JPH01136024A - Vortex flowmeter - Google Patents
Vortex flowmeterInfo
- Publication number
- JPH01136024A JPH01136024A JP29340887A JP29340887A JPH01136024A JP H01136024 A JPH01136024 A JP H01136024A JP 29340887 A JP29340887 A JP 29340887A JP 29340887 A JP29340887 A JP 29340887A JP H01136024 A JPH01136024 A JP H01136024A
- Authority
- JP
- Japan
- Prior art keywords
- vortex
- fluid
- measured
- flow
- flow velocity
- 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
Abstract
Description
【発明の詳細な説明】
〈産業上の利用分野〉
本発明は低レイノルズ数領域における渦流量計の流量特
性を多孔板を用いて改善することに関す〈従来の技術〉
従来の渦流量計の流量特性は第7図に示すようにレイノ
ルズ数5X103以下では、渦の放出が不安定となるた
め、動作可能範囲としては、下限は5X103程度であ
った。[Detailed Description of the Invention] <Industrial Application Field> The present invention relates to improving the flow characteristics of a vortex flowmeter in a low Reynolds number region using a perforated plate. As for the flow rate characteristics, as shown in FIG. 7, when the Reynolds number is less than 5X103, the vortex shedding becomes unstable, so the lower limit of the operable range was about 5X103.
〈発明が解決しようとする問題点〉
したがって、
(1)渦流量計で、化学流体、油等の高粘度流体を測定
するばあい、測定レンジが狭いくレイノルズ数<5 X
10’での測定ができない、)という問題がある。<Problems to be solved by the invention> Therefore, (1) When measuring high viscosity fluids such as chemical fluids and oil with a vortex flow meter, the measurement range is narrow and Reynolds number < 5
There is a problem that measurement at 10' is not possible.
(2)レイノルズ数2X10’以下では、第7図に示す
ように、Kファクター((渦周波数)/(流量))が急
激に上昇し、リニアリティが悪化するという問題がある
。(2) When the Reynolds number is 2×10' or less, as shown in FIG. 7, there is a problem that the K factor ((vortex frequency)/(flow rate)) increases rapidly and the linearity deteriorates.
本発明は、この問題点を、解決するものである。The present invention solves this problem.
本発明の目的は、測定下限付近のレイノルズ数を小さく
して、測定可能下限を下げ、測定可能範囲を広げると共
に、測定下限近くのリニアリティの改善により、特性の
良好な渦流量計を提供するにある。An object of the present invention is to provide a vortex flowmeter with good characteristics by reducing the Reynolds number near the lower measurement limit, lowering the measurable lower limit and widening the measurable range, and improving linearity near the measurement lower limit. be.
く問題を解決するための手段〉
この目的を達成するために、本発明は、測定流体の流れ
る管路に設けられ測定流体の整流作用をなす整流装置と
、該整流装置の下流に配置された渦発生体とを具備する
渦流量計において、(渦発生体の流れに対向する幅の寸
法)/(管路内径)が0.2〜0.3をなす渦発生体と
、整流板本体と測定流体の層流流速分布に対して逆比例
の圧力損失を与えて乱流流速分布となるように前記整流
板本体を少くとも3個の等面積部分に分けてオリフィス
の圧力損失式を利用して決定された開口比となるように
該整流板本体に設けられた複数の貫通孔とを備える整流
装置とを具備したことを特徴とする渦流量計を構成した
らのである。Means for Solving the Problems To achieve this object, the present invention provides a rectifying device that is provided in a pipe through which a measuring fluid flows and acts to rectify the measuring fluid, and a rectifying device that is disposed downstream of the rectifying device. In a vortex flowmeter comprising a vortex generator, the vortex generator has a ratio of (width dimension facing the flow of the vortex generator)/(pipe inner diameter) of 0.2 to 0.3, and a current plate main body. The rectifying plate body is divided into at least three equal area parts and the orifice pressure loss formula is used to give a pressure loss inversely proportional to the laminar flow velocity distribution of the measured fluid to create a turbulent flow velocity distribution. The vortex flow meter is characterized in that it comprises a rectifying device including a plurality of through holes provided in the rectifying plate body so as to have an aperture ratio determined by the flow rate meter.
く作用〉
以上の構成において、レイノルズ数の低い低流速流体は
層流、あるいは、乱流状態で整流装置に流入する。整流
装置で、乱流状態に整流されたのち、下流に配置された
渦発生体により測定流体の流速が測定される。Effect> In the above configuration, the low flow velocity fluid with a low Reynolds number flows into the rectifier in a laminar flow or turbulent flow state. After the flow is rectified into a turbulent state by the rectifier, the flow velocity of the measurement fluid is measured by a vortex generator disposed downstream.
以下、実施例に基づき詳細に説明する。Hereinafter, a detailed explanation will be given based on examples.
〈実施例〉 第1図は、本発明の一実施例の構成説明図である。<Example> FIG. 1 is an explanatory diagram of the configuration of an embodiment of the present invention.
図において、1は測定流体2の流れる管路、3は整流装
置である。整流装置3は円板状の整流板本体31と整流
板本体31に設けられた貫通孔32(後述する。)より
なる、4は渦発生体、5は渦発生体4によって発生する
渦の数に対応した信号を変換して出力信号とする変換回
路、6はその出力端子である。In the figure, 1 is a conduit through which a measuring fluid 2 flows, and 3 is a rectifier. The rectifying device 3 consists of a disc-shaped rectifying plate main body 31 and a through hole 32 (described later) provided in the rectifying plate main body 31, 4 is a vortex generator, and 5 is the number of vortices generated by the vortex generator 4. 6 is an output terminal of a conversion circuit which converts a signal corresponding to the signal into an output signal.
以上の構成において、レイノルズ数の低い低流速流体2
は層流、あるいは、乱流状態で整流装置3に流入する。In the above configuration, the low flow velocity fluid 2 with a low Reynolds number
flows into the rectifier 3 in a laminar or turbulent state.
整流装置3で、乱流状態に整流されたのち、下流に配置
された渦発生体4により測定流体2の流速が測定される
。After being rectified into a turbulent state by the rectifier 3, the flow velocity of the measurement fluid 2 is measured by the vortex generator 4 disposed downstream.
ところで、従来の渦流量計で、渦放出のメカニズムとリ
ニアリティとの関係は下記のとおりである。By the way, in a conventional vortex flowmeter, the relationship between the vortex shedding mechanism and linearity is as follows.
(1)レイノルズ数Re≧2X10’においては、第2
図に示す如く、流れが乱流流速分布であるため、渦発生
体の閉塞効果により、渦発生体2の真横では、はぼフラ
ットな流速分布Bとなる。(1) When the Reynolds number Re≧2X10', the second
As shown in the figure, since the flow has a turbulent flow velocity distribution, the flow velocity distribution B becomes almost flat right next to the vortex generator 2 due to the occlusion effect of the vortex generator.
このため、渦放出は安定であり、かつリニアリティが良
い。Therefore, the vortex shedding is stable and has good linearity.
但し、上記フラットな流速分布を与えるには、(渦発生
体の流れに対向する幅の寸法)/(管路内径)が0.2
〜0.3の値が必要となり、円管路用として製品化され
ている渦流1計の渦発生体は、はぼこの値となっている
。However, in order to provide the above-mentioned flat flow velocity distribution, (dimension of the width of the vortex generator facing the flow)/(pipe inner diameter) is 0.2.
A value of ~0.3 is required, and vortex generators with a single vortex current, which are commercialized for use in circular pipes, have a hollow value.
(2)レイノルズ数Re≦2XLO’になると、上記閉
塞効果だけでは流速分布のフラット化はできないが、製
糸の屈曲の程度が小さいため、渦放出は可能である。し
かし、リニアリティは悪化する6
(3)レイノルズ数Re≦5X10’になると、測定流
体の流れが層流の流速分布Cに近くなる。(2) When the Reynolds number Re≦2XLO', the flow velocity distribution cannot be flattened only by the above-mentioned occlusion effect, but since the degree of bending of the yarn is small, vortex shedding is possible. However, the linearity deteriorates.6 (3) When the Reynolds number Re≦5X10', the flow of the measured fluid approaches the flow velocity distribution C of laminar flow.
このため、第3図に示すように、製糸の屈曲が大きくな
りD、渦放出が困難となる。For this reason, as shown in FIG. 3, the curvature of the yarn becomes large D, making it difficult to release the vortex.
本発明では、円板状の整流板本体31とa流板本体31
に設けられた貫通孔32よりなる整流装置3を適用する
ことにより、I×103≦レイノルズ数≦2X10’で
の渦放出を安定化させ且つリニアリティを改善する。In the present invention, the disc-shaped current plate main body 31 and the a current plate main body 31
By applying the rectifying device 3 consisting of the through hole 32 provided in the flowchart, the vortex shedding is stabilized and the linearity is improved when I×103≦Reynolds number≦2×10′.
このために、層流(レイノルズ数Re中1×103)の
流速分布を、乱流(レイノルズ数Re中2XIO’)の
流速分布に変換する円板状の整流板本体31と整流板本
体31に設けられた貫通孔32よりなる整流装置3を使
用する。For this purpose, a disc-shaped rectifying plate main body 31 and a rectifying plate main body 31 are used to convert the flow velocity distribution of laminar flow (Reynolds number Re of 1×103) into the flow velocity distribution of turbulent flow (Reynolds number Re of 2XIO'). A rectifier 3 consisting of a through hole 32 provided is used.
ここで、整流装置3は下記のように設計する。Here, the rectifier 3 is designed as follows.
第4図に示すように、¥11fL板本体31を各部分が
等面積となるように、n等分する。この場合は、同心円
状に、面積St=面積S2=面積S、となるように3等
分する。As shown in FIG. 4, the ¥11fL plate main body 31 is divided into n equal parts so that each part has an equal area. In this case, the area is concentrically divided into three equal parts such that area St=area S2=area S.
また、第5図に示すように、各部分の平均流速を、整流
板本体31の上流側■1〜■コ、下流側Va〜vbとす
る。Further, as shown in FIG. 5, the average flow velocity of each portion is set as 1 to 2 on the upstream side and Va to vb on the downstream side of the current plate main body 31.
このとき、整流板本体31の面積S、〜S、の開口比m
l〜m3を各々V、−+Va、V2−*Vb、■3→V
Cとなるように決定する。開口比m、〜m3は、各部分
を近似的にオリフィスとみなせば、各々上記の流速分布
となる圧損計数に1〜にコを与えることにより、オリフ
ィスの実験式%式%
から求めることができる。At this time, the aperture ratio m of the area S, ~S, of the current plate main body 31
l~m3 respectively V, -+Va, V2-*Vb, ■3→V
Determine it to be C. The opening ratios m and ~m3 can be obtained from the empirical formula of the orifice by giving 1 to the pressure drop coefficient that gives the above flow velocity distribution, respectively, if each part is approximately regarded as an orifice. .
ここで、第5図において、整流装置3の上流側の層流流
速分布は下記の如き式で示される。Here, in FIG. 5, the laminar flow velocity distribution on the upstream side of the rectifier 3 is expressed by the following equation.
+11=UL (1−(r/R) 2 )uL
;距離rでの流速
UL;最大流速
R;管路1の半径
r ;任意の半径位置
整流装置3の下流側の乱流流速分布は下記の如き式で示
される。+11=UL (1-(r/R) 2 )uL
; Flow velocity UL at distance r; Maximum flow velocity R; Radius r of pipe line 1 ; Arbitrary radial position The turbulent flow velocity distribution on the downstream side of the rectifying device 3 is expressed by the following equation.
uv =UT (1(r/R) I ” )n=21
09 (Re/10)
11T;距離rでの流速
UT 、最大流速
R;管路lの半径
r :イF意の゛i径位置
Re:レイノルズ数
この結果、上記の、整流装置3を使用することにより、
t :< t o ’≦レイノルズ数Re≦2X104
の範囲で、渦信号の大きさく振幅)を約51Δ以上に強
くし、且つ渦信号を安定化させることができる。uv = UT (1(r/R) I'')n=21
09 (Re/10) 11T; Flow velocity UT at distance r, maximum flow velocity R; Radius r of pipe 1: radial position of iF Re: Reynolds number As a result, the above rectifying device 3 is used. By this,
t:<t o'≦Reynolds number Re≦2X104
Within this range, it is possible to increase the amplitude of the vortex signal to about 51Δ or more and stabilize the vortex signal.
デストデータを第6図に示す6
第6図はレイノルズ数Reキ2600での渦波形例で、
(A)図は箇流装置3なしの場合、(B)図は整流装置
3を付けた場合を示す、(A)図のX部分は過渡形が不
安定であることを示す、(A)図の渦周波数fva:Q
、71[z 、振幅Vaは約0.02V、(B)図の渦
周波数fvb:0.62 Hz −@幅vbは約0.1
■である。The dest data is shown in Fig. 6. Fig. 6 is an example of the vortex waveform at a Reynolds number Re of 2600.
(A) Figure shows the case without current flow device 3, (B) Figure shows the case with rectifier 3, (A) The X part in the figure shows that the transient type is unstable, (A) Figure vortex frequency fva:Q
, 71 [z, amplitude Va is approximately 0.02 V, vortex frequency fvb in figure (B): 0.62 Hz - @ width vb is approximately 0.1
■It is.
〈発明の効果〉
以上説明したように、本発明は、測定流体の流れる管路
に設けられ測定流体のNa作用をなす整流装置と、該整
流装置の下流に配置された渦発生体とを具備する渦流量
計において、(渦発生体の流れに対向する幅の寸法)/
(管路内径)が0゜2〜0.3をなす渦発生体と、整流
板本体と測定流体の層流流速分布に対して逆比例の圧力
損失を与えて乱流流速分布となるように前記整流板本体
を少くとも3個の等面積部分に分けてオリフィスの圧力
損失式を利用して決定された開[1比となるように該整
流板本体に設けられた複数の貫通孔とを備える整流装置
とを■L備したことを特徴とする渦流量計を構成した。<Effects of the Invention> As explained above, the present invention includes a rectifier that is provided in a pipe through which a measurement fluid flows and acts as an Na effect on the measurement fluid, and a vortex generator disposed downstream of the rectification device. In a vortex flowmeter, (width dimension facing the flow of the vortex generator)
The vortex generating body (pipe inner diameter) is 0°2 to 0.3, and the pressure loss is inversely proportional to the laminar flow velocity distribution between the baffle plate body and the measured fluid to create a turbulent flow velocity distribution. The baffle plate body is divided into at least three equal area parts, and a plurality of through holes provided in the baffle plate body are formed so that an open ratio of 1 is determined using an orifice pressure loss formula. A vortex flowmeter is constructed, characterized in that it is equipped with a rectifying device.
この結果、本発明の整流装置を、使用することにより、
I Xt o’≦レイノルズ数Re≦2X104の範囲
で、渦信号の大きさ(振幅)を約5倍以上に強くし、且
つ渦信号を安定化させることができる。As a result, by using the rectifier of the present invention,
In the range of I Xt o'≦Reynolds number Re≦2X104, the magnitude (amplitude) of the vortex signal can be increased by about 5 times or more, and the vortex signal can be stabilized.
従って、本発明によれば、測定下限付近のレイノルズ数
を小さくして、測定可能下限を下げ、測定可能範囲を広
げると共に、測定下限近くのりニアリテイの改善により
、特性の良好な渦流2計を実現することが出来る。Therefore, according to the present invention, by reducing the Reynolds number near the lower measurement limit, lowering the measurable lower limit and widening the measurable range, and improving the linearity near the lower measurement limit, a two-meter eddy current meter with good characteristics is realized. You can.
第1図は本発明の一実施例の構成説明図、第2図〜第5
図は第1図の動作説明図、第6図は第1図の効果説明図
、第7図は従来より一般に使用されている従来例の構成
説明図である。
l・・・管路、2・・・測定流体、3・・・竺流装置、
4・・・渦発生体、5・・・変換回路、6・・・出力端
子。
−二し′
第 1 図
第2図
第3図
第4図
第6図
ゼ・、7 :亡1FIG. 1 is an explanatory diagram of the configuration of one embodiment of the present invention, and FIGS. 2 to 5
FIG. 6 is an explanatory diagram of the operation of FIG. 1, FIG. 6 is an explanatory diagram of the effect of FIG. 1, and FIG. 7 is an explanatory diagram of the configuration of a conventional example that has been generally used. l...Pipeline, 2...Measurement fluid, 3...Third flow device,
4... Vortex generator, 5... Conversion circuit, 6... Output terminal. -2' Figure 1 Figure 2 Figure 3 Figure 4 Figure 6
Claims (1)
なす整流装置と、該整流装置の下流に配置された渦発生
体とを具備する渦流量計において、(渦発生体の流れに
対向する幅の寸法)/(管路内径)が0.2〜0.3を
なす渦発生体と、整流板本体と測定流体の層流流速分布
に対して逆比例の圧力損失を与えて乱流流速分布となる
ように前記整流板本体を少くとも3個の等面積部分に分
けてオリフィスの圧力損失式を利用して決定された開口
比となるように該整流板本体に設けられた複数の貫通孔
とを備える整流装置とを具備したことを特徴とする渦流
量計。In a vortex flowmeter, the vortex flowmeter is equipped with a rectifying device installed in a pipe through which the measured fluid flows and has a rectifying effect on the measured fluid, and a vortex generator disposed downstream of the rectifying device. A turbulent flow velocity is created by applying a pressure loss inversely proportional to the laminar flow velocity distribution of the current plate body and the measured fluid, using a vortex generator with a ratio of 0.2 to 0.3 (width dimension)/(pipe inner diameter). A plurality of through holes are provided in the current plate body so that the current plate body is divided into at least three equal area parts so as to have an opening ratio determined using an orifice pressure loss formula. A vortex flow meter characterized by comprising a rectifier having a hole.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP29340887A JPH01136024A (en) | 1987-11-20 | 1987-11-20 | Vortex flowmeter |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP29340887A JPH01136024A (en) | 1987-11-20 | 1987-11-20 | Vortex flowmeter |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH01136024A true JPH01136024A (en) | 1989-05-29 |
Family
ID=17794383
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP29340887A Pending JPH01136024A (en) | 1987-11-20 | 1987-11-20 | Vortex flowmeter |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH01136024A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2339041A1 (en) | 2006-03-17 | 2011-06-29 | University of Tsukuba | Actuator and engine |
| EP2655245B1 (en) | 2010-12-23 | 2015-08-05 | Sidel S.p.A. Con Socio Unico | System and method for filling a container with a pourable product |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5114372A (en) * | 1974-07-26 | 1976-02-04 | Yokogawa Electric Works Ltd | RYUSOKUSOKUTEISOCHI |
| JPS53111763A (en) * | 1977-03-11 | 1978-09-29 | Yokogawa Hokushin Electric Corp | Vortex flow meter |
| JPS5949914B2 (en) * | 1979-07-27 | 1984-12-05 | 日東電工株式会社 | Pasting method |
-
1987
- 1987-11-20 JP JP29340887A patent/JPH01136024A/en active Pending
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5114372A (en) * | 1974-07-26 | 1976-02-04 | Yokogawa Electric Works Ltd | RYUSOKUSOKUTEISOCHI |
| JPS53111763A (en) * | 1977-03-11 | 1978-09-29 | Yokogawa Hokushin Electric Corp | Vortex flow meter |
| JPS5949914B2 (en) * | 1979-07-27 | 1984-12-05 | 日東電工株式会社 | Pasting method |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2339041A1 (en) | 2006-03-17 | 2011-06-29 | University of Tsukuba | Actuator and engine |
| US8007604B2 (en) | 2006-03-17 | 2011-08-30 | University Of Tsukuba | Titanium-tantalum base shape memory alloys, actuator and engine |
| EP2655245B1 (en) | 2010-12-23 | 2015-08-05 | Sidel S.p.A. Con Socio Unico | System and method for filling a container with a pourable product |
| US10633237B2 (en) | 2010-12-23 | 2020-04-28 | Sidel S.P.A. Con Socio Unico | System and method for filling a container with a pourable product |
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