CN108562341A - A kind of reflective multichannel ultrasonic gas flowmeter runner - Google Patents
A kind of reflective multichannel ultrasonic gas flowmeter runner Download PDFInfo
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- 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
- G01F1/66—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 measuring frequency, phase shift or propagation time of electromagnetic or other waves, e.g. using ultrasonic flowmeters
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Abstract
本发明提供了一种反射式多声道超声波气体流量计流道,包含直通管道,所述直通管道设有进口端与出口端;在直通管道上设有若干超声波换能器组,直通管道内靠进口端一侧设有气体整流结构;所述气体整流结构包含横截面呈蜂窝状结构的气流通道,气流通道与直通管道轴向整体平行。本发明的有益效果在于:一方面能够适用更短的直通管道,减小气体流量计流道的占用体积,另一方面也使得超声波测量更为稳定准确。
The invention provides a reflective multi-channel ultrasonic gas flowmeter flow path, which includes a straight-through pipe, and the straight-through pipe is provided with an inlet end and an outlet end; A gas rectification structure is provided on the side near the inlet end; the gas rectification structure includes an air flow channel with a honeycomb structure in cross section, and the air flow channel is parallel to the axial direction of the straight-through pipe as a whole. The beneficial effect of the present invention is that: on the one hand, shorter straight-through pipes can be applied to reduce the occupied volume of the flow channel of the gas flowmeter; on the other hand, the ultrasonic measurement is more stable and accurate.
Description
技术领域technical field
本发明涉及燃气计量装置技术领域,具体涉及气体流量计的结构优化。The invention relates to the technical field of gas metering devices, in particular to the structural optimization of gas flowmeters.
背景技术Background technique
现有反射式超声波气体流量计的基本原理是时差法,通过流道壁上安装的与气体流动方向成一定夹角的超声波传感器测量超声信号,在超声波传感器间传播的顺流时间td和逆流时间tu,通过顺流时间和逆流时间的差值Δt可以获取气流速度信息V(Δt),但申请人经过研究发现,由于气流在气体流量计中存在紊流现象,因此超声波传感器测得的顺流时间和逆流时间的差值是存在一定误差或存在波动的,进而影响到气体流量的整体测量精度。The basic principle of the existing reflective ultrasonic gas flowmeter is the time difference method. The ultrasonic sensor installed on the flow channel wall and the direction of the gas flow at a certain angle measures the ultrasonic signal. The forward flow time td and the reverse flow time propagated between the ultrasonic sensors tu, the airflow velocity information V(Δt) can be obtained through the difference Δt between the forward flow time and the reverse flow time, but the applicant found through research that due to the turbulence of the airflow in the gas flowmeter, the forward flow measured by the ultrasonic sensor There is a certain error or fluctuation in the difference between the time and the reverse flow time, which in turn affects the overall measurement accuracy of the gas flow.
发明内容Contents of the invention
针对现有技术中所存在的不足,本发明提供了一种反射式多声道超声波气体流量计流道,其目的在于解决气体扰动带来的测量精度误差。Aiming at the deficiencies in the prior art, the present invention provides a reflective multi-channel ultrasonic gas flowmeter flow channel, which aims to solve the measurement accuracy error caused by gas disturbance.
为实现上述目的,本发明采用了如下的技术方案:To achieve the above object, the present invention adopts the following technical solutions:
一种反射式多声道超声波气体流量计流道,包含直通管道,所述直通管道设有进口端与出口端;在直通管道上设有若干超声波换能器组,直通管道内靠进口端一侧设有气体整流结构;所述气体整流结构包含横截面呈蜂窝状结构的气流通道,气流通道与直通管道轴向整体平行。A reflective multi-channel ultrasonic gas flowmeter flow channel includes a straight-through pipe, the straight-through pipe is provided with an inlet end and an outlet end; a number of ultrasonic transducer groups are arranged on the straight-through pipe, and the straight-through pipe is close to the inlet end. A gas rectification structure is provided on the side; the gas rectification structure includes an air flow channel with a honeycomb structure in cross section, and the air flow channel is generally parallel to the axial direction of the straight-through pipe.
进一步的,所述直通管道的进口端设有导流环,所述导流环整体呈锥形或喇叭形,且导流环的横截面呈流线型。Further, the inlet end of the straight-through pipe is provided with a guide ring, the guide ring is generally tapered or trumpet-shaped, and the cross-section of the guide ring is streamlined.
流道前端带有导流环和气体整流结构,使得流道前端的各向异性的混乱流动整流为与流道轴向平行的有效流动,能对前端更大雷诺数的流体进行整流,气体整流结构后端的层流尾迹小,更容易在较短直管段中消除,一方面能够适用更短的直通管道,减小气体流量计流道的占用体积,另一方面也使得超声波测量更为稳定准确。The front end of the flow channel is equipped with a guide ring and a gas rectification structure, so that the anisotropic chaotic flow at the front end of the flow channel is rectified into an effective flow parallel to the axial direction of the flow channel, which can rectify the fluid with a larger Reynolds number at the front end, and the gas rectification The laminar flow wake at the back end of the structure is small, and it is easier to eliminate it in a shorter straight pipe section. On the one hand, it can be applied to a shorter straight pipe, reducing the occupied volume of the flow channel of the gas flowmeter, and on the other hand, it also makes the ultrasonic measurement more stable and accurate. .
附图说明Description of drawings
图1为实施例的结构示意图。Fig. 1 is the structural representation of embodiment.
图2为实施例的截面示意图。Fig. 2 is a schematic cross-sectional view of the embodiment.
具体实施方式Detailed ways
下面结合附图及实施例对本发明中的技术方案进一步说明。The technical solutions in the present invention will be further described below in conjunction with the accompanying drawings and embodiments.
一种反射式多声道超声波气体流量计流道,如图1所示,包含直通管道1,所述直通管道1设有进口端与出口端;在直通管道1上设有若干超声波换能器组,还设有温度传感器与压力传感器;所述直通管道1的进口端设有导流环2,所述导流环2整体呈锥形或喇叭形,且导流环2的纵截面的内壁呈流线型,能有效减小气体在口径变小时的压力损失,并保持流体的定常流动状态;直通管道1内靠进口端一侧设有气体整流结构3;所述气体整流结构3包含横截面呈蜂窝状结构的气流通道,气流通道与直通管道轴向整体平行;气体通道所述蜂窝状结构中蜂窝单元格截面包含六边形、四边形、五边形、三角形的其中一种或多种,以使得气体整流结构3适应不同直通管道1内截面的形状设计;所述气体整流结构3的外缘与直通管道的内径为过盈配合连接,由此可根据现有气体流量计的流道结构设计与之匹配的气体整流结构3进行安装,改善现有气体流量计的紊流效应。A reflective multi-channel ultrasonic gas flowmeter flow channel, as shown in Figure 1, includes a straight-through pipeline 1, and the straight-through pipeline 1 is provided with an inlet end and an outlet end; a number of ultrasonic transducers are arranged on the straight-through pipeline 1 group, and a temperature sensor and a pressure sensor are also provided; the inlet end of the straight pipe 1 is provided with a guide ring 2, and the guide ring 2 is in the shape of a cone or a trumpet as a whole, and the inner wall of the longitudinal section of the guide ring 2 It is streamlined, which can effectively reduce the pressure loss of the gas when the caliber becomes smaller, and maintain a steady flow state of the fluid; a gas rectification structure 3 is provided on the side of the straight-through pipeline 1 near the inlet end; the gas rectification structure 3 includes a cross-section of The airflow channel of the honeycomb structure, the airflow channel is parallel to the axial direction of the straight-through pipe; the honeycomb cell section in the honeycomb structure of the gas channel includes one or more of hexagonal, quadrilateral, pentagonal, and triangular, and The gas rectification structure 3 is adapted to the shape design of the inner section of the straight-through pipe 1; the outer edge of the gas rectification structure 3 and the inner diameter of the straight-through pipe are connected by an interference fit, which can be designed according to the flow channel structure of the existing gas flowmeter The matching gas rectification structure 3 is installed to improve the turbulence effect of the existing gas flowmeter.
所述气体整流结构3满足L≥10DH;其中L为气体整流结构3长度,DH为气流通道所述蜂窝状结构中蜂窝单元格的水力直径,且是非圆管流动的特征长度;从而有效的将紊流气流整流为平顺的直通气流;所述蜂窝单元格的水力直径DH=4A/P,其中A为蜂窝单元格的过流面积,P为蜂窝单元格的湿周;所述气体整流结构需满足:d≥50a,其中,d为气流通道所述蜂窝状结构中蜂窝单元格的内切圆直径,a为蜂窝单元格侧壁的壁厚,由此设计,气流通道所呈蜂窝单元格不仅侧壁厚度小,且对管道的节流作用小,压损小;气流通道所述蜂窝状结构中蜂窝单元格的内切圆直径d满足0.077D≤d≤0.173D,其中D为流道管径,从而达到更好的整流效果,并消除了蜂窝单元格壁厚对整流器出口流场的影响。The gas rectification structure 3 satisfies L≥10D H ; where L is the length of the gas rectification structure 3, and D H is the hydraulic diameter of the honeycomb cell in the honeycomb structure of the air flow channel, and is the characteristic length of the non-circular pipe flow; thus effectively The turbulent airflow is rectified into a smooth straight-through airflow; the hydraulic diameter D H of the honeycomb cell = 4A/P, where A is the flow area of the honeycomb cell, and P is the wetted periphery of the honeycomb cell; the gas The rectification structure needs to satisfy: d≥50a, where d is the diameter of the inscribed circle of the honeycomb cell in the honeycomb structure of the air flow channel, and a is the wall thickness of the side wall of the honeycomb cell. Based on this design, the air flow channel is honeycomb The cell not only has a small side wall thickness, but also has a small throttling effect on the pipeline and a small pressure loss; the diameter d of the inscribed circle of the honeycomb cell in the honeycomb structure described in the airflow channel satisfies 0.077D≤d≤0.173D, where D is The diameter of the flow channel can achieve a better rectification effect and eliminate the influence of the wall thickness of the honeycomb cell on the flow field at the outlet of the rectifier.
综上,通过导流环2与气体整流结构3的设计,使得流道前端的各向异性的混乱流动整流为与流道轴向平行的有效流动,能对前端更大雷诺数的流体进行整流,且整流效果好。整流器后端的层流尾迹小,更容易在较短直管段中消除,整流器后端直管段要求小。In summary, through the design of the guide ring 2 and the gas rectification structure 3, the anisotropic chaotic flow at the front end of the flow channel is rectified into an effective flow parallel to the axial direction of the flow channel, and the fluid with a larger Reynolds number at the front end can be rectified , and the rectification effect is good. The laminar flow wake at the rear end of the rectifier is small, which is easier to eliminate in the shorter straight pipe section, and the straight pipe section at the rear end of the rectifier requires less.
所述超声波换能器组的数量不小于两个,至少两组超声波换能器组在流道横截面上的投影夹角在30°到90°之间。如图1,图2所示,本实施例中,超声波换能器组的数量为两个,超声波换能器组中的超声波换能器均为超声波发射-超声波接收一体式换能器,分别包含第一超声波换能器组的第一超声波换能器401、第二超声波换能器402,与第二超声波换能器组的第三超声波换能器403、第四超声波换能器404;任一超声波换能器组中的两个超声波换能器呈V形夹角安装于直通管道上,V形夹角的角度θ在40°-90°,从而可以在减小流量计外形体积的情况下增大有效声程。在直通管道1的内壁还设有若干修正式聚能反射面结构5;任一修正式聚能反射面结构5呈椭圆的弧面形状,所述弧面形状的凹面处于超声波换能器组中超声波发射接收所呈V形路径的拐点区域;使得从发射端超声波换能器发出的信号经过修正式聚能反射面结构的聚焦和反射后,增强接收传递的超声波信号强度并修正超声信号的偏移、增大流量计量程,实现接收端超声波换能器对超声波信号的有效接收。The number of the ultrasonic transducer groups is not less than two, and the projection angle of at least two groups of ultrasonic transducer groups on the flow channel cross section is between 30° and 90°. As shown in Fig. 1 and Fig. 2, in the present embodiment, the quantity of ultrasonic transducer groups is two, and the ultrasonic transducers in the ultrasonic transducer groups are all ultrasonic transmitting-ultrasonic receiving integrated transducers, respectively Including the first ultrasonic transducer 401 and the second ultrasonic transducer 402 of the first ultrasonic transducer group, and the third ultrasonic transducer 403 and the fourth ultrasonic transducer 404 of the second ultrasonic transducer group; The two ultrasonic transducers in any ultrasonic transducer group are installed on the straight-through pipe at a V-shaped angle, and the angle θ of the V-shaped angle is 40°-90°, so that the volume of the flowmeter can be reduced. In this case, the effective sound path is increased. The inner wall of the straight-through pipeline 1 is also provided with several modified energy-gathering reflective surface structures 5; any modified energy-gathered reflective surface structure 5 is in the shape of an ellipse arc, and the concave surface of the arc shape is in the ultrasonic transducer group The inflection point area of the V-shaped path of ultrasonic transmission and reception; after the signal sent from the ultrasonic transducer at the transmitting end is focused and reflected by the modified energy-gathering reflective surface structure, the strength of the received and transmitted ultrasonic signal is enhanced and the deviation of the ultrasonic signal is corrected. Move and increase the range of the flowmeter to realize the effective reception of the ultrasonic signal by the ultrasonic transducer at the receiving end.
如图1所示,第一超声波换能器401与第二超声波换能器402、第三超声波换能器403与第四超声波换能器404在流道横截面上的投影或信号传输路径所在的平面夹角在30°到90°之间。多组超声波换能器组的测量能够获得相对更为全面完整的传感数据,从而为通过算法优化通过流道的流量计算提供数据支持,大幅降低单对传感器带来的计量误差。As shown in Figure 1, the projections or signal transmission paths of the first ultrasonic transducer 401 and the second ultrasonic transducer 402, the third ultrasonic transducer 403 and the fourth ultrasonic transducer 404 on the flow channel cross section The angle between the planes is between 30° and 90°. The measurement of multiple sets of ultrasonic transducer groups can obtain relatively more comprehensive and complete sensing data, thereby providing data support for optimizing the flow calculation through the flow channel through the algorithm, and greatly reducing the measurement error caused by a single pair of sensors.
最后说明的是,以上实施例仅用以说明本发明的技术方案而非限制,尽管参照较佳实施例对本发明进行了详细说明,本领域的普通技术人员应当理解,可以对本发明的技术方案进行修改或者等同替换,而不脱离本发明技术方案的宗旨和范围,其均应涵盖在本发明的权利要求范围当中。Finally, it is noted that the above embodiments are only used to illustrate the technical solutions of the present invention without limitation. Although the present invention has been described in detail with reference to the preferred embodiments, those of ordinary skill in the art should understand that the technical solutions of the present invention can be carried out Modifications or equivalent replacements without departing from the spirit and scope of the technical solution of the present invention shall be covered by the claims of the present invention.
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