CN102735587A - Jet flow density measurement device and method - Google Patents
Jet flow density measurement device and method Download PDFInfo
- Publication number
- CN102735587A CN102735587A CN2012102343651A CN201210234365A CN102735587A CN 102735587 A CN102735587 A CN 102735587A CN 2012102343651 A CN2012102343651 A CN 2012102343651A CN 201210234365 A CN201210234365 A CN 201210234365A CN 102735587 A CN102735587 A CN 102735587A
- Authority
- CN
- China
- Prior art keywords
- jet
- differential pressure
- outlet
- pressure
- density
- 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
- Measuring Volume Flow (AREA)
Abstract
本发明公开了一种射流密度测量装置及方法。包括流动入口、入口接头、盖板、射流振荡元件、动态差压高压取压管、射流喷嘴、射流附壁、射流反馈回路、动态差压低压取压管、出口接头、流动出口;射流振荡元件所在平面与流动入口和出口相垂直;通过动态差压传感器测量出两个取压管之间的动态差压,再通过线路输入到二次仪表进行密度计量。本发明中,当流体经入口进入射流振荡元件之后,由于流体的康达效应和反馈回路,诱使腔体振荡;由动态差压传感器测量的差压为振荡的脉动差压,差压的振荡频率与射流喷嘴的工况流速成正比,差压的平均值与射流喷嘴处流体的动压头成正比,那么,动压头与流速平方之比与介质的密度成正比。本发明的优势是可以实现流动介质低雷诺数下的密度测量。
The invention discloses a jet density measuring device and method. Including flow inlet, inlet joint, cover plate, jet oscillating element, dynamic differential pressure high pressure tube, jet nozzle, jet wall, jet feedback loop, dynamic differential pressure low pressure tube, outlet joint, flow outlet; jet oscillating element The plane where it is located is perpendicular to the flow inlet and outlet; the dynamic differential pressure between the two pressure-taking pipes is measured by the dynamic differential pressure sensor, and then input to the secondary instrument through the line for density measurement. In the present invention, after the fluid enters the jet oscillating element through the inlet, the cavity is induced to oscillate due to the Coanda effect and the feedback loop of the fluid; the differential pressure measured by the dynamic differential pressure sensor is an oscillating pulsating differential pressure, and the oscillation of the differential pressure The frequency is proportional to the flow rate of the jet nozzle, and the average value of the differential pressure is proportional to the dynamic pressure head of the fluid at the jet nozzle. Then, the ratio of the dynamic pressure head to the square of the flow velocity is proportional to the density of the medium. The invention has the advantage that it can realize the density measurement of the flowing medium at a low Reynolds number.
Description
技术领域 technical field
本发明涉及一种密度测量设备,特别是涉及一种可应用于流动的气体或液体密度测量的射流密测量装置及方法,属于流体测量技术领域。 The invention relates to a density measuring device, in particular to a jet density measuring device and method applicable to the density measurement of flowing gas or liquid, and belongs to the technical field of fluid measurement.
背景技术 Background technique
密度计广泛应用于石油、天然气测量以及化工和印刷等行业;目前已有的密度计有科里奥利流量密度计、压差密度计、放射密度计、振荡管密度计等;科里奥利流量密度计的精度较高但价格昂贵,且对介质清洁度要求较高;压差密度计较多的应用在石油密度测量中,可用于液体测量却无法进行气体密度测量;放射密度测量因为存在有放射源,存在一定的安全隐患;振荡管密度计需要柱体的自激卡门涡街振荡,而卡门涡街振荡有雷诺数下限,即当流速低于某雷诺数以后,不会产生卡门涡街,则密度也无法测量。 Density meters are widely used in petroleum, natural gas measurement, chemical and printing industries; the existing densitometers include Coriolis flow densitometers, differential pressure densitometers, radioactive densitometers, oscillating tube densitometers, etc.; The flow density meter has high accuracy but is expensive, and has high requirements on the cleanliness of the medium; the differential pressure density meter is mostly used in oil density measurement, which can be used for liquid measurement but cannot be used for gas density measurement; There are certain potential safety hazards for radioactive sources; the oscillating tube density meter requires self-excited Karman vortex oscillation of the cylinder, and Karman vortex oscillation has a lower limit of Reynolds number, that is, when the flow rate is lower than a certain Reynolds number, Karman vortex street will not be generated , the density cannot be measured.
发明内容 Contents of the invention
本发明所要解决的的技术问题在于克服现有密度测量方法的不足,提供一种低雷诺数管流射流密度测量方法及测量装置。 The technical problem to be solved by the present invention is to overcome the shortcomings of existing density measurement methods, and provide a low Reynolds number tube flow jet density measurement method and a measurement device.
一种射流密度测量装置,其特征在于:包括盖板和射流振荡元件;上述射流振荡元件从前至后依次包括入口流道、射流喷嘴、中间流道、出口流道,其中射流出口和射流喷嘴之间还具有两路射流反馈回路;上述中间流道从前至后为渐扩形式;上述盖板安装于射流振荡元件上部,盖板上安装有与上述入口流道相通的入口接头,和与上述出口流道相通的出口接头;入口接头和出口接头用于连接所需测量的介质管道;上述盖板还安装有伸入射流喷嘴内的动态差压传感器高压取压管和伸入射流出口内的动态差压传感器低压取压管。 A jet density measuring device, characterized in that it includes a cover plate and a jet oscillating element; the jet oscillating element includes an inlet channel, a jet nozzle, an intermediate channel, and an outlet channel from front to back, wherein the jet outlet and the jet nozzle There are also two jet feedback loops between them; the above-mentioned middle flow channel is in the form of gradual expansion from front to back; the above-mentioned cover plate is installed on the upper part of the jet oscillating element, and the cover plate is installed with an inlet joint connected with the above-mentioned inlet flow channel, and connected with the above-mentioned outlet The outlet joint with the flow channel connected; the inlet joint and the outlet joint are used to connect the medium pipeline to be measured; the above cover plate is also equipped with a dynamic differential pressure sensor high-pressure pressure tube extending into the jet nozzle and a dynamic differential pressure sensor extending into the jet outlet. Differential pressure sensor low pressure pressure tube.
利用权利所述射流密度测量装置的射流密度测量方法,其特征在于包括以下步骤: The jet density measurement method using the jet density measurement device described in the right is characterized in that it comprises the following steps:
步骤A、将所需测量的介质管道连接于入口接头和出口接头之间;使射流通过射流振荡元件,产生振荡射流; Step A, connecting the medium pipeline to be measured between the inlet joint and the outlet joint; allowing the jet to pass through the jet oscillating element to generate an oscillating jet;
步骤B、利用动态差压传感器高压取压管和动态差压传感器低压取压管,测量射流振荡元件的射流喷嘴和射流出口的压差; Step B, using the dynamic differential pressure sensor high pressure pressure tube and the dynamic differential pressure sensor low pressure pressure tube to measure the pressure difference between the jet nozzle and the jet outlet of the jet oscillating element;
步骤C、根据下式计算射流的密度: Step C, calculate the density of the jet according to the following formula:
ρ =K*(DP/f2) , ρ =K*(DP/f 2 ),
式中,ρ表示射流的密度;DP表示射流振荡元件的射流喷嘴、射流出口的压差平均值;f表示射流的振荡频率;K为比例系数,对于特定的射流振荡元件,其为定值,根据实验预先标定得到;所述射流的振荡频率f通过以下方法得到:动态记录下差压传感器随时间的变化数值,应用快速傅里叶变换把时域信号转化成频域信号,得到振荡频率。 In the formula, ρ represents the density of the jet; DP represents the average pressure difference between the jet nozzle and the jet outlet of the jet oscillating element; f represents the oscillation frequency of the jet; K is the proportional coefficient, which is a fixed value for a specific jet oscillating element, It is pre-calibrated according to the experiment; the oscillation frequency f of the jet is obtained by the following method: dynamically record the change value of the differential pressure sensor over time, apply fast Fourier transform to convert the time domain signal into a frequency domain signal, and obtain the oscillation frequency.
所述射流的振荡频率通过以下方法得到:动态记录下差压传感器随时间的变化数值,应用快速傅里叶变换把时域信号转化成频域信号,得到振荡频率(参考何振亚著,数字信号处理的理论与应用,北京:人民邮电出版社,北京,1983)。利用已测量得到的射流喷嘴和射流出口的压差,通过计算得到射流的振荡频率,不需要设置单独的振荡频率测量部件,简化了结构,降低了成本。 The oscillation frequency of the jet is obtained by the following method: dynamically record the value of the differential pressure sensor over time, apply fast Fourier transform to convert the time domain signal into a frequency domain signal, and obtain the oscillation frequency (refer to He Zhenya, digital signal processing Theory and Application, Beijing: People's Posts and Telecommunications Press, Beijing, 1983). By using the measured pressure difference between the jet nozzle and the jet outlet, the oscillation frequency of the jet is obtained through calculation, without setting a separate oscillation frequency measurement component, which simplifies the structure and reduces the cost.
本发明涉及到的射流密度计可以大大的降低测量雷诺数的下限,结构简单,成本低廉。由流体介质流过射流振荡元件(参考蔡武昌,应启戛著,新型流量检测仪表,北京:化学工业出版社,北京,2006),在射流入口和出口之间形成振荡的差压信号,通过采集一路动态差压信号即可以进行流动介质的密度测量。相比现有技术,本发明可以实现液体和气体的流体密度测量,液体和气体的测量比例系数K一致,且本发明的可测雷诺数下限较低,测量装置结构简单,成本较低。 The jet density meter involved in the invention can greatly reduce the lower limit of the measured Reynolds number, has simple structure and low cost. The fluid medium flows through the jet oscillating element (refer to Cai Wuchang, Ying Qijia, New Flow Measuring Instrument, Beijing: Chemical Industry Press, Beijing, 2006), and an oscillating differential pressure signal is formed between the jet inlet and outlet, through The density measurement of the flowing medium can be carried out by collecting a dynamic differential pressure signal. Compared with the prior art, the present invention can realize fluid density measurement of liquid and gas, the measurement proportional coefficient K of liquid and gas is consistent, and the lower limit of the measurable Reynolds number of the present invention is lower, the measuring device has simple structure and low cost.
附图说明 Description of drawings
图1为本发明的结构示意图;图2为射流振荡元件4的俯视图。
FIG. 1 is a schematic structural diagram of the present invention; FIG. 2 is a top view of the
各标号的含义如下:1流动入口、2入口接头、3盖板、4射流振荡元件、5动态差压高压取压管、6射流喷嘴、7射流附壁、8射流反馈回路、9动态差压低压取压管、10出口接头、11流动出口、12入口流道、13中间流道、14出口流道,15射流出口。 The meanings of each label are as follows: 1 flow inlet, 2 inlet joint, 3 cover plate, 4 jet oscillating element, 5 dynamic differential pressure high pressure pressure tube, 6 jet nozzle, 7 jet attached wall, 8 jet feedback loop, 9 dynamic differential pressure Low pressure pressure pipe, 10 outlet joint, 11 flow outlet, 12 inlet channel, 13 intermediate channel, 14 outlet channel, 15 jet outlet.
具体实施方式 Detailed ways
下面结合附图对本发明的技术方案进行详细说明: The technical scheme of the present invention is described in detail below in conjunction with accompanying drawing:
本发明的射流密度测量装置的一个实施例如图1所示,它包括:流动入口1、入口接头2、盖板3、射流振荡元件4、动态差压高压取压管5、射流喷嘴6、射流附壁7、射流反馈回路8、动态差压低压取压管9、出口接头10、流动出口11、入口流道12、中间流道13、出口流道14,射流出口15,其中射流振荡元件4包括射流喷嘴6、射流附壁7、射流反馈回路8、动态差压低压取压管9、出口接头10、流动出口11、入口流道12、中间流道13、出口流道14,射流出口15。入口接头2的上端口为流动入口1,可通过软管连接所需要测量的流体管道,入口接头2的下端与盖板3通过螺纹紧固连接,出口接头10的下端也与盖板3 螺纹紧固连接,出口接头10的上端为流动出口,可通过软管连接连回所需要测量的介质管道;盖板3盖在射流振荡元件4之上并通过螺栓与之固连;射流振荡元件4的射流喷嘴6处设置有动态差压高压取压管5,射流振荡元件4的射流出口15处设置有动态差压低压取压管9。
An embodiment of the jet density measuring device of the present invention is shown in Fig. 1, and it comprises:
当进行密度测量时,将上述测量装置通过入口接头2用软管与待测流体的流动管路连接,流体从流动入口1进入射流振荡元件4,由于康达效应使射流喷嘴6出来的主体射流偏向射流附壁7的一边,主射流经射流振荡元件4的射流出口15流出,而一小部分射流经同侧的射流反馈回路8返回至射流喷嘴6处,推动主射流偏向另外一侧的附壁,一小部分射流再经另外一侧的射流反馈回路至射流喷嘴6处;如此不断循环,形成腔体振荡。采用动态压差传感器对高压取压管5、低压取压管9之间的差压进行实时测量,并将测量数据依据下式计算并显示输出射流的密度:
When performing density measurement, the above-mentioned measuring device is connected to the flow pipeline of the fluid to be measured with a hose through the inlet joint 2, and the fluid enters the
ρ =K*(DP/f2) , ρ =K*(DP/f 2 ),
式中,ρ表示射流的密度;DP表示压差传感器输出的压差的平均值;f表示射流的振荡频率,通过以下方法得到:动态记录下差压传感器随时间的变化数值,应用快速傅里叶变换把时域信号转化成频域信号,得到振荡频率(参考何振亚著,数字信号处理的理论与应用,北京:人民邮电出版社,北京,1983);K为比例系数,对于特定的射流振荡元件,其为定值,根据实验预先标定得到。 In the formula, ρ represents the density of the jet; DP represents the average value of the pressure difference output by the differential pressure sensor; f represents the oscillation frequency of the jet, which is obtained by the following method: dynamically record the value of the differential pressure sensor over time, and apply fast Fourier Leaf transform converts the time-domain signal into a frequency-domain signal to obtain the oscillation frequency (refer to He Zhenya, Theory and Application of Digital Signal Processing, Beijing: People's Posts and Telecommunications Press, Beijing, 1983); K is the proportional coefficient, for a specific jet oscillation Components, which are fixed values, are pre-calibrated according to experiments.
为使公众便于理解本发明的技术方案,下面对本发明的测量原理进行详细说明: In order to make the public easy to understand the technical solution of the present invention, the measurement principle of the present invention is described in detail below:
经理论研究和实验证明,由射流的康达效应和反馈回路诱使的腔体振荡的频率f与射流喷嘴处的流速v成正比,公式如下: Theoretical studies and experiments have proved that the frequency f of cavity oscillation induced by the Coanda effect of the jet and the feedback loop is proportional to the flow velocity v at the jet nozzle, the formula is as follows:
v = k1* f (1) v = k 1 * f (1)
其中,k1为比例系数;振荡频率f可采用现有的通过在反馈通道或者出入口附近设置热敏、力敏、光纤等检测元件,检测得到射流振荡频率的方法得到,而本发明为了简化结构,利用对动态差压信号做快速傅里叶变换的方法得到,具体为动态记录下差压传感器随时间的变化数值,应用快速傅里叶变换把时域信号转化成频域信号,得到振荡频率(参考何振亚著,数字信号处理的理论与应用,北京:人民邮电出版社,北京,1983)。 Wherein, k 1 is a proportional coefficient; the oscillation frequency f can be obtained by using the existing detection elements such as heat-sensitive, force-sensitive, and optical fibers near the feedback channel or the entrance and exit to detect the jet oscillation frequency, and the present invention is to simplify the structure , using the method of fast Fourier transform on the dynamic differential pressure signal, specifically to dynamically record the change value of the differential pressure sensor over time, apply the fast Fourier transform to convert the time domain signal into a frequency domain signal, and obtain the oscillation frequency (Refer to He Zhenya, Theory and Application of Digital Signal Processing, Beijing: People's Posts and Telecommunications Press, Beijing, 1983).
而动态差压信号的平均值DP与射流喷嘴处的动压头ρv2成正比,公式如下: The average value DP of the dynamic differential pressure signal is proportional to the dynamic pressure head ρv2 at the jet nozzle, and the formula is as follows:
ρv2=k2*DP (2) ρv 2 =k 2 *DP (2)
其中,k2为比例系数;ρ为流体密度; Wherein, k 2 is proportionality coefficient; ρ is fluid density;
由公式(1)和公式(2)可以得到公式(3)如下: Formula (3) can be obtained from formula (1) and formula (2) as follows:
ρ=(k2/k1 2)*(DP/f2) (3) ρ=(k 2 /k 1 2 )*(DP/f 2 ) (3)
流体的密度为ρ,令k2/k1的值为K,则有公式(4): The density of the fluid is ρ, let the value of k 2 /k 1 be K, then there is formula (4):
ρ=K*(DP/f2) (4) ρ=K*(DP/f 2 ) (4)
对于特定的射流振荡元件,比例系数K为定值,可根据实验预先标定得到。 For a specific jet oscillating element, the proportional coefficient K is a fixed value, which can be pre-calibrated according to experiments.
Claims (2)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012102343651A CN102735587A (en) | 2012-07-09 | 2012-07-09 | Jet flow density measurement device and method |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN2012102343651A CN102735587A (en) | 2012-07-09 | 2012-07-09 | Jet flow density measurement device and method |
Publications (1)
Publication Number | Publication Date |
---|---|
CN102735587A true CN102735587A (en) | 2012-10-17 |
Family
ID=46991479
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN2012102343651A Pending CN102735587A (en) | 2012-07-09 | 2012-07-09 | Jet flow density measurement device and method |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN102735587A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105403730A (en) * | 2015-11-13 | 2016-03-16 | 武汉大学 | Fluid instantaneous flow velocity measure apparatus and method based on Helmholtz instability |
CN110268257A (en) * | 2016-12-20 | 2019-09-20 | 恩德斯+豪斯流量技术股份有限公司 | Gas analyzer and gas analyzing apparatus |
CN110440410A (en) * | 2019-08-08 | 2019-11-12 | 珠海格力电器股份有限公司 | Protection method of water-cooled air conditioning unit and water-cooled air conditioning unit |
CN113933211A (en) * | 2021-10-14 | 2022-01-14 | 国网安徽省电力有限公司电力科学研究院 | Method and device for measuring gas mixture ratio of ternary mixed gas based on gas substitution method |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1673689A (en) * | 2005-04-22 | 2005-09-28 | 浙江大学 | Pipe wall differential pressure type vortex frequency detecting method and apparatus for vortex street flowmeter |
CN201740553U (en) * | 2010-08-06 | 2011-02-09 | 北京博思达新世纪测控技术有限公司 | Double-parameter mass flow meter |
CN102364308A (en) * | 2011-10-17 | 2012-02-29 | 南京航空航天大学 | Method and device for measuring jet mass flow rate |
-
2012
- 2012-07-09 CN CN2012102343651A patent/CN102735587A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1673689A (en) * | 2005-04-22 | 2005-09-28 | 浙江大学 | Pipe wall differential pressure type vortex frequency detecting method and apparatus for vortex street flowmeter |
CN201740553U (en) * | 2010-08-06 | 2011-02-09 | 北京博思达新世纪测控技术有限公司 | Double-parameter mass flow meter |
CN102364308A (en) * | 2011-10-17 | 2012-02-29 | 南京航空航天大学 | Method and device for measuring jet mass flow rate |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN105403730A (en) * | 2015-11-13 | 2016-03-16 | 武汉大学 | Fluid instantaneous flow velocity measure apparatus and method based on Helmholtz instability |
CN105403730B (en) * | 2015-11-13 | 2018-03-27 | 武汉大学 | Fluid instantaneous velocity measurement apparatus and method based on helmholtz instability |
CN110268257A (en) * | 2016-12-20 | 2019-09-20 | 恩德斯+豪斯流量技术股份有限公司 | Gas analyzer and gas analyzing apparatus |
US11112340B2 (en) | 2016-12-20 | 2021-09-07 | Endress+Hauser Flowtec Ag | Gas analyzer and gas analyzing device |
CN110440410A (en) * | 2019-08-08 | 2019-11-12 | 珠海格力电器股份有限公司 | Protection method of water-cooled air conditioning unit and water-cooled air conditioning unit |
CN113933211A (en) * | 2021-10-14 | 2022-01-14 | 国网安徽省电力有限公司电力科学研究院 | Method and device for measuring gas mixture ratio of ternary mixed gas based on gas substitution method |
CN113933211B (en) * | 2021-10-14 | 2024-03-15 | 国网安徽省电力有限公司电力科学研究院 | Method and device for measuring gas mixture ratio of ternary mixed gas based on gas substitution method |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Venugopal et al. | Review on vortex flowmeter—Designer perspective | |
CN102759383B (en) | Method and device for online measurement of gas-phase flow rate of gas-liquid two-phase flow based on single throttling element | |
RU2013150525A (en) | NUCLEAR MAGNETIC FLOWMETER AND METHOD OF OPERATION OF NUCLEAR MAGNETIC FLOWMETERS | |
WO2009018694A1 (en) | A multiphase flow metering method and a multiphase flow meter using the same | |
CN107843297B (en) | On-line measurement device and method for liquid phase flow rate of gas-liquid two-phase flow with low gas fraction based on V-cone | |
CN106643945B (en) | A kind of homogeneity gas-liquid mixed media mass-flow measurement device and method | |
CN104614029B (en) | A kind of passage aisle biphase gas and liquid flow flow measurement device and method based on PVT methods | |
CN107976222A (en) | A kind of Pitot tube integrated gas mass flow measurement methods | |
CN108680208A (en) | A kind of hot type flux of vortex street metering device, flowmeter and its flow-measuring method | |
CN102735587A (en) | Jet flow density measurement device and method | |
CN202256376U (en) | Combination of constriction section and flow measurement section of medium and low speed wind tunnel | |
CN204705570U (en) | The permeability experimental provision that a kind of automatic pressure detects | |
CN204514402U (en) | A kind of differential pressure mass flowmeter for vortex street | |
CN101393043A (en) | High frequency response flowmeter and measurement method thereof | |
CN101251397A (en) | Bypass in-line flowmeter | |
CN211904339U (en) | On-line detection standard device for small-flow gas flowmeter | |
CN102364308A (en) | Method and device for measuring jet mass flow rate | |
CN101819051B (en) | Vortex street flowmeter probe and vortex street flowmeter using probe | |
CN107255501B (en) | Gas-liquid mixed flow vortex flowmeter calibration detection device system and control method | |
CN204085597U (en) | A kind of Pitot bar mass flowmeter | |
CN215177929U (en) | Vortex street flowmeter | |
CN208847264U (en) | A kind of tandem coriolis mass flowmeters | |
CN209280059U (en) | A kind of ultrasonic type gas-liquid two-phase measuring device | |
CN205679275U (en) | A kind of momentum-type flow sensor | |
CN202350849U (en) | Mass flow measurement device for jet flow |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20121017 |