CN1392391A - Multiple air channel air amount measuring method and device in large air channel - Google Patents
Multiple air channel air amount measuring method and device in large air channel Download PDFInfo
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- CN1392391A CN1392391A CN 02136270 CN02136270A CN1392391A CN 1392391 A CN1392391 A CN 1392391A CN 02136270 CN02136270 CN 02136270 CN 02136270 A CN02136270 A CN 02136270A CN 1392391 A CN1392391 A CN 1392391A
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- 230000003068 static effect Effects 0.000 claims abstract description 5
- 238000005259 measurement Methods 0.000 abstract description 9
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Abstract
The measurement method includes separating large air channel into several parts, measuring the total pressure and static pressure difference of the parts separately with several wind-measuring devices, transferring pressure difference via pressure sensor to signal collector and completing air channel wind amount calculation and display via system unit. The present invention has the advantages of raised measurement precision owing to the grille to commutate; lowered space position precision requirement in wind-measuring device owing to the reduced channel equivalent diameter and size of wine-measuring device; and reduced size of required straight pipe section owing to the reduced channel equivalent diameter.
Description
Technical field
The present invention relates to multiple duct air measuring method and device in a kind of wind trunk.
Background technology
For a long time, the air quantity on-line measurement of large section duct is a difficult problem, air current flow in the wind trunk often is subjected to that air door, runner are turned, shunt and confluxed, the expansion of pipeline section and the influence of external factor such as dwindle, and the wind trunk pipeline is flowed develop into flowing of velocity flow profile complexity.
The influence factor of flow measurement is diversified, and this is because exist: 1, fluidity qualitative diversity, as the difference of fluid viscosity, single-phase and heterogeneous, compressible and incompressible, pressure and the height of density parameter, clean-up performance of fluid or the like; 2, the diversity of piping system, as the circle of pipeline section and non-circle, inwall smooth and coarse, whether crooked, shunt and conflux, the size of flow etc.; 3, the diversity of flow state is as laminar flow and turbulent flow, rotating flow and pulsating flow, mobilely whether reach abundant development etc.Also be subjected to the principle of work of measurement mechanism simultaneously and whether satisfy the influence of its technical stipulation.
At present, the wind measuring device that the wind trunk air measuring mainly adopts has wing, air channel type venturi, flute type pipe and double-venturi etc., and it treats each tool a little.The measuring principle of wind trunk apparatus for measuring air quantity has all been utilized the notion of mean flow rate, if will make output signal can represent corresponding mean flow rate, velocity flow profile in the time of just must guaranteeing to measure reaches relative even flow and distributes, and this is to guarantee to measure necessary condition accurately.Generally all consider, require to have before the measurement mechanism straight length of certain-length by full-blown velocity flow profile.
The measurement requirement of air quantity has the stable or moving phase in flow field seemingly, but the operation adjustment process can not make and flow stablely in the air channel in, also makes also dissmilarity of its velocity flow profile sometimes.Measure accurately, just necessary current stabilization rectification satisfy the requirement of measurement mechanism, but measurement requirement can't be satisfied sometimes in field condition and locus
Summary of the invention
The purpose of this invention is to provide multiple duct air measuring method and device in a kind of wind trunk.
Measuring method is that wind trunk is separated into the n part, utilizes n wind measuring device to measure total head and static pressure difference in each air channel, transmits pressure difference value to signal picker by pressure transducer, is finished the air channel Wind Coverage Calculation and is shown by system host.
Measurement mechanism is to be provided with fairing, wind measuring device, air channel demarcation strip in the air channel successively.
The present invention has the following advantages:
1. install grid before the wind measuring device additional the gas that enters wind measuring device has been carried out rectification, eliminated the eddy current that elbow or air door etc. cause, improved measuring accuracy.
2. separate each little air channel equivalent diameter of back and reduce, the apparatus for measuring air quantity size is corresponding reduces for airfoil type or venturi etc., has reduced the requirement of wind measuring device to the locus.
3. use this technology that the equivalent diameter in branch air channel is reduced, the straight length absolute growth that requires before the wind measuring device reduces that (the short straight tube section size that wind measuring device requires is general and the air channel equivalent diameter is proportional, as having the straight length of 0.6 times of equivalent diameter before the airfoil type apparatus for measuring air quantity claimed apparatus at least), under the comparatively narrow situation in wind trunk locus, satisfied the requirement of wind measuring device to straight length.
4. before satisfying wind measuring device size and device reluctantly during the flow development length requirement, wind trunk is cut apart, and the wind measuring device size reduces on the one hand, and branch air channel equivalent diameter reduces on the other hand, then the flow development length before the wind measuring device increases relatively, and the apparatus for measuring air quantity measuring accuracy improves greatly.
When 5. each minute, air quantity deviation in air channel was big, adopt to each minute the air channel measure air quantity respectively and sue for peace then, reduced the air measuring error.
6. because the resistance coefficient unanimity of the apparatus for measuring air quantity in each air channel, when in each air channel during the wind speed skewness, the branch duct resistance that wind speed is high is big, wind speed is low to divide duct resistance little, the air channel that resistance is big will force the part air-flow to go to the little air channel of resistance to pass through, automatically reach a kind of equilibrium state, therefore wind speed profile is more even behind undue air channel.
Description of drawings
Fig. 1 is the windy measuring device structural representation in the wind trunk;
Fig. 2 is a differential pressure signal output connection synoptic diagram.
Embodiment
It is to transmit pressure difference value to signal picker by pressure transducer to adopt each wind measuring device pressure difference value parallel connection to go out a pressure difference value transmission that large section duct is separated the air measuring method, or adopts each wind measuring device pressure difference value to transmit respectively.
The said system main frame is finished in the branch air channel in the Wind Coverage Calculation of air channel the wind measuring device coefficient of flow and is calculated according to calibration value separately.
It is to be provided with fairing 1, wind measuring device 2, air channel demarcation strip 3 in the air channel successively that large section duct is separated apparatus for measuring air quantity.Fairing is even or non-homogeneous grid.Wind measuring device 2 is airfoil type wind measuring device, venturi wind measuring device, bourdon's tube, double-venturi wind measuring device, Pitot tube, backing tube, Annubar pipe, thermoelectric wind measuring device.Demarcation strip is for being separated into wind trunk on the dividing plate in little air channel.
The present invention is divided into a plurality of relatively stable or similar heavy fields according to the concrete condition that institute's survey wind trunk flows with an instability, dissimilar flow field, carries out air measuring respectively, the foundation and the essence of multiple duct air measuring proposition that Here it is.Though on a certain cross section in air channel, owing to the influence of various factors, the distribution instability of its speed, through adding separator lined for behind several zones, each is distinguished in the city can obtain relatively stable or similar velocity distribution.
And, after the air channel is cut apart, the equivalent diameter in air channel is shortened, prolong the flow development length of wind measuring device position relatively, thereby can reach the purpose of steady flow condition.Simultaneously the length of apparatus for measuring air quantity can shorten greatly, and the space requirement in straight air channel is reduced greatly.As a square air channel, be divided into two and shorten to 75% when two diameters after partly; Four can shorten to 50% after dividing equally.This is when arrangement space is narrow and small at the scene, and seeming is highly profitable.
The present invention is separated into n part (n decides according to field condition and duct dimension) with wind trunk, utilize n wind measuring device to measure total head and static pressure difference in each air channel, be passed to signal picker by pressure transducer, finish the calculating and the demonstration of air channel air quantity by system host.For eliminating the vortex that the air channel inlet may exist, before separating device, installed fairing additional.
Fairing 1 is installed in before the demarcation strip 2, generally adopts flow straightening grid, its objective is to eliminate the eddy current that enters when separating the air channel.Separating the quantity in air channel and the length of demarcation strip is the key parameter of this measuring technique, should decide according to field condition, line size and wind measuring device 3 forms etc.Wind measuring device 3 is installed in respectively to be separated in the air channel, and wind measuring device 3 can adopt the probe of airfoil type, venturi, bourdon's tube or other form, and concrete form is determined according to field position, measuring accuracy, resistance size requirements etc.Flow development length before the wind measuring device 3 should satisfy the requirement of this form sensing device to straight length.
The pressure signal that each wind measuring device 3 comes out is determined output in parallel or output respectively according to the air channel structure position, if each little air duct flow field is similar, flow is more or less the same, and can be connected in parallel to a differential pressure transformer output to total head and static pressure, otherwise should export separately, calculated flow rate is sued for peace then respectively.Output signal connects as shown in Figure 2.Wind Coverage Calculation is as follows.During in parallel output,
In the formula, Q--air channel total blast volume; K--wind measuring device coefficient of flow; A--separates little air channel, back area; Total differential pressure after the Δ p--parallel connection; ρ--gas density; When exporting respectively,
In the formula, Q--air channel total blast volume; The little air channel of n--number; k
i--each wind measuring device coefficient of flow; A
i--separate each little air channel area of back; Δ p
i--each little air channel wind measuring device output differential pressure; Fairing ρ
i--gas density in each little air channel;
Claims (7)
1. a large section duct is separated the air measuring method, it is characterized in that wind trunk is separated into the n part, utilize n wind measuring device to measure total head and static pressure difference in each air channel, transmit pressure difference value to signal picker by pressure transducer, finish air channel Wind Coverage Calculation and demonstration by system host.
2. large section duct according to claim 1 is separated the air measuring method, it is characterized in that saidly transmitting pressure difference value to signal picker by pressure transducer and adopting each wind measuring device pressure difference value parallel connection to go out a pressure difference value to transmit, or adopt each wind measuring device pressure difference value to transmit respectively.
3. large section duct according to claim 1 is separated the air measuring method, it is characterized in that said system host finishes in the branch air channel in the Wind Coverage Calculation of air channel the wind measuring device coefficient of flow and calculate according to calibration value separately.
4. a large section duct is separated apparatus for measuring air quantity, it is characterized in that being provided with successively in the air channel fairing (1), wind measuring device (2), air channel demarcation strip (3).
5. large section duct according to claim 3 is separated apparatus for measuring air quantity, it is characterized in that said fairing is even or non-homogeneous grid.
6. large section duct according to claim 3 is separated apparatus for measuring air quantity, it is characterized in that said wind measuring device (2) is airfoil type wind measuring device, venturi wind measuring device, bourdon's tube, double-venturi wind measuring device, Pitot tube, backing tube, Annubar pipe, thermoelectric wind measuring device.
7. large section duct according to claim 3 is separated apparatus for measuring air quantity, it is characterized in that said demarcation strip is for being separated into wind trunk on the dividing plate in little air channel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02136270 CN1218164C (en) | 2002-07-25 | 2002-07-25 | Multiple air channel air amount measuring method and device in large air channel |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 02136270 CN1218164C (en) | 2002-07-25 | 2002-07-25 | Multiple air channel air amount measuring method and device in large air channel |
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| CN1392391A true CN1392391A (en) | 2003-01-22 |
| CN1218164C CN1218164C (en) | 2005-09-07 |
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| CN 02136270 Expired - Fee Related CN1218164C (en) | 2002-07-25 | 2002-07-25 | Multiple air channel air amount measuring method and device in large air channel |
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Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101865193A (en) * | 2010-07-19 | 2010-10-20 | 中国航空工业集团公司西安飞机设计研究所 | Easy rectification method of irregular air duct flow field |
| CN102680037A (en) * | 2012-06-06 | 2012-09-19 | 上海华东电脑***工程有限公司 | Air quantity differential pressure calibration method applied to liquid cooling type frame |
| CN102116656B (en) * | 2010-01-06 | 2012-10-03 | 华北电力科学研究院有限责任公司 | Method and device for detecting air volume in air passage |
| CN104568027A (en) * | 2015-02-05 | 2015-04-29 | 辽宁毕托巴科技有限公司 | Pitotbar gas flow measuring device |
| CN106525144A (en) * | 2015-09-09 | 2017-03-22 | 山洋电气株式会社 | Measurement device |
| CN106841672A (en) * | 2017-01-20 | 2017-06-13 | 北京博希格动力技术有限公司 | The apparatus and method of the small wing detection boiler secondary point duct velocity of array |
| CN107289170A (en) * | 2016-03-31 | 2017-10-24 | 倚世节能科技（上海）有限公司 | Ventilation valve |
| CN107389133A (en) * | 2017-08-08 | 2017-11-24 | 张晨 | Exhaust measurement, sampling apparatus and methods and applications |
| CN109596307A (en) * | 2018-12-03 | 2019-04-09 | 南京慧和建筑技术有限公司 | A kind of air supply tube resistance measurement equipment |
| CN109738665A (en) * | 2019-01-19 | 2019-05-10 | 重庆芯力源科技有限公司 | A kind of flow velocity method for automatic measurement based on Pitot tube |
| CN110514569A (en) * | 2019-07-08 | 2019-11-29 | 佛山市顺德区阿波罗环保器材有限公司 | The ducting assembly of strainability detection system of fume filtering element |
| CN113203874A (en) * | 2021-03-31 | 2021-08-03 | 华能山东石岛湾核电有限公司 | Supplementary amount of wind cover of ventilation system and wind volume measuring device are piled to high temperature |
| CN114858408A (en) * | 2022-02-25 | 2022-08-05 | 浙江大学 | Test device and test method for testing dynamic oscillation performance of hydrofoil |
| WO2023151565A1 (en) * | 2022-02-09 | 2023-08-17 | 付成 | Modular flow measurement method and apparatus, and application |
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2002
- 2002-07-25 CN CN 02136270 patent/CN1218164C/en not_active Expired - Fee Related
Cited By (18)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102116656B (en) * | 2010-01-06 | 2012-10-03 | 华北电力科学研究院有限责任公司 | Method and device for detecting air volume in air passage |
| CN101865193A (en) * | 2010-07-19 | 2010-10-20 | 中国航空工业集团公司西安飞机设计研究所 | Easy rectification method of irregular air duct flow field |
| CN102680037A (en) * | 2012-06-06 | 2012-09-19 | 上海华东电脑***工程有限公司 | Air quantity differential pressure calibration method applied to liquid cooling type frame |
| CN102680037B (en) * | 2012-06-06 | 2013-10-09 | 上海华东电脑***工程有限公司 | Air quantity differential pressure calibration method applied to liquid cooling type frame |
| CN104568027A (en) * | 2015-02-05 | 2015-04-29 | 辽宁毕托巴科技有限公司 | Pitotbar gas flow measuring device |
| CN106525144B (en) * | 2015-09-09 | 2020-08-04 | 山洋电气株式会社 | Measuring device |
| CN106525144A (en) * | 2015-09-09 | 2017-03-22 | 山洋电气株式会社 | Measurement device |
| CN107289170A (en) * | 2016-03-31 | 2017-10-24 | 倚世节能科技（上海）有限公司 | Ventilation valve |
| CN106841672A (en) * | 2017-01-20 | 2017-06-13 | 北京博希格动力技术有限公司 | The apparatus and method of the small wing detection boiler secondary point duct velocity of array |
| CN106841672B (en) * | 2017-01-20 | 2023-12-29 | 北京博希格动力技术有限公司 | Array winglet detection boiler secondary device and method for dividing wind speed of wind channel |
| CN107389133A (en) * | 2017-08-08 | 2017-11-24 | 张晨 | Exhaust measurement, sampling apparatus and methods and applications |
| CN109596307A (en) * | 2018-12-03 | 2019-04-09 | 南京慧和建筑技术有限公司 | A kind of air supply tube resistance measurement equipment |
| CN109738665A (en) * | 2019-01-19 | 2019-05-10 | 重庆芯力源科技有限公司 | A kind of flow velocity method for automatic measurement based on Pitot tube |
| CN109738665B (en) * | 2019-01-19 | 2020-12-01 | 重庆芯力源科技有限公司 | Pitot tube-based flow velocity automatic measurement method |
| CN110514569A (en) * | 2019-07-08 | 2019-11-29 | 佛山市顺德区阿波罗环保器材有限公司 | The ducting assembly of strainability detection system of fume filtering element |
| CN113203874A (en) * | 2021-03-31 | 2021-08-03 | 华能山东石岛湾核电有限公司 | Supplementary amount of wind cover of ventilation system and wind volume measuring device are piled to high temperature |
| WO2023151565A1 (en) * | 2022-02-09 | 2023-08-17 | 付成 | Modular flow measurement method and apparatus, and application |
| CN114858408A (en) * | 2022-02-25 | 2022-08-05 | 浙江大学 | Test device and test method for testing dynamic oscillation performance of hydrofoil |
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| CN1218164C (en) | 2005-09-07 |
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