CN114777853A - Turbine flowmeter for measuring micro gas flow - Google Patents
Turbine flowmeter for measuring micro gas flow Download PDFInfo
- Publication number
- CN114777853A CN114777853A CN202210396559.5A CN202210396559A CN114777853A CN 114777853 A CN114777853 A CN 114777853A CN 202210396559 A CN202210396559 A CN 202210396559A CN 114777853 A CN114777853 A CN 114777853A
- Authority
- CN
- China
- Prior art keywords
- hole
- stepped
- gas flow
- small
- turbine flowmeter
- 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
- 238000011144 upstream manufacturing Methods 0.000 claims description 14
- 239000007787 solid Substances 0.000 claims 2
- 239000003638 chemical reducing agent Substances 0.000 claims 1
- BGOFCVIGEYGEOF-UJPOAAIJSA-N helicin Chemical compound O[C@@H]1[C@@H](O)[C@H](O)[C@@H](CO)O[C@H]1OC1=CC=CC=C1C=O BGOFCVIGEYGEOF-UJPOAAIJSA-N 0.000 claims 1
- 238000007789 sealing Methods 0.000 claims 1
- 239000007858 starting material Substances 0.000 claims 1
- 238000005259 measurement Methods 0.000 abstract description 11
- 238000001514 detection method Methods 0.000 abstract description 5
- 239000007789 gas Substances 0.000 description 24
- 239000012530 fluid Substances 0.000 description 8
- 238000009987 spinning Methods 0.000 description 7
- 230000007423 decrease Effects 0.000 description 2
- 238000009434 installation Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 description 2
- 239000003034 coal gas Substances 0.000 description 1
- 230000005674 electromagnetic induction Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 230000006698 induction Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000003345 natural gas Substances 0.000 description 1
- 239000003208 petroleum Substances 0.000 description 1
Images
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F1/00—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow
- G01F1/05—Measuring 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
- G01F1/20—Measuring 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
- G01F1/28—Measuring 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 by drag-force, e.g. vane type or impact flowmeter
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F15/00—Details of, or accessories for, apparatus of groups G01F1/00 - G01F13/00 insofar as such details or appliances are not adapted to particular types of such apparatus
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F15/00—Details of, or accessories for, apparatus of groups G01F1/00 - G01F13/00 insofar as such details or appliances are not adapted to particular types of such apparatus
- G01F15/14—Casings, e.g. of special material
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01F—MEASURING VOLUME, VOLUME FLOW, MASS FLOW OR LIQUID LEVEL; METERING BY VOLUME
- G01F15/00—Details of, or accessories for, apparatus of groups G01F1/00 - G01F13/00 insofar as such details or appliances are not adapted to particular types of such apparatus
- G01F15/18—Supports or connecting means for meters
- G01F15/185—Connecting means, e.g. bypass conduits
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Volume Flow (AREA)
Abstract
一种测量微小气体流量的涡轮流量计,包括传感器壳体,所述传感器壳体的上端通过放大器连接转换器,所述传感器壳体的进口端、出口端均设有水平接管,所述传感器壳体内设有一阶梯形通孔,所述阶梯形通孔的进口端、出口端均为大径段,中间为小径段,所述小径段与进口端之间设有一变径段;所述进口端内设置一起旋器,出口端内设置一导流架,所述导流架的一端插入阶梯形通孔的小径段中,一叶轮位于小径段中,所述叶轮的轴的两端分别支承于起旋器、导流架上设置的轴孔中。本发明提供一种测量微小气体流量的涡轮流量计,解决测量微小气体流量时,检测难度大,检测效率低,测量精度底,使用寿命低的问题。
A turbine flowmeter for measuring tiny gas flow, comprising a sensor housing, the upper end of the sensor housing is connected to a converter through an amplifier, the inlet end and the outlet end of the sensor housing are provided with horizontal pipes, and the sensor housing A stepped through hole is arranged in the body, the inlet end and the outlet end of the stepped through hole are large-diameter sections, and the middle is a small-diameter section, and a variable-diameter section is arranged between the small-diameter section and the inlet end; the inlet end A co-rotator is set inside, a guide frame is set in the outlet end, one end of the guide frame is inserted into the small-diameter section of the stepped through hole, an impeller is located in the small-diameter section, and both ends of the shaft of the impeller are respectively supported in the small diameter section. In the shaft hole set on the spinner and the guide frame. The invention provides a turbine flowmeter for measuring micro gas flow, which solves the problems of high detection difficulty, low detection efficiency, low measurement accuracy and low service life when measuring micro gas flow.
Description
技术领域technical field
本发明涉及一种流量测量技术领域,特别涉及一种测量微小气体流量的涡轮流量计。The invention relates to the technical field of flow measurement, in particular to a turbine flowmeter for measuring tiny gas flow.
背景技术Background technique
涡轮流量计是一种速度式流量计,当被测流体流过涡轮流量计传感器时,在流体的作用下,叶轮受力旋转,其转速与管道平均流速成正比,同时,叶片周期性地切割电磁铁产生的磁力线,改变线圈的磁通量,根据电磁感应原理,在线圈内将感应出脉动的电势信号,即电脉冲信号,此电脉冲信号的频率与被测流体的流量成正比。电脉冲信号的频率与被测流体的流量的公式如下:Turbine flowmeter is a kind of velocity flowmeter. When the measured fluid flows through the turbine flowmeter sensor, under the action of the fluid, the impeller is forced to rotate, and its rotational speed is proportional to the average flow velocity of the pipeline. At the same time, the blades are periodically cut. The magnetic field lines generated by the electromagnet change the magnetic flux of the coil. According to the principle of electromagnetic induction, a pulsating potential signal, that is, an electric pulse signal, will be induced in the coil. The frequency of this electric pulse signal is proportional to the flow rate of the fluid being measured. The formula for the frequency of the electrical pulse signal and the flow rate of the fluid to be measured is as follows:
式中,Q为被测流体流量,f为电脉冲信号的频率,K为比例系数。In the formula, Q is the flow rate of the fluid to be measured, f is the frequency of the electrical pulse signal, and K is the proportionality coefficient.
涡轮流量计广泛应用于以下一些测量对象:石油、有机液体、无机液、液化气、天然气、煤气和低温流体等。Turbine flowmeters are widely used in the following measurement objects: petroleum, organic liquids, inorganic liquids, liquefied gas, natural gas, coal gas and cryogenic fluids.
由于涡轮流量计是速度式流量计,在测量微小气体流量时,被测流体流速低使得叶轮旋转速度慢,导致叶片切割磁感线的频率低,使得产生的电脉冲信号无法被检测或检测精度降低,进而使得被测流体流量无法被测量或产生较大的测量误差。当前测量微小气体流量时,通常采用小口径涡轮流量计进行测量,小口径涡轮流量计的零部件体积更小,因此零部件出现磨损时,对测量精度的影响更加巨大,导致测量精度降低。故小口径涡轮流量计使用寿命更低,无法长期准确检测流量。Since the turbine flowmeter is a velocity flowmeter, when measuring the small gas flow, the low flow rate of the measured fluid makes the impeller rotate slowly, resulting in a low frequency of the blades cutting the magnetic field lines, so that the generated electrical pulse signal cannot be detected or detected. decrease, so that the flow rate of the fluid being measured cannot be measured or a larger measurement error occurs. When measuring tiny gas flow, small-diameter turbine flowmeters are usually used for measurement. The components of small-diameter turbine flowmeters are smaller in volume. Therefore, when the components are worn, the impact on measurement accuracy is greater, resulting in reduced measurement accuracy. Therefore, the small-diameter turbine flowmeter has a lower service life and cannot accurately detect the flow rate for a long time.
发明内容SUMMARY OF THE INVENTION
本发明的目的是针对现有技术存在的不足,提供一种测量微小气体流量的涡轮流量计,解决测量微小气体流量时,检测难度大,检测效率低,测量精度底,使用寿命低的问题。The purpose of the present invention is to provide a turbine flowmeter for measuring tiny gas flow, which solves the problems of high detection difficulty, low detection efficiency, low measurement accuracy and low service life when measuring tiny gas flow.
本发明的目的是这样实现的:The object of the present invention is achieved in this way:
一种测量微小气体流量的涡轮流量计,包括传感器壳体,所述传感器壳体的上端通过放大器连接转换器,所述传感器壳体的进口端、出口端均设有水平接管,所述传感器壳体内设有一阶梯形通孔,所述阶梯形通孔的进口端、出口端均为大径段,中间为小径段,所述小径段与进口端之间设有一变径段;所述进口端内设置一起旋器,出口端内设置一导流架,所述导流架的一端插入阶梯形通孔的小径段中,一叶轮位于小径段中,所述叶轮的轴的两端分别支承于起旋器、导流架上设置的轴孔中;所述进口端水平接管的孔径与阶梯形通孔的大径段相同,所述出口端水平接管的管孔为阶梯孔,该阶梯孔上游为小径端,该小径端的孔径小于传感器壳体的阶梯形通孔的小径段孔径,该阶梯孔下游的大径端孔径与进口端水平接管的孔径相同。A turbine flowmeter for measuring tiny gas flow, comprising a sensor housing, the upper end of the sensor housing is connected to a converter through an amplifier, the inlet end and the outlet end of the sensor housing are provided with horizontal pipes, and the sensor housing A stepped through hole is arranged in the body, the inlet end and the outlet end of the stepped through hole are large diameter sections, the middle is a small diameter section, and a variable diameter section is arranged between the small diameter section and the inlet end; the inlet end A co-rotator is set inside, a guide frame is set at the outlet end, one end of the guide frame is inserted into the small diameter section of the stepped through hole, an impeller is located in the small diameter section, and the two ends of the shaft of the impeller are respectively supported in the small diameter section. In the shaft hole provided on the spinner and the guide frame; the diameter of the horizontal nozzle at the inlet end is the same as the large diameter section of the stepped through hole, the pipe hole of the horizontal nozzle at the outlet end is a stepped hole, and the upstream of the stepped hole is the small diameter end, the diameter of the small diameter end is smaller than the diameter of the small diameter section of the stepped through hole of the sensor housing, and the diameter of the large diameter end downstream of the stepped hole is the same as the diameter of the horizontal nozzle of the inlet end.
所述叶轮的轴的两端均通过止推轴承和滑动轴承分别支承于起旋器、导流架上的轴孔中。Both ends of the shaft of the impeller are respectively supported in the shaft holes on the spinner and the guide frame through a thrust bearing and a sliding bearing.
所述起旋器上设有多个绕轴心呈螺旋状的起旋叶片,相邻两个起旋叶片之间形成流道,起旋器的一端设有固定环,固定环与起旋叶片固定连接,起旋器通过固定环与传感器壳体固定连接,起旋器的另一端设置用于安装轴承的轴孔。The spinner is provided with a plurality of helical spinning blades around the axis, and a flow channel is formed between two adjacent spinning blades. One end of the spinner is provided with a fixing ring. The fixing ring and the spinning blades Fixed connection, the spinner is fixedly connected with the sensor housing through the fixing ring, and the other end of the spinner is provided with a shaft hole for installing the bearing.
所述起旋器的起旋叶片的数量不少于4个。The number of spinning blades of the spinner is not less than four.
所述导流架包括中心柱,所述中心柱圆周设有至少三个用于导向的支撑片,一定位环位于导流架下游端与支撑片固定连接,所述定位环位于传感器壳体的阶梯形通孔的出口端与传感器壳体固定,所述中心柱的上游端设置用于安装轴承的轴孔。The guide frame includes a central column, and at least three support sheets for guiding are arranged on the circumference of the central column. A positioning ring is located at the downstream end of the guide frame and is fixedly connected to the support sheet, and the positioning ring is located on the sensor housing. The outlet end of the stepped through hole is fixed with the sensor housing, and the upstream end of the central column is provided with a shaft hole for installing the bearing.
所述导流架的定位环通过一定位销与传感器壳体固定。The positioning ring of the guide frame is fixed with the sensor housing through a positioning pin.
所述传感器壳体的阶梯形通孔的变径段,从进口端向小径段方向孔径逐渐变小。The diameter-reducing section of the stepped through hole of the sensor housing gradually decreases in diameter from the inlet end to the direction of the small-diameter section.
所述叶轮固定在一叶轮轴上。The impeller is fixed on an impeller shaft.
所述进口端水平接管上游端设有一连接法兰,下游端通过一卡套螺母与传感器壳体固定连接;所述出口端水平接管上游端通过卡套螺母与传感器壳体固定连接,下游端设有连接法兰。The upstream end of the horizontal pipe at the inlet end is provided with a connecting flange, and the downstream end is fixedly connected with the sensor shell through a ferrule; the upstream end of the horizontal pipe at the outlet end is fixedly connected with the sensor shell through a ferrule, and the downstream end is There are connecting flanges.
所述进口端水平接管、出口端水平接管与传感器壳体之间均设有密封垫。Gaskets are provided between the horizontal pipe at the inlet end, the horizontal pipe at the outlet end and the sensor housing.
本发明的一种测量微小气体流量的涡轮流量计,包括传感器壳体,所述传感器壳体的上端通过放大器连接转换器,所述传感器壳体的进口端、出口端均设有水平接管,所述传感器壳体内设有阶梯形通孔,所述阶梯形通孔的进口端、出口端均为大径段,中间为小径段,所述小径段与进口端之间设有一变径段;所述进口端内设置一起旋器,出口端内设置一导流架,所述导流架的一端插入阶梯形通孔的小径段中,一叶轮位于小径段中,所述叶轮的轴的两端分别支承于起旋器、导流架上设置的轴孔中;当微小气体通过起旋器形成漩涡流,该漩涡流经过传感器壳体内部的变径段进行加速,形成高速的漩涡流,从而增大感器壳体内气体流速,进而增大叶轮的转动速度,从而可有效的测量微小气体流量,提高了检测效率及测量精度。所述进口端水平接管的孔径与阶梯形通孔的大径段相同,所述出口端水平接管的管孔为阶梯孔,该阶梯孔上游为小径端,该小径端的孔径小于传感器壳体的阶梯形通孔的小径段孔径,该阶梯孔下游的大径端孔径与进口端水平接管的孔径相同。从而快速有效的使高速的漩涡流得到复原,避免经过涡轮流量计的气体对其他部件造成影响。所述叶轮的轴的两端分别通过止推轴承和滑动轴承支承于起旋器、导流架上的轴孔中。采用止推轴承和滑动轴承,有效降低叶轮的轴与起旋器、导流架之间的磨损,提高了涡轮流量计的使用寿命。The present invention provides a turbine flowmeter for measuring tiny gas flow, comprising a sensor housing, the upper end of the sensor housing is connected to a converter through an amplifier, and the inlet and outlet ends of the sensor housing are provided with horizontal pipes, so The sensor housing is provided with a stepped through hole, the inlet end and the outlet end of the stepped through hole are large-diameter sections, the middle is a small-diameter section, and a variable-diameter section is arranged between the small-diameter section and the inlet end; The inlet end is provided with a co-rotator, and the outlet end is provided with a guide frame, one end of the guide frame is inserted into the small diameter section of the stepped through hole, an impeller is located in the small diameter section, and both ends of the shaft of the impeller are located in the small diameter section. They are respectively supported in the shaft holes provided on the spinner and the guide frame; when the tiny gas passes through the spinner to form a vortex flow, the vortex flow is accelerated through the variable diameter section inside the sensor housing to form a high-speed vortex flow, thereby The gas flow rate in the sensor shell is increased, thereby increasing the rotation speed of the impeller, so that the small gas flow rate can be effectively measured, and the detection efficiency and measurement accuracy are improved. The diameter of the horizontal pipe at the inlet end is the same as the large diameter section of the stepped through hole, the pipe hole of the horizontal pipe at the outlet end is a stepped hole, the upstream of the stepped hole is the small diameter end, and the diameter of the small diameter end is smaller than that of the sensor housing. The diameter of the small diameter section of the through hole is the same as the diameter of the large diameter end downstream of the stepped hole. Therefore, the high-speed vortex flow can be restored quickly and effectively, and the gas passing through the turbine flowmeter can be prevented from affecting other components. Both ends of the shaft of the impeller are respectively supported in the shaft holes on the spinner and the guide frame through a thrust bearing and a sliding bearing. Thrust bearing and sliding bearing are used to effectively reduce the wear between the shaft of the impeller, spinner and guide frame, and improve the service life of the turbine flowmeter.
本发明的测量微小气体流量的涡轮流量计,与现有技术相比,当测量微小气体流量时,测量效率高,测量精度高,对零部件的磨损小,极大的提高了涡轮流量计的使用寿命。设计巧妙,结构简单,易于实现降低了安装难度,减少了安装工时,提升了装配效率,极大的降低了成本。Compared with the prior art, the turbine flowmeter for measuring tiny gas flow of the present invention has high measurement efficiency, high measurement accuracy, and less wear on components when measuring tiny gas flow, which greatly improves the performance of the turbine flowmeter. service life. The design is ingenious, the structure is simple, and it is easy to realize, which reduces the difficulty of installation, reduces the installation time, improves the assembly efficiency, and greatly reduces the cost.
附图说明Description of drawings
图1为测量微小气体流量的涡轮流量计的结构示意图;Fig. 1 is the structural representation of the turbine flowmeter for measuring tiny gas flow;
图2为测量微小气体流量的涡轮流量计的轴侧图;Fig. 2 is the axonometric view of the turbine flowmeter measuring minute gas flow;
图3为测量微小气体流量的涡轮流量计的俯视图;Fig. 3 is the top view of the turbine flowmeter measuring tiny gas flow;
图4为测量微小气体流量的涡轮流量计的侧视图;Fig. 4 is the side view of the turbine flowmeter measuring minute gas flow;
图5为起旋器的结构示意图;Fig. 5 is the structural representation of the spinner;
图6为起旋器的侧视图;Figure 6 is a side view of the spinner;
图7为导流架的侧视图;Figure 7 is a side view of the guide frame;
图8为图7的A-A向剖视图。FIG. 8 is a cross-sectional view taken along the line A-A in FIG. 7 .
具体实施方式Detailed ways
参考图1至图8,包括一种测量微小气体流量的涡轮流量计,包括传感器壳体4,所述传感器壳体4的上端通过放大器6连接转换器7,所述传感器壳体4的进口端、出口端均设有水平接管,所述传感器壳体4内设有一阶梯形通孔,所述阶梯形通孔的进口端、出口端均为大径段,中间为小径段,所述小径段与进口端之间设有一变径段;所述传感器壳体4的阶梯形通孔的变径段,从进口端向小径段方向孔径逐渐变小,形成锥形孔,用于对通过的气体进行加速。所述进口端内设置一起旋器9,所述起旋器9上设有多个绕轴心呈螺旋状的起旋叶片17,所述起旋器9的起旋叶片17的数量不少于4个,相邻两个起旋叶片之间形成流道,起旋器9的一端设有固定环16,固定环16与起旋叶片17固定连接,起旋器9通过固定环16与传感器壳体4固定连接,起旋器9的另一端设置用于安装轴承的轴孔。本实施例的起旋叶片17的数量为4个,从而形成4个螺旋状流道,使通过的气体形成漩涡流。出口端内设置一导流架15,所述导流架15的一端插入阶梯形通孔的小径段中,所述导流架15包括中心柱20,所述中心柱20圆周设有至少三个用于导向的支撑片21,一定位环19位于导流架15下游端与支撑片21固定连接,所述定位环19位于传感器壳体4的阶梯形通孔的出口端与传感器壳体4固定。本实施例的支撑片21数量为3个,支撑片21为径向延伸的凸起,且沿着中心柱20轴向延伸,形成3个导流通道。所述导流架15的定位环19通过一定位销14与传感器壳体4固定。所述中心柱20的上游端设置用于安装轴承的轴孔。本实施例的导流架15的中心柱20的上游端插入传感器壳体4的阶梯形通孔的小径段中。一叶轮12位于小径段中,所述叶轮12固定在一叶轮轴11上。所述叶轮12的轴的两端分别支承于起旋器9、导流架15上设置的轴孔中;所述叶轮12的轴的两端均通过止推轴承10和滑动轴承13分别支承于起旋器9、导流架15上的轴孔中。本实施例的叶轮轴11一端通过止推轴承10和滑动轴承13支承于起旋器9轴孔中,另一端通过止推轴承10和滑动轴承13支承于导流架15的中心柱20的轴孔中。所述进口端水平接管2的孔径与阶梯形通孔的大径段相同,所述出口端水平接管5的管孔为阶梯孔,该阶梯孔上游为小径端,该小径端的孔径小于传感器壳体4的阶梯形通孔的小径段孔径,该阶梯孔下游的大径端孔径与进口端水平接管2的孔径相同。本实施例的出口端水平接管5的小径端与大径端之间设有直径逐渐变大的变径段。所述进口端水平接管2上游端设有一连接法兰1,下游端通过一卡套螺母3与传感器壳体4固定连接;所述出口端水平接管5上游端通过卡套螺母3与传感器壳体4固定连接,下游端设有连接法兰1。所述进口端水平接管2、出口端水平接管5与传感器壳体4之间均设有密封垫8。Referring to FIGS. 1 to 8 , it includes a turbine flowmeter for measuring tiny gas flow, including a
本发明的测量微小气体流量的涡轮流量计工作时,微小气体通过进口端水平接管进入传感器壳体,微小气体通过起旋器的起旋叶片形成漩涡流,漩涡流流经传感器壳体内的变径段加速,形成高速的漩涡流,高速漩涡流冲击叶轮带动叶轮转动,所述叶轮为导磁叶轮,放大器上设有磁场线圈及磁感应装置,叶轮旋转会切割磁感线,放大器感应叶轮切割频率,结合K值,计算出微小流量气体的准确流量。When the turbine flowmeter of the present invention for measuring the flow rate of tiny gas works, the tiny gas enters the sensor housing through the horizontal nozzle at the inlet end, and the tiny gas passes through the spinning blades of the spinner to form a vortex flow, and the vortex flow flows through the variable diameter in the sensor housing. The high-speed eddy current impacts the impeller to drive the impeller to rotate. The impeller is a magnetic-conducting impeller. The amplifier is equipped with a magnetic field coil and a magnetic induction device. Combined with the K value, the accurate flow rate of the micro-flow gas is calculated.
以上所述仅为本发明的优选实施例,并不用于限制本发明,本领域的技术人员在不脱离本发明的精神的前提下,对本发明进行的改动均落入本发明的保护范围。The above descriptions are only preferred embodiments of the present invention, and are not intended to limit the present invention. Those skilled in the art may make changes to the present invention without departing from the spirit of the present invention.
Claims (10)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210396559.5A CN114777853A (en) | 2022-04-15 | 2022-04-15 | Turbine flowmeter for measuring micro gas flow |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202210396559.5A CN114777853A (en) | 2022-04-15 | 2022-04-15 | Turbine flowmeter for measuring micro gas flow |
Publications (1)
Publication Number | Publication Date |
---|---|
CN114777853A true CN114777853A (en) | 2022-07-22 |
Family
ID=82429631
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202210396559.5A Pending CN114777853A (en) | 2022-04-15 | 2022-04-15 | Turbine flowmeter for measuring micro gas flow |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN114777853A (en) |
-
2022
- 2022-04-15 CN CN202210396559.5A patent/CN114777853A/en active Pending
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5529084A (en) | Laminar flow elbow system and method | |
CN201007664Y (en) | Hall flow sensor | |
US5509305A (en) | Closely coupled, dual turbine volumetric flow meter | |
CN217442616U (en) | Turbine flowmeter for measuring tiny gas flow | |
US6439062B2 (en) | Flow anomaly detector | |
CN114777853A (en) | Turbine flowmeter for measuring micro gas flow | |
CN114046298A (en) | Flow field uniform distribution device suitable for adjustable shrinkage cavity of pulverized coal pipeline | |
US8505378B2 (en) | Orbital ball flowmeter for gas and fluid | |
JP7159754B2 (en) | Impeller type flow meter | |
CN109443458B (en) | A concave arc dual-flow direction average velocity tube flowmeter | |
CN210268751U (en) | Liquid turbine flowmeter with multiple rectifying devices | |
US3143882A (en) | Fluid transducer | |
CN116182960B (en) | Gas turbine flowmeter with swirl guide body | |
RU2082102C1 (en) | Turbine flow rate converter | |
Salami | Effect of upstream velocity profile and integral flow straighteners on turbine flowmeters | |
CN1595070A (en) | Front flow guiding apparatus and turbine gas flow measurement device equipped with the same | |
EP1464927A2 (en) | A flowmeter with magnetic sensor | |
US3427879A (en) | Flow meter | |
CN210981383U (en) | Portable turbine flowmeter | |
CN113503291B (en) | Flow regulator for measuring flow field behind bent pipe | |
WO1995005581A1 (en) | Closely coupled, dual turbine volumetric flow meter | |
RU2337321C1 (en) | Turbine flow meter | |
KR20110035846A (en) | Turbine flowmeter | |
CN210922718U (en) | Multistage Turbine for Turbine Flow Meters | |
CN219996244U (en) | Impeller mechanism and flowmeter |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination |