CN219871124U - Device for rapidly analyzing gas components and explosion characteristics - Google Patents
Device for rapidly analyzing gas components and explosion characteristics Download PDFInfo
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- CN219871124U CN219871124U CN202320390316.0U CN202320390316U CN219871124U CN 219871124 U CN219871124 U CN 219871124U CN 202320390316 U CN202320390316 U CN 202320390316U CN 219871124 U CN219871124 U CN 219871124U
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- 238000004880 explosion Methods 0.000 title claims abstract description 120
- 230000007246 mechanism Effects 0.000 claims abstract description 72
- 238000004868 gas analysis Methods 0.000 claims abstract description 38
- 230000003287 optical effect Effects 0.000 claims abstract description 25
- 238000002474 experimental method Methods 0.000 claims abstract description 24
- 238000002347 injection Methods 0.000 claims abstract description 21
- 239000007924 injection Substances 0.000 claims abstract description 21
- 239000000203 mixture Substances 0.000 claims abstract description 20
- 238000005070 sampling Methods 0.000 claims description 22
- 238000004458 analytical method Methods 0.000 claims description 9
- 239000007789 gas Substances 0.000 abstract description 201
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 abstract description 6
- 239000001301 oxygen Substances 0.000 abstract description 6
- 229910052760 oxygen Inorganic materials 0.000 abstract description 6
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 abstract description 4
- 238000011156 evaluation Methods 0.000 abstract description 3
- 229910052757 nitrogen Inorganic materials 0.000 abstract description 2
- 238000001514 detection method Methods 0.000 description 16
- 239000004215 Carbon black (E152) Substances 0.000 description 9
- 229930195733 hydrocarbon Natural products 0.000 description 9
- 150000002430 hydrocarbons Chemical class 0.000 description 9
- 238000012360 testing method Methods 0.000 description 7
- 239000010963 304 stainless steel Substances 0.000 description 6
- 229910000589 SAE 304 stainless steel Inorganic materials 0.000 description 6
- 239000007788 liquid Substances 0.000 description 6
- 230000036284 oxygen consumption Effects 0.000 description 5
- 230000008859 change Effects 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 238000005259 measurement Methods 0.000 description 4
- 238000001237 Raman spectrum Methods 0.000 description 2
- 230000020169 heat generation Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012544 monitoring process Methods 0.000 description 2
- 239000000243 solution Substances 0.000 description 2
- 230000003595 spectral effect Effects 0.000 description 2
- 238000001228 spectrum Methods 0.000 description 2
- 230000000087 stabilizing effect Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 230000033228 biological regulation Effects 0.000 description 1
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- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 230000001276 controlling effect Effects 0.000 description 1
- 238000013500 data storage Methods 0.000 description 1
- 230000006837 decompression Effects 0.000 description 1
- 238000013461 design Methods 0.000 description 1
- 238000010586 diagram Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000835 fiber Substances 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 239000002245 particle Substances 0.000 description 1
- 230000035699 permeability Effects 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 238000012545 processing Methods 0.000 description 1
- 238000010926 purge Methods 0.000 description 1
- 238000011002 quantification Methods 0.000 description 1
- 238000004445 quantitative analysis Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 239000002341 toxic gas Substances 0.000 description 1
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Abstract
The device for rapidly analyzing the gas components and the explosion characteristics comprises a gas inlet mechanism, wherein the gas outlet end of the gas inlet mechanism is communicated with a gas analysis mechanism, the gas outlet end of the gas analysis mechanism is communicated with an experiment mechanism, and the gas outlet end of the experiment mechanism is communicated with the gas inlet mechanism; the gas analysis mechanism comprises an electronic pressure control valve communicated with the gas outlet end of the gas inlet mechanism, the gas outlet end of the electronic pressure control valve is communicated with an optical gas analysis system, and the gas outlet end of the optical gas analysis system is communicated with the experimental mechanism through an explosion sample injection control electromagnetic valve; the utility model can detect the components and the content of the combustible gas, can detect the content of nitrogen and oxygen in the gas mixture, can perform preliminary judgment on the explosion risk of the mixed gas, and then performs ignition experiment on the mixture of the combustible gas and air according to the preliminary judgment result to determine the actual explosion limit of the combustible gas; the comprehensive evaluation of the explosion characteristics of the combustible gas is realized.
Description
Technical Field
The utility model relates to the technical field of flammable gas risk evaluation, in particular to a device for rapidly analyzing gas components and explosion characteristics.
Background
In the energy fields of petroleum, mines, new energy exchange and the like, various combustible gas mixtures remain for a long time or the combustible gas mixtures are accidentally generated and released due to accidents, and when the combustible gas mixtures are continuously gathered in a limited space to reach explosion concentration, ignition sources such as high temperature or spark can cause the combustible gas mixtures to be severely exploded, so that the life safety of practitioners is seriously endangered.
The existing combustible gas explosion characteristic measuring device only considers the mixing proportion of the combustible gas and air, only measures the explosion pressure and the explosion flame temperature in an ignition experiment, and lacks the mechanistic analysis of explosion and the quantification of explosion energy.
Disclosure of Invention
The present utility model is directed to a device for rapidly analyzing gas components and explosion characteristics, which solves the above-mentioned problems of the prior art.
The device for rapidly analyzing the gas components and the explosion characteristics comprises a gas inlet mechanism, wherein the gas outlet end of the gas inlet mechanism is communicated with a gas analysis mechanism, the gas outlet end of the gas analysis mechanism is communicated with an experiment mechanism, and the gas outlet end of the experiment mechanism is communicated with the gas inlet mechanism;
the gas analysis mechanism comprises an electronic pressure control valve communicated with the gas outlet end of the gas inlet mechanism, the gas outlet end of the electronic pressure control valve is communicated with an optical gas analysis system, and the gas outlet end of the optical gas analysis system is communicated with the experimental mechanism through an explosion sample injection control electromagnetic valve;
the experimental mechanism comprises an explosion cabin communicated with the explosion sample injection control electromagnetic valve, an ignition assembly and a pressure sensor are fixedly arranged on the bulkhead of the explosion cabin, and the air outlet end of the explosion cabin is communicated with the air inlet mechanism through the explosion cabin pressure release control electromagnetic valve and the air loop control electromagnetic valve;
the gas outlet end of the optical gas analysis system is also communicated with a gas storage mechanism, and the gas outlet end of the explosion cabin pressure relief control electromagnetic valve is also communicated with a tail gas treatment mechanism.
Preferably, the air inlet mechanism comprises a large-flow sampling pump communicated with the air inlet end of the electronic pressure control valve, the air inlet end of the large-flow sampling pump is communicated with a sample inlet control ball valve, and the air inlet end of the sample inlet control ball valve is communicated with a gas sample inlet; the air inlet end of the large-flow sampling pump is also communicated with the air outlet end of the gas loop control electromagnetic valve.
Preferably, the ignition assembly comprises an ignition rod and a high-energy igniter, the ignition rod is fixedly arranged on the bulkhead of the explosion cabin, the working end of the ignition rod penetrates through the bulkhead of the explosion cabin from outside to inside, and the high-energy igniter is electrically connected with the ignition rod through a wire.
Preferably, the gas storage mechanism comprises a gas storage tank control ball valve communicated with the gas outlet end of the optical gas analysis system, and the output end of the gas storage tank control ball valve is communicated with a gas storage tank.
Preferably, the tail gas treatment mechanism comprises a tail gas treatment control ball valve communicated with the air outlet end of the explosion cabin pressure relief control electromagnetic valve, and the air outlet end of the tail gas treatment control ball valve is communicated with a tail gas treatment device.
Preferably, the inner cavity of the explosion cabin is also communicated with a pressure reducing mechanism, the pressure reducing mechanism comprises a rotary vane vacuum pump, and the air inlet end of the rotary vane vacuum pump is communicated with the inner cavity of the explosion cabin through a vacuum degree control electromagnetic valve.
The utility model discloses the following technical effects:
1. the utility model can detect the components and the content of the combustible gas, can detect the content of nitrogen and oxygen in the gas mixture, can perform preliminary judgment on the explosion risk of the mixed gas, and then performs ignition experiment on the mixture of the combustible gas and air according to the preliminary judgment result to determine the actual explosion limit of the combustible gas; after the ignition experiment is finished, the product can ignite residual gas in the cabin to perform component detection, analyze the oxygen consumption of the explosion, calculate the heat released by the explosion based on the oxygen consumption principle, and realize comprehensive evaluation of the explosion characteristics of the combustible gas.
2. According to the utility model, explosion characteristic test and gas detection are combined, so that the explosion characteristic can be effectively and quickly judged preliminarily, meanwhile, the preliminary judgment content can be verified through an actual experiment, and meanwhile, the quantitative calculation of explosion power is realized.
3. Most of the operations of the utility model realize automatic processing, the main content of the experiment can be completed according to the computer instruction, and the experimental flow can be customized according to the requirement.
4. The utility model can test different gas components according to the requirement, and can upgrade the capacity in the later period.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions of the prior art, the drawings that are needed in the embodiments will be briefly described below, it being obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.
FIG. 1 is a schematic diagram of the overall system of the present utility model.
Wherein:
1. a gas inlet; 2. a sample inlet control ball valve; 3. a large flow sampling pump; 4. an electronic pressure control valve; 5. an optical gas analysis system; 6. a computer; 7. a gas storage tank control ball valve; 8. a gas storage tank; 9. an explosion sample injection control electromagnetic valve; 10. a vacuum degree control solenoid valve; 11. an explosion chamber; 12. an ignition rod; 13. a high energy igniter; 14. a pressure sensor; 15. decompression control electromagnetic valve of explosion cabin; 16. tail gas treatment control ball valve; 17. a tail gas treatment device; 18. a rotary vane vacuum pump; 19. the gas circuit controls the solenoid valve.
Detailed Description
The following description of the embodiments of the present utility model will be made clearly and completely with reference to the accompanying drawings, in which it is apparent that the embodiments described are only some embodiments of the present utility model, but not all embodiments. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model.
In order that the above-recited objects, features and advantages of the present utility model will become more readily apparent, a more particular description of the utility model will be rendered by reference to the appended drawings and appended detailed description.
Referring to fig. 1, a device for rapidly analyzing gas components and explosion characteristics comprises a gas inlet mechanism, wherein a gas outlet end of the gas inlet mechanism is communicated with a gas analysis mechanism, the gas analysis mechanism is communicated with a gas outlet end of the gas analysis mechanism, and a gas outlet end of the experiment mechanism is communicated with the gas inlet mechanism;
the gas analysis mechanism comprises an electronic pressure control valve 4 communicated with the gas outlet end of the gas inlet mechanism, the gas outlet end of the electronic pressure control valve 4 is communicated with an optical gas analysis system 5, and the gas outlet end of the optical gas analysis system 5 is communicated with the experimental mechanism through an explosion sample injection control electromagnetic valve 9;
the experimental mechanism comprises an explosion cabin 11 communicated with an explosion sample injection control electromagnetic valve 9, an ignition assembly and a pressure sensor 14 are fixedly arranged on the bulkhead of the explosion cabin 11, and the air outlet end of the explosion cabin 11 is communicated with the air inlet mechanism through an explosion cabin pressure relief control electromagnetic valve 15 and an air loop control electromagnetic valve 19;
the air outlet end of the optical gas analysis system 5 is also communicated with an air storage mechanism, and the air outlet end of the explosion cabin pressure release control electromagnetic valve 15 is also communicated with a tail gas treatment mechanism.
The air inlet mechanism can enable external combustible gas to enter the device; the air inlet end of the electronic pressure control valve 4 is communicated with the air inlet mechanism, the air outlet end of the electronic pressure control valve 4 is communicated with the air inlet end of the optical gas analysis system 5, the electronic pressure control valve 4 is used for stabilizing the gas pressure in a gas pipeline, and the pressure sensor 14 is in threaded connection with the bulkhead of the explosion cabin 11 and is communicated with the inner cavity of the explosion cabin 11, so as to monitor the pressure in the explosion cabin 11 in real time; the gas storage mechanism can temporarily store the gas to be detected; the tail gas treatment mechanism can treat and then discharge the gas after the experiment is finished; the combustible gas enters the device through the gas inlet mechanism, enters the explosion cabin 11 after being analyzed by the optical gas analysis system 5, the ignition component detonates the combustible gas in the explosion cabin 11, and the detonated gas sequentially passes through the explosion cabin pressure release control electromagnetic valve 15 and the gas loop control electromagnetic valve 19 and then returns to the gas inlet mechanism again and is then sent into the optical gas analysis system 5 again for gas component analysis, so that the rapid detection of gas components and the quantitative analysis of gas explosion characteristics are realized.
The optical gas analysis system 5 can be used for measuring components of the combustible gas or the combustible liquid vapor mixture to be measured, and is provided with more than 5 special models for characteristic gases, so that the modeling of the characteristic gases, the expanded detection of hydrocarbon and non-hydrocarbon gases, the secondary calibration and the expanded gas modeling function are supported; the connecting pipelines among all the components in the device and the explosion cabin 11 are made of 304 stainless steel, and can bear high temperature and high pressure generated by the gas to be tested or the gas explosion.
In a further optimization scheme, the air inlet mechanism comprises a large-flow sampling pump 3 communicated with the air inlet end of an electronic pressure control valve 4, the air inlet end of the large-flow sampling pump 3 is communicated with a sample inlet control ball valve 2, and the air inlet end of the sample inlet control ball valve 2 is communicated with a gas sample inlet 1; the air inlet end of the large-flow sampling pump 3 is also communicated with the air outlet end of the air loop control electromagnetic valve 19.
The external combustible gas can enter from the gas sample inlet 1 and then sequentially passes through the sample inlet control ball valve 2 and the large-flow sampling pump 3; the gas injection time can be manually controlled by the injection port control ball valve 2; if the quantity of the gas to be detected is small, the gas pressure is low, the large-flow sampling pump 3 can be started to assist in sample injection and improve the pressure and flow of the gas pipeline.
In a further optimized scheme, the ignition assembly comprises an ignition rod 12 and a high-energy igniter 13, wherein the ignition rod 12 is fixedly arranged on the bulkhead of the explosion cabin 11, the working end of the ignition rod 12 penetrates through the bulkhead of the explosion cabin 11 from outside to inside, and the high-energy igniter 13 is electrically connected with the ignition rod 12 through a wire.
The ignition rod 12 is screw-mounted on the bulkhead of the explosion chamber 11, and the high-energy igniter 13 can supply power to the ignition rod 12 to ignite the ignition rod 12, thereby igniting the combustible gas in the explosion chamber 11.
Further optimizing scheme, gas storage mechanism includes the gas holder control ball valve 7 with the end intercommunication of giving vent to anger of optical gas analysis system 5, and the output of gas holder control ball valve 7 communicates there is gas holder 8.
The air storage tank control ball valve 7 can be controlled manually, and the air storage tank 8 is made of 304 stainless steel and is used for storing experimental gas.
Further optimizing scheme, tail gas treatment mechanism includes the tail gas treatment control ball valve 16 with explosion cabin pressure release control solenoid valve 15's the end intercommunication of giving vent to anger, and the end intercommunication has tail gas treatment device 17 of tail gas treatment control ball valve 16.
When the experiment is completed, the tail gas treatment control ball valve 16 is opened, the experiment gas enters the tail gas treatment device 17, and the air is discharged after the experiment is completed.
In a further optimized scheme, the inner cavity of the explosion cabin 11 is also communicated with a pressure reducing mechanism, the pressure reducing mechanism comprises a rotary vane vacuum pump 18, and the air inlet end of the rotary vane vacuum pump 18 is communicated with the inner cavity of the explosion cabin 11 through a vacuum degree control electromagnetic valve 10.
When the internal pressure of the explosion cabin 11 needs to be reduced, the vacuum control electromagnetic valve 10 is opened, the rotary vane vacuum pump 18 is opened, and when the internal pressure of the explosion cabin 11 reaches a preset value, the vacuum control electromagnetic valve 10 is automatically closed, and the rotary vane vacuum pump 18 is automatically closed.
The optical gas analysis system 5, the explosion sample injection control electromagnetic valve 9, the vacuum degree control electromagnetic valve 10 and the explosion cabin pressure relief control electromagnetic valve 15 are electrically connected with a computer 6 which is uniformly and externally controlled by the computer 6.
The following steps are required when the utility model is used:
1) And (3) introducing combustible gas: the sample inlet control ball valve 2 is manually opened, external combustible gas can enter the system from the gas sample inlet 1, and the large-flow sampling pump 3 can be used for auxiliary sample injection;
2) Analyzing the gas composition: the optical gas analysis system 5 can perform component measurement on the combustible gas or the combustible liquid vapor mixture to be measured;
3) Detonating gas: introducing combustible gas into the explosion cabin 11, and electrifying the ignition rod 12 to detonate the combustible gas;
4) Re-analysis of gas composition: introducing the detonated combustible gas into the optical gas analysis system 5 again for gas component measurement, calculating oxygen content change values in the explosion cabin before and after the explosion and calculating heat generation quantity according to an oxygen consumption principle;
5) Exhaust gas: after the experiment is finished, the tail gas treatment control ball valve 16 is opened, the experiment gas enters the tail gas treatment device 17, and air is discharged after the experiment is finished.
The combustible gas or the combustible liquid steam mixture to be measured enters a gas product through a gas sample inlet 1;
the gas injection time can be manually controlled by the injection port control ball valve 2;
if the quantity of the gas to be detected is small, the gas pressure is low, a large-flow sampling pump 3 can be used for auxiliary sample injection, and the pressure and flow of a gas pipeline are improved;
the electronic pressure control valve 4 is used for stabilizing the gas pressure in the gas pipeline;
the optical gas analysis system 5 can be used for measuring components of the combustible gas or the combustible liquid vapor mixture to be measured, and is provided with more than 5 special models for characteristic gases, supports the modeling of the characteristic gases, supports the expanded detection of hydrocarbon and non-hydrocarbon gases, supports the secondary calibration and supports the modeling function of the expanded gases.
The computer 6 is connected with the optical gas analysis system 5, can realize online continuous sampling, converts spectrum information into gas concentration data, automatically calculates the explosion limit value of the combustible gas according to the Le Chatelier principle and displays the explosion limit value in a display screen.
The gas storage tank control ball valve 7 is used for manually controlling whether gas to be detected needs to be temporarily stored in the gas storage tank 8 according to the situation, the volume of the gas storage tank 8 is 20L, and the gas storage tank is made of 304 stainless steel.
The explosion sample injection control electromagnetic valve 9 is linked with the computer 6, the switch action is carried out according to the computer instruction, when the gas to be detected needs to be introduced into the explosion cabin 11, the explosion sample injection control electromagnetic valve 9 is opened, and after sample injection is completed, the explosion sample injection control electromagnetic valve 9 is automatically closed.
The explosion chamber 11 has a volume of 5L and is made of 304 stainless steel. An ignition rod 12 is screwed onto the explosion chamber and connected to a high-energy igniter 13, and a pressure sensor 14 is screwed onto the explosion chamber for monitoring the pressure change in the explosion chamber in real time.
The vacuum control electromagnetic valve 10 is linked with the computer 6, and is switched according to the computer instruction, when the internal pressure of the explosion cabin 11 needs to be reduced, the vacuum control electromagnetic valve 10 is opened, the rotary vane vacuum pump 18 is opened, and when the internal pressure of the explosion cabin 11 reaches the preset value, the vacuum control electromagnetic valve 10 is automatically closed, and the rotary vane vacuum pump 18 is automatically closed.
After the explosion experiment is completed, the explosion cabin pressure relief control electromagnetic valve 15 is opened according to the instruction of the computer 6, the gas loop control electromagnetic valve 19 is opened, the gas after the explosion enters the optical gas analysis system 5 again through the gas loop control electromagnetic valve 19 for gas component measurement, the measurement result is displayed on the computer 6, and the computer 6 can automatically calculate the oxygen content change value in the explosion cabin before and after the explosion and calculate the heat generation amount according to the oxygen consumption principle.
When all experiments are completed, the tail gas treatment control ball valve 16 is opened, the experimental gas enters the tail gas treatment device 17, and air is discharged after the treatment is completed.
The gas pipelines, the explosion cabin 11 and the gas storage tank 8 in the product are all made of 304 stainless steel, and are all provided with heating devices, and the heating temperature is more than or equal to 150 ℃.
The materials of the pressure parts of the gas pipeline, the explosion experiment cabin, the gas tank and the like in the product are 304 stainless steel, and the product can bear high temperature and high pressure generated by the gas to be detected or the gas explosion.
The gas pipeline in this product, explosion experiment cabin, the equal area pressure position all is provided with heating device, can avoid some flammable liquid steam at the inside condensation of product, heating device temperature regulation scope: room temperature to 200 ℃.
The gas pipeline is provided with a pressure regulating valve, and the internal pressure of the gas pipeline is controlled to be constant.
Glass windows with antireflection films are used at two ends of the gas tank, so that the permeability of laser is ensured.
The gas detection function of the product is realized by a gas Raman spectrum testing system, and the Raman spectrum gas detection type: h2, CO2, hydrocarbon gases (including but not limited to CH4, C2H6, C3H 6), N2, O2, and common flammable liquid vapors. The gas qualitative accuracy is higher than 95%.
Gas sampling time: the sampling interval is less than or equal to 5s; the rapid sampling mode is supported, and the sampling time is less than or equal to 1s; continuous sampling: the continuous sampling time is more than or equal to 2 hours; the continuous working time is more than or equal to 24 hours; the detection performance is as follows: the precision is less than or equal to 2 percent, the repeatability is less than or equal to 1 percent, and the zero drift is less than or equal to 2 percent/h;
degree of automation of gas detection: the method can realize online continuous sampling, can convert spectral information into gas concentration data in real time, automatically calculate the explosion limit value of the combustible gas according to the Le Chatelier principle and display the explosion limit value in a display screen. After the ignition test is finished, the oxygen amount change before and after ignition can be measured, and the heat generated by explosion can be calculated according to the oxygen consumption principle;
gas detection data output format: supporting various output formats such as excel, mat, accdb and the like; the detection result, record and database information can be saved;
the ratio of the combustible gas and the air in the explosion cabin is determined by the explosion limit calculated by the gas detection system, the electromagnetic valve is controlled by the singlechip in the product, and the electromagnetic valve switch is controlled according to the calculated explosion limit or the manually input explosion limit to realize sample injection. An automatic/manual dual-mode adjusting system is carried, and the measuring precision reaches +/-0.01%.
Spectrometer performance: CCD wavelength range: 150-3200cm < -1 >, and the CCD refrigerating temperature is less than or equal to 15 ℃ and the spectral resolution is less than or equal to 15 ℃: better than 11cm-1, signal to noise ratio: 10000:1 or more, the effective dynamic range 60000 or more, have laser power self calibration function. Integration time: 20ms-60s. Support SMA fiber interface. The total power of the laser is more than or equal to 400mw, the dynamic adjustment of the power is supported, and the laser power feedback function is realized. The spectrometer has a mounting size of not more than 60cm×44cm×24.5cm
The gas detection system supports a database of common hydrocarbon and non-hydrocarbon characteristics. The characteristic spectrum can be identified to be not less than 20. The software is provided with more than 5 special models for characteristic gases, supports the modeling of the characteristic gases and supports the expanded detection of hydrocarbon and non-hydrocarbon gases; the secondary calibration is supported, and the expanding gas modeling function is supported;
the sample to be tested can be linked with other gas detection devices before and after the test to realize gas component detection, a gas storage cabin is provided to realize short-time gas storage, and the maximum adjustable temperature of the gas storage cabin is 200 ℃.
The instantaneous temperature resistance of the ignition end of the high-energy igniter in the explosion cabin is not lower than 1200 ℃, the ignition frequency is between 6 and 12 times per second, the spark energy is not less than 15J, the thread and the length of the ignition rod are customized according to the size of the explosion cabin, a protection element is contained in the ignition device, and the ignition is automatically stopped when the ignition time is not less than 8 s.
The explosion chamber and the gas storage chamber should be equipped with an air purge system.
The product is loaded with NI labview upper computer software, so that the real-time monitoring, display and data storage of data such as temperature, cavity pressure, oxygen concentration and the like and test flow are realized, report and report output can be carried out on test process data, and the data can be stored in a file format form such as Excel, word, PDF and the like, so that the data is convenient to check and edit. The data recording interval should be less than or equal to 50ms.
The product is provided with a tail gas treatment system, and can adsorb toxic gases and tiny particles generated by explosion.
In the description of the present utility model, it should be understood that the terms "longitudinal," "transverse," "upper," "lower," "front," "rear," "left," "right," "vertical," "horizontal," "top," "bottom," "inner," "outer," and the like indicate or are based on the orientation or positional relationship shown in the drawings, merely to facilitate description of the present utility model, and do not indicate or imply that the devices or elements referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus should not be construed as limiting the present utility model.
The above embodiments are only illustrative of the preferred embodiments of the present utility model and are not intended to limit the scope of the present utility model, and various modifications and improvements made by those skilled in the art to the technical solutions of the present utility model should fall within the protection scope defined by the claims of the present utility model without departing from the design spirit of the present utility model.
Claims (6)
1. An apparatus for rapid analysis of gas composition and explosion characteristics, comprising: the gas outlet end of the gas inlet mechanism is communicated with the gas analysis mechanism, the gas outlet end of the gas analysis mechanism is communicated with the experiment mechanism, and the gas outlet end of the experiment mechanism is communicated with the gas inlet mechanism;
the gas analysis mechanism comprises an electronic pressure control valve (4) communicated with the gas outlet end of the gas inlet mechanism, the gas outlet end of the electronic pressure control valve (4) is communicated with an optical gas analysis system (5), and the gas outlet end of the optical gas analysis system (5) is communicated with the experimental mechanism through an explosion sample injection control electromagnetic valve (9);
the experimental mechanism comprises an explosion cabin (11) communicated with the explosion sample injection control electromagnetic valve (9), an ignition assembly and a pressure sensor (14) are fixedly arranged on the bulkhead of the explosion cabin (11), and the air outlet end of the explosion cabin (11) is communicated with the air inlet mechanism through an explosion cabin pressure release control electromagnetic valve (15) and a gas loop control electromagnetic valve (19);
the gas outlet end of the optical gas analysis system (5) is also communicated with a gas storage mechanism, and the gas outlet end of the explosion cabin pressure relief control electromagnetic valve (15) is also communicated with a tail gas treatment mechanism.
2. The apparatus for rapid analysis of gas composition and explosion characteristics according to claim 1, wherein: the air inlet mechanism comprises a large-flow sampling pump (3) communicated with the air inlet end of the electronic pressure control valve (4), the air inlet end of the large-flow sampling pump (3) is communicated with a sample inlet control ball valve (2), and the air inlet end of the sample inlet control ball valve (2) is communicated with a gas sample inlet (1); the air inlet end of the large-flow sampling pump (3) is also communicated with the air outlet end of the air loop control electromagnetic valve (19).
3. The apparatus for rapid analysis of gas composition and explosion characteristics according to claim 1, wherein: the ignition assembly comprises an ignition rod (12) and a high-energy igniter (13), wherein the ignition rod (12) is fixedly installed on a bulkhead of the explosion cabin (11), a working end of the ignition rod (12) penetrates through the bulkhead of the explosion cabin (11) from outside to inside, and the high-energy igniter (13) is electrically connected with the ignition rod (12) through a wire.
4. The apparatus for rapid analysis of gas composition and explosion characteristics according to claim 1, wherein: the gas storage mechanism comprises a gas storage tank control ball valve (7) communicated with the gas outlet end of the optical gas analysis system (5), and the output end of the gas storage tank control ball valve (7) is communicated with a gas storage tank (8).
5. The apparatus for rapid analysis of gas composition and explosion characteristics according to claim 1, wherein: the tail gas treatment mechanism comprises a tail gas treatment control ball valve (16) communicated with the air outlet end of the explosion cabin pressure relief control electromagnetic valve (15), and the air outlet end of the tail gas treatment control ball valve (16) is communicated with a tail gas treatment device (17).
6. The apparatus for rapid analysis of gas composition and explosion characteristics according to claim 1, wherein: the inner cavity of the explosion cabin (11) is also communicated with a pressure reducing mechanism, the pressure reducing mechanism comprises a rotary vane vacuum pump (18), and the air inlet end of the rotary vane vacuum pump (18) is communicated with the inner cavity of the explosion cabin (11) through a vacuum degree control electromagnetic valve (10).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN202320390316.0U CN219871124U (en) | 2023-03-06 | 2023-03-06 | Device for rapidly analyzing gas components and explosion characteristics |
Applications Claiming Priority (1)
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CN202320390316.0U CN219871124U (en) | 2023-03-06 | 2023-03-06 | Device for rapidly analyzing gas components and explosion characteristics |
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CN219871124U true CN219871124U (en) | 2023-10-20 |
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CN202320390316.0U Active CN219871124U (en) | 2023-03-06 | 2023-03-06 | Device for rapidly analyzing gas components and explosion characteristics |
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2023
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