WO2014079056A1 - Cavity flow meter - Google Patents

Cavity flow meter Download PDF

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Publication number
WO2014079056A1
WO2014079056A1 PCT/CN2012/085255 CN2012085255W WO2014079056A1 WO 2014079056 A1 WO2014079056 A1 WO 2014079056A1 CN 2012085255 W CN2012085255 W CN 2012085255W WO 2014079056 A1 WO2014079056 A1 WO 2014079056A1
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WIPO (PCT)
Prior art keywords
flow
cavity
hole
fluid
measurement
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PCT/CN2012/085255
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French (fr)
Chinese (zh)
Inventor
路明
Original Assignee
Lu Ming
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Priority to PCT/CN2012/085255 priority Critical patent/WO2014079056A1/en
Publication of WO2014079056A1 publication Critical patent/WO2014079056A1/en

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01FMEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
    • G01F1/00Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
    • G01F1/05Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects
    • G01F1/20Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects by detection of dynamic effects of the flow
    • G01F1/32Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow by using mechanical effects by detection of dynamic effects of the flow using swirl flowmeters
    • G01F1/325Means for detecting quantities used as proxy variables for swirl
    • G01F1/3259Means for detecting quantities used as proxy variables for swirl for detecting fluid pressure oscillations

Definitions

  • the invention relates to the field of fluid measurement, and is a device for measuring fluid flow, in particular to utilize hole flow.
  • the flow meter is a meter that indicates the total amount of fluid being measured flowing over a selected time interval. It can be used to measure the flow of fluid in pipes and open channels.
  • flow meters In the fields of metallurgy, electric power, coal, chemical, petroleum, transportation, construction, textile, food, medicine, agriculture, environmental protection, etc., there are a wide variety of flow meters. To date, there are as many as 60 types of flow meters available for industrial use. In the field of fluid flow measurement technology, the most widely used flowmeters are mostly differential pressure flowmeters, such as orifice flowmeters, nozzle flowmeters, venturi flowmeters, and the like. In addition, turbine flow meters and vortex flow meters are also used. Flow meters of the above type are simple in construction and low in cost, but face an intractable problem in measurement.
  • the fluid to be tested often contains more impurities or corrosive components, it may have corrosion or wear on the components of the flowmeter, or blockages may occur at the time, resulting in high maintenance cost and excessive measurement error. Even the measurement failed.
  • the current industrial field requires a flow meter that is simple in structure, accurate, and capable of eliminating the above drawbacks.
  • Cavity Flow is a common fluid flow phenomenon in engineering. For example, the flow in the gap between the train cars, the flow in the aircraft landing gear bay, and the like. Hole flow has always been a research hotspot in the field of fluid mechanics. Because there is a measurable, use-valued movement mechanism in this flow phenomenon.
  • Figure 1 shows a theoretical schematic of the internal mechanism of a hole flow. As shown in Figure 1, when the fluid flows (1) through the cavity (2), at the leading edge (3) of the hole, that is, at the corner, this is theoretically a flow singularity, so the fluid The rate of change of pressure in the direction perpendicular to the flow direction (1) in the viscous boundary layer of (1) suddenly becomes large, thereby causing flow separation at the leading edge (3).
  • a shear layer (4) of fluid moving downstream is formed at the leading edge.
  • the shear layer (4) collides with the trailing edge of the hole (5), is reflected back to the leading edge (3) in the hole (2), and forms a reflection opposite to the incoming stream (1) in the hole (2) Come back to the flow (6).
  • the reflected flow (6) to the leading edge (3) forms a further disturbance to the fluid at the leading edge (3), and the continuous incoming flow (1) continues to separate at the leading edge, forming a shear layer (4).
  • This process continues with the flow of the fluid, so that in the cavity (2), a swirling flow is generated, and the pressure field in the cavity (2) changes periodically, so that the hole flows to form a Self-sustained osci l lation in a cavity 0
  • This self-sustained oscillation is mainly related to the geometry of the holes and the Reynolds number of the incoming flow.
  • a dimensionless number, Reynolds number is used, which describes the ratio of the inertial force to the viscous force of the fluid.
  • the Reynolds number Tfe of the compressible fluid can be expressed by the following formula.
  • a ⁇ represents the density, velocity, and dynamic viscosity coefficient of the fluid flow, respectively;
  • represents the characteristic length dimension of the object, and in the hole flow, it can be represented by the length of the hole opening in FIG.
  • V ⁇ where f is the frequency at which the vortex falls off.
  • the Strouhal number is generally a fixed value of 0.2.
  • An object of the present invention is to provide a cavity flowmeter that operates using the principle of hole flow, which is a flowmeter made by the principle of a self-sustained oscillation phenomenon generated when a fluid flows through a cavity on a wall surface of a flowmeter.
  • FIG. 2 is a schematic structural view of a hole flow meter proposed by the present invention.
  • the cavity flowmeter includes a flow conduit (8) with a front flange (7) and a rear flange (9).
  • the hole (2) for measurement on the wall of the flow pipe (8), and the hole (2) has a sharp leading edge (3) and a trailing edge (5).
  • the measuring hole (2) is equipped with a pressure sensor (12) at the bottom and connected to the measuring circuit (13).
  • the Reynolds number calculator (10) is installed on the wall of the flow pipe (8) and transmitted to the measuring circuit (13) through the data line (11).
  • the fluid enters the flow conduit (8).
  • the measurement circuit (13) is started, the transient pressure signal in the pressure sensor (12) is read. Since at this time, the self-sustained oscillation in the hole (2) has been formed, it is inevitable that a vortex flow pattern like (6) in Fig. 1 is generated in the hole (2).
  • Measuring circuit (13) obtains pressure within a certain sampling time The transient signal then decomposes the frequency of this vortex. Methods for decomposing frequency signals from time domain signals are well known and will not be described here.
  • the flow velocity ⁇ can be obtained according to the formula (2).
  • the Reynolds number of the fluid is calculated according to the formula (1) by the Reynolds number calculator (10) installed on the circulation pipe (8), and The data line (11) is sent to the measuring circuit (13). According to the foregoing theory, if the calculated Reynolds number is in the range of 2 ⁇ 10 4 to 7 ⁇ 10 5 , the measurement is effective, and the flow value of the steady flow in the pipeline is obtained; otherwise, the warning that the measurement range is exceeded is proposed.
  • Figure 1 is a theoretical schematic of the internal mechanism of hole flow. In the figure, 1 fluid flows, 2 holes, 3 front edges, 4 shear layers, 5 trailing edges, and 6 reflected back flows (vortexes).
  • 2 is a schematic structural view of a hole flow meter.
  • 1 fluid flows 2 holes, 3 front edges, 5 trailing edges, 7 connected front flanges, 8 flow pipes, 9 connected rear flanges, 10 Reynolds number calculator, 11 data lines, 12 pressure sensors, 13 Connect to the measurement circuit.
  • the cavimeter flowmeter includes a flow conduit (8) having a front flange (7) connected thereto and a rear flange (9) connected between the tubes to be measured.
  • a cavity (2) on the bottom edge of the circulation pipe (8) the opening length L is 50 mm, and the cross-sectional shape along the depth direction (the direction perpendicular to the incoming flow) is rectangular, thus having a sharp leading edge (3) and rear.
  • a pressure sensor (12) is attached to the bottom and connected to the measuring circuit (13).
  • a Reynolds number calculator (10) is mounted on the wall of the flow conduit (8) upstream of the cavity (2) along the flow direction (1) and transmitted to the measurement circuit (13) via the data line (11).
  • the device is used to measure a steady flow in the pipe, ie the incoming flow rate is constant.
  • the front flange (7) of the device Connect the rear flange (9) between the pipes to be measured.
  • the pressure sensor (12) for measuring the vortex frequency is connected to the measuring circuit (13), and the transient signal of the pressure is obtained within 10 seconds of the sampling time by the sampling frequency of 1 KHZ, and then the frequency of the vortex is decomposed by the FFT method.
  • formula (2) /, Z and the available flow velocity ⁇ are known .
  • the Reynolds number calculator (10) can calculate the Reynolds number of the fluid flow (1) according to the formula (1) and transmit it through the data line (11). To the measurement circuit (13).
  • the measuring circuit (13) proposes a warning that the measuring range is exceeded.
  • the flow rate can be obtained by multiplying the flow velocity in the future by the cross-sectional area of the pipe.
  • the flow value can be converted to a standard current signal output.

Abstract

A cavity flow meter, comprising a circulation pipe (8) provided with a front connecting flange (7) and a back connecting flange (9) thereon; a measurement cavity (2) is disposed on the wall surface of the circulation pipe (8); the cavity (2) has a sharp leading edge (3) and a trailing edge (5); a pressure sensor (12) is installed at the bottom of the measurement cavity (2) and is connected to a measurement circuit (13); a Reynolds number counter (10) is installed on the wall surface of the circulation pipe (8) at the upstream of the cavity (2) in the flow direction (1), and transmits data to the measurement circuit (13) via a data wire (11). When fluid flows by the cavity on the wall surface of the pipe of the flow meter, the fluid generates self-sustained oscillation; the vortex frequency is in proportion to the incoming flow speed, therefore the flow value can be obtained by measuring pressure oscillation frequency.

Description

一种空穴流量计  Cavity flowmeter
技术领域 Technical field
本发明涉及流体测量领域, 是一种测量流体流量的装置, 具体是一种利用空穴流动的  The invention relates to the field of fluid measurement, and is a device for measuring fluid flow, in particular to utilize hole flow.
背景技术 Background technique
流量计是指示被测流体在选定的时间间隔内流动总量的仪表。 可以用于测量管 道、 明渠中流体流量的测量。 在冶金、 电力、 煤炭、 化工、 石油、 交通、 建筑、 轻纺、 食品、 医药、 农业、 环境保护等各个领域, 流量计种类繁多。 至今为止, 可供工业用 的流量仪表种类达 60种之多。在流体流量测量技术领域, 目前使用最广泛的流量计大多 是差压式流量计, 如孔板流量计, 喷嘴流量计, 文丘里管流量计等。 此外, 涡轮流量计、 涡街流量计也有使用。 上述类型的流量计结构简单、 使用成本较低, 但是在测量中面临一 个难以解决的问题。  The flow meter is a meter that indicates the total amount of fluid being measured flowing over a selected time interval. It can be used to measure the flow of fluid in pipes and open channels. In the fields of metallurgy, electric power, coal, chemical, petroleum, transportation, construction, textile, food, medicine, agriculture, environmental protection, etc., there are a wide variety of flow meters. To date, there are as many as 60 types of flow meters available for industrial use. In the field of fluid flow measurement technology, the most widely used flowmeters are mostly differential pressure flowmeters, such as orifice flowmeters, nozzle flowmeters, venturi flowmeters, and the like. In addition, turbine flow meters and vortex flow meters are also used. Flow meters of the above type are simple in construction and low in cost, but face an intractable problem in measurement.
由于被测流体经常往往含有较多杂质,或者有腐蚀性成分,对流量计的零部件有腐蚀、 磨损的影响, 或是时有发生堵塞现象, 造成流量计维护成本高、 测量误差过大, 甚至测量 失败。 总之, 目前工业领域需要一种结构简单、 准确、 同时能过排除上述弊端的流量计。  Since the fluid to be tested often contains more impurities or corrosive components, it may have corrosion or wear on the components of the flowmeter, or blockages may occur at the time, resulting in high maintenance cost and excessive measurement error. Even the measurement failed. In short, the current industrial field requires a flow meter that is simple in structure, accurate, and capable of eliminating the above drawbacks.
空穴流动 (Cavity Flow) 是工程上一种常见的流体流动现象。 例如, 火车车厢之间 的缝隙中的流动、 飞机起落架舱中的流动等等。 空穴流动一直是流体力学领域一个研究热 点。 因为在这种流动现象存在一种可探明的、 用利用价值的运动机制。 图 1给出了一个空 穴流动的内部机制的理论示意图。 如图 1所示, 当流体来流 (1 ) 流过空穴 (2 ) 时, 在空 穴的前沿 (3), 也就是拐角处, 理论上这是一个流动奇点 (singularity), 所以流体 (1 ) 的粘性边界层中沿着与流动方向 (1 ) 垂直的方向上的压力变化率会突然变大, 从而在前 沿 (3 ) 产生流动分离。 由于流体产生分离, 会在前沿开始形成一个向下游运动的流体的 剪切层 (4)。 剪切层 (4) 碰撞到空穴的后沿 (5), 在空穴 (2 ) 中被反射回前沿 (3), 在 空穴 (2 ) 中形成一个与来流 (1 ) 相反的反射回来的流动 (6 )。 反射回来的流动 (6 ) 到 了前沿 (3 ) 形成了对前沿 (3 ) 处的流体的进一步扰动, 持续的来流 (1 ) 在前沿继续分 离, 形成剪切层 (4)。 这个过程随着流体的流动而持续着, 因而在空穴 (2 ) 中, 产生了 一个旋涡形的流动, 空穴 (2 ) 内的压力场呈周期性振荡的变化, 因而空穴流动形成一种 在空穴内的自持振荡 ( self-sustained osci l lation) 0 这个自持振荡主要与空穴的几何形状、 来流的雷诺数 (Reynolds number) 有关。 描述流体 (如空气、 水等) 的运动时, 经常用到无量纲数, 雷诺数, 它描述了流体的 惯性力和粘性力之比。 可压缩流体的雷诺数 Tfe可以用下式来表示, Cavity Flow is a common fluid flow phenomenon in engineering. For example, the flow in the gap between the train cars, the flow in the aircraft landing gear bay, and the like. Hole flow has always been a research hotspot in the field of fluid mechanics. Because there is a measurable, use-valued movement mechanism in this flow phenomenon. Figure 1 shows a theoretical schematic of the internal mechanism of a hole flow. As shown in Figure 1, when the fluid flows (1) through the cavity (2), at the leading edge (3) of the hole, that is, at the corner, this is theoretically a flow singularity, so the fluid The rate of change of pressure in the direction perpendicular to the flow direction (1) in the viscous boundary layer of (1) suddenly becomes large, thereby causing flow separation at the leading edge (3). Due to the separation of the fluid, a shear layer (4) of fluid moving downstream is formed at the leading edge. The shear layer (4) collides with the trailing edge of the hole (5), is reflected back to the leading edge (3) in the hole (2), and forms a reflection opposite to the incoming stream (1) in the hole (2) Come back to the flow (6). The reflected flow (6) to the leading edge (3) forms a further disturbance to the fluid at the leading edge (3), and the continuous incoming flow (1) continues to separate at the leading edge, forming a shear layer (4). This process continues with the flow of the fluid, so that in the cavity (2), a swirling flow is generated, and the pressure field in the cavity (2) changes periodically, so that the hole flows to form a Self-sustained osci l lation in a cavity 0 This self-sustained oscillation is mainly related to the geometry of the holes and the Reynolds number of the incoming flow. When describing the motion of a fluid (such as air, water, etc.), a dimensionless number, Reynolds number, is used, which describes the ratio of the inertial force to the viscous force of the fluid. The Reynolds number Tfe of the compressible fluid can be expressed by the following formula.
Re = Re =
^ (1) 其中, A , 分别代表流体来流的密度、 速度和动力粘性系数; Ζ代表物体的特征长度尺 度, 在空穴流动中, 可以用图 1中的空穴开口的长度表示。 大量实验表明, 雷诺数在 2χ104至 7χ105范围内, 空穴流动中的旋涡的结构是稳定的, 而且旋涡产生频率和流体来流的流速的关系是唯一确定的。 在诸如空穴流动这样的振荡的 流场中常用到无量纲参数,斯特哈雷数(Strouhal number)数来描述流场的特征。 Strouhal 数, S 定义为 ^ (1) where A represents the density, velocity, and dynamic viscosity coefficient of the fluid flow, respectively; Ζ represents the characteristic length dimension of the object, and in the hole flow, it can be represented by the length of the hole opening in FIG. A large number of experiments have shown that the Reynolds number is in the range of 2χ10 4 to 7χ10 5 , the structure of the vortex in the hole flow is stable, and the relationship between the vortex generation frequency and the flow rate of the fluid flow is uniquely determined. In the oscillating flow field such as hole flow, a dimensionless parameter is often used, and the Strouhal number is used to describe the characteristics of the flow field. Strouhal number, S is defined as
St = ^- (2)St = ^- (2)
V 其中, f 为旋涡的脱落频率。 在上述雷诺数范围内, Strouhal 数一般为固定值 0.2。 因 而在空穴流动中, 如果获得旋涡的脱落频率 /, 即可获得流体来流的流速。 V where f is the frequency at which the vortex falls off. In the above Reynolds number range, the Strouhal number is generally a fixed value of 0.2. Thus, in the flow of holes, if the frequency of shedding of the vortex is obtained, the flow rate of the fluid can be obtained.
发明内容 Summary of the invention
本发明的目的是提供一种利用空穴流动原理工作的空穴流量计, 它是利用流体流过流 量计管道壁面上的空穴时产生的自持振荡现象的原理制成的流量计。  SUMMARY OF THE INVENTION An object of the present invention is to provide a cavity flowmeter that operates using the principle of hole flow, which is a flowmeter made by the principle of a self-sustained oscillation phenomenon generated when a fluid flows through a cavity on a wall surface of a flowmeter.
根据上述理论, 可以设计一种利用空穴流动原理工作的、 用于测量管道内稳定流动的 流量的空穴流量计。 图 2是本发明提出的一种空穴流量计的结构示意图。 图中表示, 该空 穴流量计包括一个流通管道 (8), 其上有连接前法兰 (7)、 连接后法兰 (9)。 在流通管道 (8) 壁面上有一测量用的空穴 (2), 空穴 (2) 有尖锐的前沿 (3) 和后沿 (5)。 测量空 穴 (2) 底部装有压力传感器 (12), 连接到测量电路 (13)。 沿着流动方向 (1), 在空穴 (2) 的上游, 在流通管道 (8) 壁面上安装雷诺数计算器 (10), 并通过数据线 (11) 传 送至测量电路 (13)。  According to the above theory, a hole flow meter for measuring the flow rate of steady flow in a pipe which works by the principle of hole flow can be designed. 2 is a schematic structural view of a hole flow meter proposed by the present invention. The figure shows that the cavity flowmeter includes a flow conduit (8) with a front flange (7) and a rear flange (9). There is a hole (2) for measurement on the wall of the flow pipe (8), and the hole (2) has a sharp leading edge (3) and a trailing edge (5). The measuring hole (2) is equipped with a pressure sensor (12) at the bottom and connected to the measuring circuit (13). In the flow direction (1), upstream of the cavity (2), the Reynolds number calculator (10) is installed on the wall of the flow pipe (8) and transmitted to the measuring circuit (13) through the data line (11).
流量计工作时,流体进入流通管道(8)。启动测量电路(13)后,读取压力传感器(12) 中的瞬态压力信号。 因为此时, 空穴 (2) 中的自持振荡已经形成, 势必在空穴 (2) 中产 生和图 1 中的 (6) —样的旋涡流动模式。 测量电路 (13) 在一定的采样时间内获得压力 的瞬态信号, 然后分解出这个旋涡的频率。 从时域信号分解出频率信号的方法是公知的, 这里不再叙述。 When the flow meter is working, the fluid enters the flow conduit (8). After the measurement circuit (13) is started, the transient pressure signal in the pressure sensor (12) is read. Since at this time, the self-sustained oscillation in the hole (2) has been formed, it is inevitable that a vortex flow pattern like (6) in Fig. 1 is generated in the hole (2). Measuring circuit (13) obtains pressure within a certain sampling time The transient signal then decomposes the frequency of this vortex. Methods for decomposing frequency signals from time domain signals are well known and will not be described here.
因为旋涡频率与来流速度成比例、 Strouhal 数是以固定值 0. 2, 且空穴 (2 ) 的开口 长度 Z是已知的, 所以按照公式(2), 即可获得来流速度 。此时, 因为流体来流的密度、 速度和动力粘性系数均为已知, 由安装在流通管道 (8 ) 上的雷诺数计算器 (10 ) 按照公 式 (1 ) 计算流体的雷诺数, 并通过数据线 (11 ) 传送至测量电路 (13)。 按照前述理论, 如果计算的雷诺数在 2X104至 7χ105范围内, 则测量有效, 得到管道内稳定流动的流量值; 否则, 提出测量范围超出的警示。 Since the vortex frequency is proportional to the incoming flow velocity, the Strouhal number is a fixed value of 0.2, and the opening length Z of the cavity (2) is known, the flow velocity can be obtained according to the formula (2). At this time, since the density, velocity and dynamic viscosity coefficient of the fluid flow are known, the Reynolds number of the fluid is calculated according to the formula (1) by the Reynolds number calculator (10) installed on the circulation pipe (8), and The data line (11) is sent to the measuring circuit (13). According to the foregoing theory, if the calculated Reynolds number is in the range of 2 × 10 4 to 7χ10 5 , the measurement is effective, and the flow value of the steady flow in the pipeline is obtained; otherwise, the warning that the measurement range is exceeded is proposed.
由于本发明提出的空穴流量计的流量测量在空穴中进行, 整个仪表内部无阻碍流体流 动的部件, 所以压力损失非常微小, 而且结构上更加牢固可靠, 不怕腐蚀、 磨损、 堵塞等 问题, 拆装方便、 结构简单、 实用。  Since the flow measurement of the hole flowmeter proposed by the present invention is carried out in the cavity, there is no component inside the meter that hinders the flow of the fluid, so the pressure loss is very small, and the structure is more firm and reliable, and is not afraid of corrosion, wear, blockage, etc. Easy to assemble and disassemble, simple and practical.
附图说明 DRAWINGS
图 1是空穴流动的内部机制的理论示意图。 图中, 1流体来流、 2空穴、 3前沿、 4剪 切层、 5后沿、 6反射回来的流动 (旋涡)。  Figure 1 is a theoretical schematic of the internal mechanism of hole flow. In the figure, 1 fluid flows, 2 holes, 3 front edges, 4 shear layers, 5 trailing edges, and 6 reflected back flows (vortexes).
图 2是一种空穴流量计的结构示意图。 图中, 1流体来流、 2空穴、 3前沿、 5后沿、 7连接前法兰、 8流通管道、 9连接后法兰、 10雷诺数计算器、 11数据线、 12压力传感器、 13连接到测量电路。  2 is a schematic structural view of a hole flow meter. In the figure, 1 fluid flows, 2 holes, 3 front edges, 5 trailing edges, 7 connected front flanges, 8 flow pipes, 9 connected rear flanges, 10 Reynolds number calculator, 11 data lines, 12 pressure sensors, 13 Connect to the measurement circuit.
具体实施方式 detailed description
以下以一个具体实施方式进一步说明本发明提出的一种空穴流量计的原理和结构。 具 体实施方式的结构示意图如图 2所示。 空穴流量计包括一个流通管道 (8), 其上有连接前 法兰 (7)、 连接后法兰 (9), 可以连接在欲测量的管道之间。 在流通管道 (8 ) 底边上有 一空穴(2), 开口长度 L为 50mm、沿着纵深方向(与来流垂直的方向)的剖面形状为矩形, 因而具有尖锐的前沿(3 )和后沿(5), 底部装有压力传感器(12), 连接到测量电路(13)。 沿着流动方向 (1 ), 在空穴(2 )的上游, 在流通管道(8 )壁面上安装雷诺数计算器(10), 并通过数据线 (11 ) 传送至测量电路 (13)。  The principle and structure of a hole flow meter proposed by the present invention will be further described below in a specific embodiment. A schematic structural view of a specific embodiment is shown in Fig. 2. The cavimeter flowmeter includes a flow conduit (8) having a front flange (7) connected thereto and a rear flange (9) connected between the tubes to be measured. There is a cavity (2) on the bottom edge of the circulation pipe (8), the opening length L is 50 mm, and the cross-sectional shape along the depth direction (the direction perpendicular to the incoming flow) is rectangular, thus having a sharp leading edge (3) and rear. Along the (5), a pressure sensor (12) is attached to the bottom and connected to the measuring circuit (13). A Reynolds number calculator (10) is mounted on the wall of the flow conduit (8) upstream of the cavity (2) along the flow direction (1) and transmitted to the measurement circuit (13) via the data line (11).
该装置用于测量管道内的稳定流动, 即来流速度是恒定的。 将该装置的前法兰 (7)、 连接后法兰 (9) 连接到欲测量的管道之间。 测量时, 来流流过空穴 (2) 时, 流体边界层 在空穴的前沿 (3) 产生流动分离, 分离的剪切层碰撞到空穴的后沿 (5), 在空穴 (2) 中 被反射回前沿 (3), 形成了对前沿的流体的扰动, 流体来流 (1 ) 在此处继续分离。 这个 过程随着流体的流动而持续着, 因而在空穴 (2) 中, 产生旋涡, 使得空穴 (2) 压力的周 期性振荡。 测量旋涡频率的压力传感器 (12) 连接到测量电路 (13), 通过 1KHZ的采样频 率,在采样时间 10秒内获得压力的瞬态信号,然后通过 FFT方法分解出这个旋涡的频率 /。 按照公式 (2), 已知 /、 Z和 可获得来流速度 。 此时, 因为来流的密度和动力粘性 系数均为已知, 所以雷诺数计算器(10)可以按照公式(1 )计算流体来流(1 ) 的雷诺数, 并通过数据线 (11 ) 传送至测量电路 (13 )。 按照前述理论, 如果计算的雷诺数在 2X104 至 7χ105范围内, 则测量有效, 得到管道内稳定流动的流量值; 否则, 测量电路 (13) 提 出测量范围超出的警示。 The device is used to measure a steady flow in the pipe, ie the incoming flow rate is constant. The front flange (7) of the device, Connect the rear flange (9) between the pipes to be measured. When measuring, when the flow flows through the hole (2), the fluid boundary layer generates flow separation at the leading edge of the hole (3), and the separated shear layer collides with the trailing edge of the hole (5), in the cavity (2) The middle is reflected back to the leading edge (3), creating a disturbance to the fluid at the leading edge, where the fluid flow (1) continues to separate. This process continues as the fluid flows, so that in the cavity (2), a vortex is generated, causing periodic oscillation of the hole (2) pressure. The pressure sensor (12) for measuring the vortex frequency is connected to the measuring circuit (13), and the transient signal of the pressure is obtained within 10 seconds of the sampling time by the sampling frequency of 1 KHZ, and then the frequency of the vortex is decomposed by the FFT method. According to formula (2), /, Z and the available flow velocity ∞ are known . At this time, since the density of the incoming flow and the dynamic viscosity coefficient are both known, the Reynolds number calculator (10) can calculate the Reynolds number of the fluid flow (1) according to the formula (1) and transmit it through the data line (11). To the measurement circuit (13). According to the foregoing theory, if the calculated Reynolds number is in the range of 2 × 10 4 to 7χ10 5 , the measurement is effective, and the flow value of the steady flow in the pipe is obtained; otherwise, the measuring circuit (13) proposes a warning that the measuring range is exceeded.
对于有效测量, 将来流速度乘以管道截面积即可获得来流的流量, 可将流量值转换成 标准电流信号输出。  For effective measurements, the flow rate can be obtained by multiplying the flow velocity in the future by the cross-sectional area of the pipe. The flow value can be converted to a standard current signal output.
附图标号列表 List of reference numerals
1流体来流  1 fluid flow
2空穴 2 holes
3前沿 3 frontiers
4剪切层 4 shear layer
5后沿 5 trailing edge
6反射回来的流动 (旋涡)  6 reflected back flow (vortex)
7连接前法兰  7 connection front flange
8流通管道  8 circulation pipeline
9连接后法兰  9 connected rear flange
10雷诺数计算器  10 Reynolds number calculator
11数据线  11 data lines
12压力传感器  12 pressure sensor
13测量电路。  13 measurement circuit.

Claims

权 利 要 求 书 Claim
1. 一种空穴流量计, 其特征在于: 它包括连个流通管道(8), 其上有连接前法兰(7)、 连接 后法兰(9); 在流通管道(8)壁面上有一测量用的空穴(2), 空穴(2)有尖锐的前沿(3) 和后沿 (5 ); 测量空穴 (2) 底部装有压力传感器 (12 ), 连接到测量电路 (13); 沿着流 动方向 (1 ), 在空穴 (2) 的上游, 在流通管道 (8) 壁面上安装雷诺数计算器 (10), 并 通过数据线 (11 ) 传送至测量电路 (13)。 A cavity flow meter characterized in that it comprises a continuous flow conduit (8) having a front flange (7) connected thereto and a rear flange (9) connected thereto; on the wall of the flow conduit (8) There is a hole (2) for measurement, the hole (2) has a sharp leading edge (3) and a trailing edge (5); the bottom of the measuring hole (2) is equipped with a pressure sensor (12) connected to the measuring circuit (13) In the flow direction (1), upstream of the cavity (2), the Reynolds number calculator (10) is installed on the wall of the circulation pipe (8), and is transmitted to the measuring circuit (13) through the data line (11). .
2. 根据权利要求 1所述的空穴流量计, 其特征在于: 所说的空穴 (2) 沿着与来流垂直的方 向的剖面形状为矩形。 The hole flowmeter according to claim 1, wherein the hole (2) has a rectangular cross-sectional shape in a direction perpendicular to the incoming flow.
PCT/CN2012/085255 2012-11-26 2012-11-26 Cavity flow meter WO2014079056A1 (en)

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3035223A1 (en) * 2015-04-17 2016-10-21 Polyvionics ROBUST DEVICE FOR MEASURING THE SPEED OF DISPLACING A FLUID IN RELATION TO AN OBJECT

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Publication number Priority date Publication date Assignee Title
CN1035559A (en) * 1987-12-04 1989-09-13 施鲁博格工业公司 Vortex flowmeter transducer
CN1425901A (en) * 2003-01-15 2003-06-25 中国计量学院 Integrated intelligent cavity flow meter
CN2593158Y (en) * 2003-01-15 2003-12-17 中国计量学院 Cavity flow sensor
CN2935095Y (en) * 2006-06-30 2007-08-15 上海创杰工程自动化有限公司 Wedge-type flowmeter
CN202171476U (en) * 2011-05-26 2012-03-21 天津空中代码工程应用软件开发有限公司 Cavitation flow meter
CN102384774A (en) * 2010-09-03 2012-03-21 日立汽车系统株式会社 Thermal air flow sensor

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN1035559A (en) * 1987-12-04 1989-09-13 施鲁博格工业公司 Vortex flowmeter transducer
CN1425901A (en) * 2003-01-15 2003-06-25 中国计量学院 Integrated intelligent cavity flow meter
CN2593158Y (en) * 2003-01-15 2003-12-17 中国计量学院 Cavity flow sensor
CN2935095Y (en) * 2006-06-30 2007-08-15 上海创杰工程自动化有限公司 Wedge-type flowmeter
CN102384774A (en) * 2010-09-03 2012-03-21 日立汽车系统株式会社 Thermal air flow sensor
CN202171476U (en) * 2011-05-26 2012-03-21 天津空中代码工程应用软件开发有限公司 Cavitation flow meter

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3035223A1 (en) * 2015-04-17 2016-10-21 Polyvionics ROBUST DEVICE FOR MEASURING THE SPEED OF DISPLACING A FLUID IN RELATION TO AN OBJECT

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