitation" effect on the overall burner. Fuel and air respectively enter the outer pipe 5 from the first outer pipe air inlet pipe 7 and the second outer pipe air inlet pipe 8 left and right, and respectively bypass the pipelines to form convection so as to carry out first-step mixing; the fuel and the air respectively enter the cavity 11 from the first cavity air inlet pipe 15 and the second cavity air inlet pipe 16 from left to right, and respectively bypass the central space of the cavity to form convection for carrying out the first-step mixing. The chamber gas mixture passes through the aluminum foil honeycomb pore plate 9 to rectify the airflow, so that the airflow becomes smoother and more uniform. The mixed gas in the inner pipeline and the outer pipeline is mixed in the respective pipelines to obtain the mixed gas with different mixing degrees. Hydrogen, carbon monoxide and methane can enter the central pipeline 4 from the central air inlet pipe 13, and then can enter the inner pipe 6 from the side wall opening of the central pipeline 4, and the mixing degree with the incoming flow can be adjusted by changing the height of the opening position, so that partial premixing combustion modes with different degrees are realized; alternatively, the top of the central duct 4 is perforated so that the gas enters the visible cylindrical combustion chamber 1 directly from the top, obtaining a non-premixed combustion mode. The mixed gas in the outer pipe 5 enters the outer pipe swirl channel 2, the mixed gas in the inner pipe 6 enters the inner pipe swirl channel 3, and due to the action of the fan blades and the inertia effect, stable rotating turbulent airflow is formed and enters the visual cylindrical combustion chamber 1. The stable rotating turbulent gas enters the visual cylindrical combustion chamber 1, is ignited and is correspondingly observed and measured by laser diagnosis. The diameter and the length of the visual cylindrical combustion chamber 1 can be adjusted, and the response characteristics of the combustion chamber to different sound excitation frequencies are tested. The outlet of the outer tube cyclone channel 2 and the outlet of the inner tube cyclone channel 3 are slightly higher than the bottom of the visual cylindrical combustion chamber 1, so that the light path can enter and the laser diagnosis experiment can be facilitated. The visual cylindrical combustion chamber 1 is a semi-sealing device with an opening at the top end, a pressure monitoring device can be installed on the wall surface of the visual cylindrical combustion chamber, and a tail gas treatment device can be installed at the top end of the visual cylindrical combustion chamber.
The invention adopts a three-layer circular tube structure design, the structures of the middle layer and the outer layer are very similar, the middle layer (namely the inner tube) and the inner layer (namely the central pipeline) are mutually related through a small hole, different premixing effects are achieved by adjusting the position of the open hole, a single-layer or double-layer flame experiment can be designed according to actual requirements, a mixing combustion experiment of various fuel gases can be carried out according to requirements, an ideal partial premixing/non-premixing and swirling flow effect is achieved, and meanwhile, the invention can be well matched with other measuring and detecting instruments for use; the device is characterized in that the large cavity below the device is designed, so that the full premixing effect of gas is met, sufficient space is provided for good resonance reaction of excitation generated by the loudspeaker, the measurement requirements of flame combustion parameters under different self-excitation states can be met, the device is novel in design, convenient to process and reliable in work. In addition, the rotational flow channel is printed and processed by 3D, the geometric accuracy is high, the cost is reasonable, parts with different specifications are easy to disassemble and replace, and the application is wide. And corresponding parameter changes can be carried out according to the specific experimental requirements, great help is provided for the research of turbulent flow rotary combustion, and a reference combustor is provided for the domestic development of the experiment of sound excitation turbulent flow combustion.
What has been described above are merely some embodiments of the present invention. It will be apparent to those skilled in the art that various changes and modifications can be made without departing from the inventive concept thereof, and these changes and modifications can be made without departing from the spirit and scope of the invention.
Claims (10)
1. The utility model provides a visual combustion test device with sound excitation system which characterized in that: the visual cylindrical combustion chamber is made of quartz tubes, an outer tube cyclone channel and an inner tube cyclone channel are located below the visual cylindrical combustion chamber, the visual cylindrical combustion chamber and the outer tube cyclone channel are connected with a visual combustion chamber base, the visual cylindrical combustion chamber and the visual combustion chamber base are directly compressed, and the outer tube cyclone channel is in threaded connection with the visual combustion chamber base; the center of the inner pipe rotational flow channel is connected with a central pipeline, and an aluminum foil honeycomb pore plate is arranged at the bottom of the inner pipe; the first outer pipe air inlet pipe and the second outer pipe air inlet pipe are connected with the outer pipe through a pagoda head in a welding mode; the inner pipe base and the outer pipe base are hermetically connected with the chamber through mortise and tenon joints and bolts; the central pipeline and the central air inlet pipe are hermetically connected through a Teflon elbow with conical threads; the central air inlet pipeline penetrates through the chamber, and the joint of the chamber and the central air inlet pipeline is sealed by the thread sealing device; the first chamber air inlet pipe and the second chamber air inlet pipe are communicated with the chamber through welding of a pagoda head; the chamber is connected with the chamber base through a bolt; the chamber porous plate is connected with the special loudspeaker through a bolt; the special loudspeaker is connected with the chamber base through a bolt; the special power amplifier is connected with the special loudspeaker through a signal line, and the waveform generator is connected with the special power amplifier through a data line.
2. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the chamber is a large chamber with the bottom diameter of 146 mm.
3. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the length of the inner pipe and the outer pipe is 300 mm.
4. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the outer pipe rotational flow channel is processed with external conical threads, the outer pipe is processed with internal conical threads, and the corresponding threads are matched with each other.
5. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the inner tube rotational flow channel is processed with external conical threads, the inner tube is processed with internal conical threads, and the corresponding threads are matched with each other.
6. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the outer pipe and the inner pipe are respectively provided with external conical threads at the bottom, the inner pipe base and the outer pipe base are respectively provided with corresponding internal conical threads, and the corresponding threads are matched with each other.
7. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the positions where the inner pipe base and the outer pipe base are contacted with the chamber are all step-shaped connectors and are connected through sealing glue and bolts.
8. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the outer pipe swirl passage and the inner pipe swirl passage are slightly higher than the bottom of the visual cylindrical combustion chamber.
9. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the aluminum foil honeycomb pore plate is welded between the inner pipe and the central pipeline through the pagoda head.
10. The visual combustion testing apparatus with an acoustic stimulation system as set forth in claim 1, wherein: the diameter of the special loudspeaker corresponds to the diameter of the chamber porous plate.
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010201827.4A CN111272947A (en) | 2020-03-20 | 2020-03-20 | Visual combustion test device with sound excitation system |
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| Application Number | Priority Date | Filing Date | Title |
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| CN202010201827.4A CN111272947A (en) | 2020-03-20 | 2020-03-20 | Visual combustion test device with sound excitation system |
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| CN111272947A true CN111272947A (en) | 2020-06-12 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111829787A (en) * | 2020-06-23 | 2020-10-27 | 江苏大学 | Visual combustion experiment platform capable of realizing multiple mixing |
| CN113960242A (en) * | 2021-09-17 | 2022-01-21 | 江苏大学 | Staged combustor with two radial rotating inflow channels |
| WO2022127932A1 (en) * | 2020-12-18 | 2022-06-23 | 郑州大学 | Experimentation apparatus for turbulent flames |
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| Publication number | Priority date | Publication date | Assignee | Title |
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| CN102410533A (en) * | 2011-10-27 | 2012-04-11 | 中国科学院广州能源研究所 | Swirl triple-tube burner |
| CN108414231A (en) * | 2018-06-07 | 2018-08-17 | 湖南云顶智能科技有限公司 | Modular trial device for swirl flow combustion thermal acoustic oscillation characteristic research |
| CN109164203A (en) * | 2018-07-24 | 2019-01-08 | 江苏大学 | A kind of low-loss turbulent combustion Visualization platform device with rotation inflow channel |
| CN212060112U (en) * | 2020-03-20 | 2020-12-01 | 蓝色火焰能源科技(镇江)有限公司 | Visual combustion test device with sound excitation system |
-
2020
- 2020-03-20 CN CN202010201827.4A patent/CN111272947A/en active Pending
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102410533A (en) * | 2011-10-27 | 2012-04-11 | 中国科学院广州能源研究所 | Swirl triple-tube burner |
| CN108414231A (en) * | 2018-06-07 | 2018-08-17 | 湖南云顶智能科技有限公司 | Modular trial device for swirl flow combustion thermal acoustic oscillation characteristic research |
| CN109164203A (en) * | 2018-07-24 | 2019-01-08 | 江苏大学 | A kind of low-loss turbulent combustion Visualization platform device with rotation inflow channel |
| CN212060112U (en) * | 2020-03-20 | 2020-12-01 | 蓝色火焰能源科技(镇江)有限公司 | Visual combustion test device with sound excitation system |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111829787A (en) * | 2020-06-23 | 2020-10-27 | 江苏大学 | Visual combustion experiment platform capable of realizing multiple mixing |
| CN111829787B (en) * | 2020-06-23 | 2022-07-22 | 江苏大学 | Visual combustion experiment platform capable of realizing multiple mixing |
| WO2022127932A1 (en) * | 2020-12-18 | 2022-06-23 | 郑州大学 | Experimentation apparatus for turbulent flames |
| CN113960242A (en) * | 2021-09-17 | 2022-01-21 | 江苏大学 | Staged combustor with two radial rotating inflow channels |
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