JPS6143205Y2 - - Google Patents
Info
- Publication number
- JPS6143205Y2 JPS6143205Y2 JP594781U JP594781U JPS6143205Y2 JP S6143205 Y2 JPS6143205 Y2 JP S6143205Y2 JP 594781 U JP594781 U JP 594781U JP 594781 U JP594781 U JP 594781U JP S6143205 Y2 JPS6143205 Y2 JP S6143205Y2
- Authority
- JP
- Japan
- Prior art keywords
- flow
- pressure
- upstream
- pressure guiding
- flow rate
- 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.)
- Expired
Links
- 238000011144 upstream manufacturing Methods 0.000 claims description 20
- 239000012530 fluid Substances 0.000 claims description 19
- 238000001514 detection method Methods 0.000 claims description 10
- 230000007423 decrease Effects 0.000 claims description 5
- 238000000926 separation method Methods 0.000 description 7
- 230000001154 acute effect Effects 0.000 description 3
- 230000000694 effects Effects 0.000 description 3
- WABPQHHGFIMREM-UHFFFAOYSA-N lead(0) Chemical compound [Pb] WABPQHHGFIMREM-UHFFFAOYSA-N 0.000 description 2
- 239000000428 dust Substances 0.000 description 1
- 238000002474 experimental method Methods 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 238000007789 sealing Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
Landscapes
- Measuring Volume Flow (AREA)
Description
【考案の詳細な説明】
本考案は被測流体が流れる管路の途中に柱状の
渦発生体を設け、該渦発生体から発生する渦を検
出することにより流速または流量を計測するよう
にした流速・流量計測装置に関するものである。[Detailed description of the invention] This invention provides a columnar vortex generator in the middle of the pipe through which the fluid to be measured flows, and measures the flow velocity or flow rate by detecting the vortex generated from the vortex generator. This relates to flow velocity/flow measuring devices.
従来、渦発生体として三角柱、T型柱等を使用
し、該渦発生体は流体流中で上流側に面する第1
表面と、該第1表面から下流に向うに従つて横方
向断面が減小する第2表面とを有し、前記第1表
面には高圧を導びく第1の導圧孔を設け、第2表
表面の中間位置には該第1の導圧孔と連通する第
2、第3の導圧孔を設け、これらを連通する流路
の途中にサーミスタの如き渦検出素子を設けてな
る渦流量計が知られている。 Conventionally, a triangular prism, a T-shaped prism, etc. has been used as a vortex generator, and the vortex generator has a first part facing upstream in a fluid flow.
a second surface whose lateral cross section decreases downstream from the first surface; the first surface is provided with a first pressure guiding hole for guiding high pressure; A vortex flow rate is provided by providing second and third pressure guiding holes communicating with the first pressure guiding hole at an intermediate position on the front surface, and providing a vortex detecting element such as a thermistor in the middle of a flow path that communicates these holes. The meter is known.
しかし、かかる渦流量計においては、渦発生体
の上流側に面する第1表面が平面であるため、ス
トローハル数の安定した領域が狭く、流量計とし
て広範囲な計測に適しない欠点があつた。また、
第1表面と第2表面との交点の隅角は渦発生体が
正三角柱である場合に60゜であり、それ以外の形
状では隅角が60゜以上となり、隅角部で流体が十
分に剥離せず、強固なカルマン渦を得ることがで
きない欠点があつた。このため、第2表面に設け
られた第2、第3の導圧孔間の圧力変化が小さ
く、高レベルな信号を得ることができない欠点が
あつた。 However, in such a vortex flowmeter, since the first surface facing the upstream side of the vortex generator is a flat surface, the region in which the Strouhal number is stable is narrow, making it unsuitable for wide-range measurement as a flowmeter. . Also,
The corner angle of the intersection of the first surface and the second surface is 60° when the vortex generator is an equilateral triangular prism, and for other shapes, the corner angle is 60° or more, and the fluid does not flow sufficiently at the corner. There was a drawback that separation did not occur and a strong Karman vortex could not be obtained. For this reason, the pressure change between the second and third pressure guiding holes provided on the second surface is small, resulting in a drawback that a high-level signal cannot be obtained.
本考案はこのような従来技術による流速・流量
計測装置の欠点を改良したもので、以下これを図
面に示す実施例と共に説明する。 The present invention is an improvement on the drawbacks of the conventional flow rate/flow measuring device, and will be described below with reference to embodiments shown in the drawings.
図面において、1は管路の途中に設けられた柱
状の渦発生体で、該渦発生体1は管路となる流
速・流量計の本体2の直径部分を貫いて設けら
れ、密封部材3,3により気液密にシールされて
いる。また、本体2の上部には後述の渦検出素子
と接続されるプリアンプ4が設けられている。 In the drawings, reference numeral 1 denotes a columnar vortex generator provided in the middle of the pipe, and the vortex generator 1 is provided through the diameter portion of the main body 2 of the flow rate/flow meter that serves as the pipe, and includes a sealing member 3, 3, it is air-liquid-tightly sealed. Furthermore, a preamplifier 4 is provided at the upper part of the main body 2 to be connected to an eddy detection element to be described later.
次に、前記渦発生体は第2図に示す如く、流れ
に対向する第1表面11と、流れの下流に向うと
共に横方向断面が減小する図中上、下の第2表面
12,13とを有する。前記第1表面11は所定
の曲率半径を有する凹面11Aとして形成され、
第2表面12,13はそれぞれ流体流と平行な上
流側第2表面12A,13Aと、該各上流側第2
表面12A,13Aと連続し下流に向うに従つて
横方向断面が減小する下流側第2表面12B,1
3Bとからなる。そして、第1表面11と上流側
第2表面12A,13Aとの交点は鋭い角度を有
する隅角部14,14となり、該各隅角部14に
おいて流体の剥離を確実に行なわせ、強力なカル
マン渦を発生しうるように構成している。 Next, as shown in FIG. 2, the vortex generator has a first surface 11 facing the flow, and second surfaces 12 and 13 at the top and bottom of the figure whose lateral cross section decreases as they move downstream of the flow. and has. The first surface 11 is formed as a concave surface 11A having a predetermined radius of curvature,
The second surfaces 12 and 13 are respectively parallel to the fluid flow and include upstream second surfaces 12A and 13A;
A downstream second surface 12B, 1 which is continuous with the surfaces 12A, 13A and whose lateral cross section decreases as it goes downstream.
It consists of 3B. The intersections of the first surface 11 and the upstream second surfaces 12A, 13A become corner portions 14, 14 having sharp angles, and the separation of the fluid is ensured at each corner portion 14, and strong Karman It is configured to generate vortices.
また、渦発生体1には第1表面11の凹面11
A最奥部に第1の導圧孔15が開口し、第2表面
12,13にもそれぞれ第2、第3の導圧孔1
6,17が開口している。そして、第1乃至第3
の導圧孔15,16,17はそれぞれ連通管1
8,19,20を介して渦発生体1の軸中心に穿
設された円筒部21と連通している。ここで、前
記第2、第3の導圧孔16,17は上流側第2表
面12A,12Bにそれぞれ開口し、しかも該各
導圧孔16,17の開口位置は流体流中で第1の
導圧孔15の開口位置よりも距離δだけ上流側で
開口している。このように構成することにより、
第1の導圧孔15と第2、第3の導圧孔16,1
7との間の圧力差をより大きくし、高レベルな信
号を検出することができる。 The vortex generator 1 also has a concave surface 11 on the first surface 11.
A first pressure guiding hole 15 is opened at the innermost part of A, and second and third pressure guiding holes 1 are also opened on the second surfaces 12 and 13, respectively.
6 and 17 are open. And the first to third
The pressure guiding holes 15, 16, 17 are connected to the communication pipe 1, respectively.
It communicates with a cylindrical portion 21 bored at the axial center of the vortex generating body 1 via 8, 19, and 20. Here, the second and third pressure guiding holes 16 and 17 open on the upstream second surfaces 12A and 12B, respectively, and the opening positions of the respective pressure guiding holes 16 and 17 are located at the first and second surfaces in the fluid flow. It opens at a distance δ upstream of the opening position of the pressure guiding hole 15 . By configuring like this,
The first pressure hole 15 and the second and third pressure holes 16,1
7 can be made larger, and a high level signal can be detected.
さらに、22は渦発生体1の円筒部21に挿嵌
される内筒を示し、該内筒22は第4図及び第5
図に示される如くその上方部分には3本の環状溝
23が刻設され、該環状溝23から図中下方に延
びる2本の垂直溝24,25が刻説されている。
ここで、環状溝23は連通管18の円筒部21側
開口に対応する位置とされると共に、該環状溝2
3の周囲は塵埃侵入防止用のストレーナ26によ
り施蓋されている(第4図参照)。また、垂直溝
24,25は連通管19,20の円筒部21側開
口に対応する位置まで垂下し(第3図参照)、流
路となる該各垂直溝24,25の途中には例えば
サーミスタ、圧電素子、歪ゲージ等の渦検出素子
27,28がそれぞれ設けられている。29は前
記渦検出素子27,28からの信号をプリアンプ
4に入力するためのリード線である。 Further, 22 indicates an inner cylinder that is inserted into the cylindrical part 21 of the vortex generator 1, and the inner cylinder 22 is shown in FIGS. 4 and 5.
As shown in the figure, three annular grooves 23 are carved in the upper portion thereof, and two vertical grooves 24 and 25 extending downward in the figure from the annular grooves 23 are carved.
Here, the annular groove 23 is located at a position corresponding to the opening on the cylindrical portion 21 side of the communication pipe 18, and the annular groove 23
3 is covered with a strainer 26 to prevent dust from entering (see Fig. 4). Further, the vertical grooves 24 and 25 hang down to positions corresponding to the openings on the cylindrical portion 21 side of the communication pipes 19 and 20 (see FIG. 3), and a thermistor, for example, , piezoelectric elements, strain gauges, and other vortex detection elements 27 and 28 are provided, respectively. 29 is a lead wire for inputting the signals from the eddy detection elements 27 and 28 to the preamplifier 4.
このように構成される流速・流量計測装置にお
いて、流体が第1図中矢示方向に流れると渦発生
体1の隅角部14,14で流体が剥離してカルマ
ン渦が交互に発生し、この渦が発生しない側の静
圧が低くなる。この結果、第1の導圧孔15Aよ
り連通路18及びストレーナ26を介して環状溝
23内に入つた流体は、垂直溝24,25に交互
に流れ、連通路19,20を介して導圧孔16,
17から交互に流出する。この際、垂直溝24,
25の途中に設けられた渦検出素子27,28は
該垂直溝24,25内を流れる流体の流速、温
度、圧力等を差動的に検出し、この検出信号をリ
ード線29を介してプリアンプ4に入力し、流速
または流量として計測する。 In the flow velocity/flow measuring device configured in this way, when the fluid flows in the direction indicated by the arrow in FIG. The static pressure on the side where no vortex is generated is lower. As a result, the fluid entering the annular groove 23 from the first pressure guiding hole 15A via the communication path 18 and the strainer 26 flows alternately into the vertical grooves 24 and 25, and flows through the communicating paths 19 and 20 into the annular groove 23. hole 16,
17 alternately flow out. At this time, the vertical groove 24,
The vortex detection elements 27 and 28 provided in the middle of the vertical grooves 25 differentially detect the flow velocity, temperature, pressure, etc. of the fluid flowing in the vertical grooves 24 and 25, and send this detection signal to a preamplifier via a lead wire 29. 4 and measure it as flow velocity or flow rate.
然るに、渦発生体1は流れに対向する第1表面
11が凹面11Aとして形成されているから、隅
角部14が非常に鋭角となり、流体の剥離点を固
定できると共に該凹面11Aに当つた流体の剥離
が一層確実かつ強力となり、カルマン渦の強度を
増加させることができる。また、凹面11Aの最
奥部に第1の導圧孔15が開口しているから、上
流から下流に向う流体流はそのまま導圧孔15か
ら吸込まれ、導圧作用を良好ならしめることがで
きると共に、第2、第3の導圧孔16,17を上
流側第2表面12A,13Aの隅角部14直下に
開口させることにより、剥離した瞬間で圧力が最
小状態となつたところに流出されることができ、
上記第1の導圧孔15との間の圧力変化を最も大
きくすることができる。 However, since the first surface 11 of the vortex generating body 1 facing the flow is formed as a concave surface 11A, the corner portion 14 becomes a very acute angle, and the separation point of the fluid can be fixed, and the fluid that hits the concave surface 11A can be fixed. The separation becomes more reliable and strong, and the strength of the Karman vortex can be increased. Further, since the first pressure guiding hole 15 is opened at the innermost part of the concave surface 11A, the fluid flow from upstream to downstream is sucked in from the pressure guiding hole 15 as it is, and a good pressure guiding effect can be achieved. At the same time, by opening the second and third pressure guiding holes 16 and 17 directly below the corner portions 14 of the upstream second surfaces 12A and 13A, the pressure is discharged to the point where the pressure is at its minimum state at the moment of separation. can be done,
The pressure change between the first pressure guiding hole 15 and the first pressure guiding hole 15 can be maximized.
なお、実験の結果第1の導圧孔15に比較し、
第2、第3の導圧孔16,17を流体流中で距離
δだけ上流に位置させることにより第1の導圧孔
15から流入し、第2、第3の導圧孔16,17
から流出する流れが規則正しく交互に変化し、ス
トローハル数の安定な領域が大きく、低流量域ま
で器差特性を改善させた流量計を得ることができ
た。 In addition, as a result of the experiment, compared to the first pressure guiding hole 15,
By locating the second and third pressure-pulling holes 16 and 17 upstream by a distance δ in the fluid flow, the pressure flows from the first pressure-pulling hole 15 and flows into the second and third pressure-pulling holes 16 and 17.
We were able to obtain a flowmeter in which the flow flowing out from the flowmeter changes regularly and alternately, the Strouhal number has a large stable region, and the instrumental error characteristics are improved down to the low flow rate region.
なお、本考案の実施例においては渦発生体1の
第2表面12,13を上流側第2表面12A,1
3Aと下流側第2表面12B,13Bとから形成
するものとして述べたが、このような形状に限定
されるものではなく、流体流と平行な上流側第2
表面12A,13Aを省略した三角形状の渦発生
体としてもよいものである。この場合には本実施
例のものと比較して隅角部14をさらに鋭角に形
成することができる。また、工作上の問題から内
筒22を環状溝23。垂直溝24,25とから形
成し、該各垂直溝24に渦検出素子27,28を
設けるものとして述べたが、要は第1の導圧孔1
5と第2、第3の導圧孔16,17とをそれぞれ
流路により連通し、該各流路の途中に渦検出素子
27,28を設ければよいものである。 In the embodiment of the present invention, the second surfaces 12 and 13 of the vortex generator 1 are the upstream second surfaces 12A and 1
3A and the downstream second surfaces 12B and 13B, but the shape is not limited to this, and the upstream second surface parallel to the fluid flow is
It is also possible to use a triangular vortex generator with the surfaces 12A and 13A omitted. In this case, the corner portions 14 can be formed to have even more acute angles than those of this embodiment. In addition, due to manufacturing problems, the inner cylinder 22 has an annular groove 23. Although it has been described that the vertical grooves 24 and 25 are formed and the vortex detection elements 27 and 28 are provided in each of the vertical grooves 24, the point is that the first pressure guiding hole 1
5 and the second and third pressure guiding holes 16 and 17 through a flow path, respectively, and vortex detection elements 27 and 28 are provided in the middle of each flow path.
本考案の流速・流量検出装置は以上詳細に述べ
た如くであつて下記各項のような効果を奏する。 The flow rate/flow rate detection device of the present invention is as described in detail above, and has the following effects.
上流側に面する第1表面を凹面に形成したか
ら、隅角部が鋭角となり、流体の剥離点を固定
することができると共に、剥離が確実となり、
渦の強度を高めることができる。 Since the first surface facing the upstream side is formed into a concave surface, the corner portion becomes an acute angle, and the separation point of the fluid can be fixed, and separation is ensured.
The strength of the vortex can be increased.
第1の導圧孔を第1表面の凹面最奥部に開口
させ、第2、第3の導圧孔を第2表面、特に第
2表面の隅角部直下に開口させたから、第1の
導圧孔と第2、第3の導圧孔との間の圧力変化
を大きくすることができ、高レベルな渦信号を
得ることができる。 Since the first pressure-conducting hole is opened at the innermost part of the concave surface of the first surface, and the second and third pressure-conducting holes are opened at the second surface, especially directly under the corner of the second surface, the first It is possible to increase the pressure change between the pressure guiding hole and the second and third pressure guiding holes, and it is possible to obtain a high level vortex signal.
第1の導圧孔の開口位置に比較し、第2、第
3の導圧孔の開口位置の方を上流側とすれば、
前記各項の効果はさらに大である。 If the opening positions of the second and third pressure holes are on the upstream side compared to the opening position of the first pressure hole,
The effects of each of the above items are even greater.
第1図は本考案に係る流速・流量計測装置を示
す一部を破断にした全体図、第2図は第1図中の
−矢示方向断面図、第3図は渦発生体の外観
斜視図、第4図は渦発生体内に設けられる内筒の
外観斜視図、第5図は第4図においてストレーナ
を除去した状態を示す斜視図である。
1……渦発生体、2……本体、11……第1表
面、11A……凹面、12,13……第2表面、
12A,13A……上流側第2表面、12B,1
3B……下流側第2表面、14……隅角部、1
5,16,17……第1〜3の導圧孔、18,1
9,20……連通路、21……円筒部、22……
内筒、23……環状溝、24,25……垂直溝、
26……ストレーナ、27,28……渦検出部。
Fig. 1 is a partially cutaway overall view of the flow rate/flow measuring device according to the present invention, Fig. 2 is a cross-sectional view in the direction of the − arrow in Fig. 1, and Fig. 3 is a perspective view of the appearance of the vortex generator. 4 is an external perspective view of the inner cylinder provided in the vortex generator, and FIG. 5 is a perspective view showing a state in which the strainer is removed from FIG. 4. 1... Vortex generator, 2... Main body, 11... First surface, 11A... Concave surface, 12, 13... Second surface,
12A, 13A... Upstream second surface, 12B, 1
3B...Downstream second surface, 14...Corner part, 1
5, 16, 17... 1st to 3rd pressure guiding holes, 18, 1
9, 20...Communication path, 21...Cylindrical portion, 22...
Inner cylinder, 23... annular groove, 24, 25... vertical groove,
26... Strainer, 27, 28... Vortex detection section.
Claims (1)
生体を設け、該渦発生体は流体流中で上流側に
面する第1表面と、該第1表面から下流に向う
に従つて横方向断面が減小する第2表面とを有
する流速・流量計測装置において、前記第1表
面は流れに対向する面を凹面に形成し、該凹面
のほぼ最奥部には第1の導圧孔を開口し、また
前記第2表面には第2、第3の導圧孔を開口
し、前記第1の導圧孔と第2、第3の導圧孔と
をそれぞれ流路により接続し、該各流路の途中
には渦検出素子を設けたことを特徴とする流
速・流量計測装置。 (2) 前記第1の導圧孔に比較し、第2、第3の導
圧孔を流体流中で上流側に開口させてなる実用
新案登録請求の範囲(1)項記載の流速・流量計測
装置。 (3) 前記第2表面を流体流と平行な上流側第2表
面と、該上流側第2表面と連続し下流に向うに
従つて横方向断面が減小する下流側第2表面と
から形成し、前記第1表面と上流側第2表面と
の交点を隅角部となし、かつ前記第2、第3の
導圧孔を前記上流側第2表面に開口してなる実
用新案登録請求の範囲(1)項記載の流速・流量計
測装置。[Claims for Utility Model Registration] (1) A columnar vortex generator is provided in the middle of the pipe through which the fluid to be measured flows, and the vortex generator has a first surface facing upstream in the fluid flow, In a flow velocity/flow rate measuring device having a second surface whose lateral cross section decreases downstream from the first surface, the first surface has a concave surface facing the flow, and the first surface has a concave surface facing the flow, and the first surface has a concave surface facing the flow, and the first surface has a concave surface facing the flow. A first pressure guiding hole is opened in the innermost part, and second and third pressure guiding holes are opened in the second surface, and the first pressure guiding hole and the second and third pressure guiding holes are connected to each other. 1. A flow rate/flow rate measuring device, characterized in that the pressure holes are connected to each other by a flow path, and a vortex detection element is provided in the middle of each flow path. (2) The flow rate/flow rate according to claim (1) of the utility model registration claim, in which the second and third pressure holes are opened on the upstream side in the fluid flow compared to the first pressure hole. Measuring device. (3) The second surface is formed from an upstream second surface that is parallel to the fluid flow, and a downstream second surface that is continuous with the upstream second surface and whose lateral cross section decreases downstream. and the intersection of the first surface and the upstream second surface is a corner part, and the second and third pressure guiding holes are opened in the upstream second surface. Flow rate/flow measuring device described in scope (1).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP594781U JPS6143205Y2 (en) | 1981-01-20 | 1981-01-20 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP594781U JPS6143205Y2 (en) | 1981-01-20 | 1981-01-20 |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS57120256U JPS57120256U (en) | 1982-07-26 |
JPS6143205Y2 true JPS6143205Y2 (en) | 1986-12-06 |
Family
ID=29804287
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP594781U Expired JPS6143205Y2 (en) | 1981-01-20 | 1981-01-20 |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS6143205Y2 (en) |
-
1981
- 1981-01-20 JP JP594781U patent/JPS6143205Y2/ja not_active Expired
Also Published As
Publication number | Publication date |
---|---|
JPS57120256U (en) | 1982-07-26 |
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