JPH0823506B2 - Vortex flowmeter - Google Patents
Vortex flowmeterInfo
- Publication number
- JPH0823506B2 JPH0823506B2 JP1106656A JP10665689A JPH0823506B2 JP H0823506 B2 JPH0823506 B2 JP H0823506B2 JP 1106656 A JP1106656 A JP 1106656A JP 10665689 A JP10665689 A JP 10665689A JP H0823506 B2 JPH0823506 B2 JP H0823506B2
- Authority
- JP
- Japan
- Prior art keywords
- vortex
- fluid
- conduit
- flow
- 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.)
- Expired - Fee Related
Links
Landscapes
- Details Of Flowmeters (AREA)
Description
【発明の詳細な説明】 〔産業上の利用分野〕 この発明は渦流量計、特に内燃機関に用いられる渦流
量計に関するものである。The present invention relates to a vortex flowmeter, and more particularly to a vortex flowmeter used in an internal combustion engine.
一般に、内燃機関に渦流量計を用いる場合には、例え
ば特公昭62−26686号公報や特開昭58−21517号公報に示
されるように、渦流量計が必らず機関の吸入空気の汚れ
を除去するエアクリーナの後流に設けられていた。Generally, when an vortex flowmeter is used in an internal combustion engine, as shown in, for example, Japanese Patent Publication No. 62-26686 and Japanese Unexamined Patent Publication No. 58-21517, the vortex flowmeter does not necessarily pollute the intake air of the engine. It was installed in the downstream of the air cleaner that removes.
ところで、流量計は被測定流体の流れの安定性が得ら
れなければ、測定精度の低下はもちろんのこと、測定そ
のものも成立しなくなる。渦流量計を内燃機関に用いた
場合には上記のようにエアクリーナの後流に設けられる
ので、流体の流れに十分安定性を持たせるだけの寸法が
確保できない場合が多く、大流量時に偏流さ乱れが極め
て大きくなり、公知の整流機構を用いた場合には渦発生
さえも阻害されることがあった。By the way, if the flowmeter cannot obtain the stability of the flow of the fluid to be measured, not only the measurement accuracy will be deteriorated, but also the measurement itself will not be established. When a vortex flowmeter is used in an internal combustion engine, it is installed in the wake of the air cleaner as described above, so it is often not possible to secure a dimension that provides sufficient stability for the fluid flow. The turbulence becomes extremely large, and even when a known rectifying mechanism is used, even vortex generation may be hindered.
第3図は従来の渦流量計を機関のエアクリーナの後流
に設けた場合の断面図を示し、1は渦流量計で、被測定
流体が流通する断面四辺形の導管11と、導管11内に設け
られてカルマン渦を発生する第1の渦発生柱12と、同じ
く導管11内に第1の渦発生柱12より下流側に設けられて
カルマン渦を発生し、かつ渦検出導圧口を有する第2の
渦発生柱13と、導管11の流体流入側に設けられたハニカ
ム整流器14及び導管11の外側に設けられた制御回路15と
から成る。2はエアクリーナで、流体流入口を有する上
流カバー21と、導管11が接続された流出口を有する下流
カバー22及び上流カバー21と下流カバー22の間に設けら
れたダスト除去エレメント23からなる。3は導管11の下
流側に接続され、流体を図示しないスロットルバルブを
介して機関に導く吸気管である。FIG. 3 is a cross-sectional view of a conventional vortex flowmeter installed downstream of an air cleaner of an engine. Reference numeral 1 is a vortex flowmeter, which is a quadrilateral conduit 11 through which a fluid to be measured flows and the inside of the conduit 11. And a first vortex generating column 12 for generating a Karman vortex, and a Karman vortex for generating a Karman vortex in the conduit 11 downstream of the first vortex generating column 12 The second vortex generating column 13 has, a honeycomb rectifier 14 provided on the fluid inflow side of the conduit 11, and a control circuit 15 provided outside the conduit 11. An air cleaner 2 is composed of an upstream cover 21 having a fluid inlet, a downstream cover 22 having an outlet to which the conduit 11 is connected, and a dust removing element 23 provided between the upstream cover 21 and the downstream cover 22. Reference numeral 3 is an intake pipe that is connected to the downstream side of the conduit 11 and guides the fluid to the engine through a throttle valve (not shown).
上記構成において、被測定流体即ち空気の流れはエア
クリーナ2の上流カバー21から流線FINで流入し、下流
カバー22内を流線F1〜F4に示すように流れて渦流量計1
の入口に達する。流体は抵抗の小さい所を選んで流れる
ため、一般的に流速が最も速いのは流線F2であり、次に
流線F1,F3となり、最も遅いのが流線F4であり、流線F4
の流速は極めて不安定である。渦流量計1の入口に達し
た流体は流線FOUTに沿って吸気管3へ流出する。In the above configuration, the flow of the fluid to be measured, that is, the air flows from the upstream cover 21 of the air cleaner 2 along the streamline F IN and flows in the downstream cover 22 as shown by the streamlines F 1 to F 4 , and the vortex flowmeter 1
Reach the entrance. Since the fluid flows by selecting a place with a small resistance, the flow velocity is generally fastest in the streamline F 2 , then streamlines F 1 and F 3 , and the slowest is the flowline F 4 . Streamline F 4
The flow velocity of is extremely unstable. The fluid reaching the inlet of the vortex flowmeter 1 flows out to the intake pipe 3 along the streamline F OUT .
次に、エアクリーナ2内で流線F1〜F4に沿って流れた
流体が渦流量計1内でどのような流速分布で流れるかに
ついて説明する。第4図はエアクリーナ2の出口側と渦
流量計1の上流側とを部分拡大した断面図であり、11a
は導管11の全周に設けられたベルマウス部で、ハニカム
整流器14の後流に設けられている。従って、ハニカム整
流器14の直前に達した流線F1〜F4は引き続き破線で示す
方向に流れようとするが、ハニカム整流器14により矯正
されて実線方向に流れる。次に、流線F1,F3は一番速い
流線F2の速度に近づくようにベルマウス部11aで増速さ
れる。従って、いま流線F4がないとすると、第1の渦発
生柱12の直前における導管11内の流速分布は実線vLに示
すように比較的均一化された状態となるが、実際には流
線F4が存在するので流線F3が押し流されてベルマウス部
11a付近の流速が減少し、流速分布は破線vL′に示すよ
うに歪んだものとなる。このような流速分布のときに発
生した渦は、渦の強さが変動し、時々消滅する。この状
態を第5図に示す。第5図(a)に示すVCは導管11内に
発生した渦柱の中心即ち渦糸の位置を示すものであり、
また第5図(b)に示すV0は渦の強さ即ち渦圧力を示
す。時間Tが右から左へ経過する間において、渦はV1〜
V6の6個発生したとする。渦V1では渦糸のゆがみはまだ
少ないが、渦V2〜V4と進むにつれてゆがみが大きくな
り、やがて渦V5では遂に渦糸が切れる。この間の渦の強
さV0は徐々に小さくなり、渦糸が切れる渦V5ではV0は零
となる。即ち、渦V5は実質的には存在しない。渦糸が切
れた後、渦の強さV0がやや小さい渦V6が発生し、徐々に
強くなる。しかし、再び渦V1〜V4の経過をたどって渦が
消滅する。Next, the flow velocity distribution of the fluid flowing along the streamlines F 1 to F 4 in the air cleaner 2 in the vortex flowmeter 1 will be described. FIG. 4 is a partially enlarged sectional view of the outlet side of the air cleaner 2 and the upstream side of the vortex flowmeter 1.
Is a bell mouth portion provided all around the conduit 11, and is provided downstream of the honeycomb rectifier 14. Therefore, the streamlines F 1 to F 4 reaching immediately before the honeycomb rectifier 14 continue to flow in the direction indicated by the broken line, but are corrected by the honeycomb rectifier 14 and flow in the solid line direction. Next, the streamlines F 1 and F 3 are accelerated by the bell mouth portion 11a so as to approach the speed of the fastest streamline F 2 . Therefore, if there is no streamline F 4 now, the flow velocity distribution in the conduit 11 immediately before the first vortex generating column 12 will be in a relatively uniform state as shown by the solid line v L , but in reality, Since streamline F 4 exists, streamline F 3 is swept away and bellmouth part
The flow velocity near 11a decreases and the flow velocity distribution becomes distorted as shown by the broken line v L ′. The vortices generated in such a flow velocity distribution change in intensity of the vortices and sometimes disappear. This state is shown in FIG. V C shown in FIG. 5 (a) indicates the center of the vortex column generated in the conduit 11, that is, the position of the vortex filament,
Further, V 0 shown in FIG. 5 (b) indicates the strength of the vortex, that is, the vortex pressure. During the passage of time T from right to left, the vortex is V 1 ~
It is assumed that 6 of V 6 are generated. In the vortex V 1 , the distortion of the vortex filament is still small, but as the vortex V 2 to V 4 progresses, the distortion becomes larger, and eventually the vortex filament is cut in the vortex V 5 . During this period, the vortex strength V 0 gradually decreases, and V 0 becomes zero in the vortex V 5 where the vortex filament is cut. That is, the vortex V 5 practically does not exist. After the vortex filament is broken, a vortex V 6 with a slightly smaller vortex strength V 0 is generated and gradually becomes stronger. However, the vortices disappear again following the course of the vortices V 1 to V 4 .
〔発明が解決しようとする課題〕 上記したように従来の渦流量計においては、間欠的に
渦が存在しなくなり、偏流や乱れが多い流体にあっては
測定精度が大きく低下し、使用不能になるという課題が
あった。[Problems to be Solved by the Invention] As described above, in the conventional vortex flowmeter, vortices do not exist intermittently, and in a fluid with a large amount of drift or turbulence, the measurement accuracy is greatly reduced, making it unusable. There was a problem of becoming.
この発明は上記のような課題を解決するために成され
たものであり、偏流や乱れが多い流体であってもその流
れを安定化し、精度が高く安定した流量計測を行うこと
ができる渦流量計を得ることを目的とする。The present invention has been made to solve the above problems, and even for a fluid with a large amount of uneven flow or turbulence, the flow is stabilized and the vortex flow rate is capable of performing highly accurate and stable flow rate measurement. The purpose is to obtain a total.
この発明に係る渦流量計は、導管の流体流入側端部に
形成され、流体の絞り作用を行う第1の絞り部と、導管
の第1の絞り部の下流に設けられ、流体の整流作用を行
う整流器と、整流器の下流でかつ渦発生柱の上流の導管
に設けられ、流体の絞り作用を行う第2の絞り部を備
え、上記第1の絞り部の入口と出口の寸法比が、上記渦
発生柱と平行方向で1.1〜1.5:1、直角方向で1.2〜1.5:1
であるものである。A vortex flowmeter according to the present invention is provided at a fluid inlet side end portion of a conduit, is provided with a first throttle portion that performs a fluid throttle action, and is provided downstream of the first throttle portion of the conduit, and has a flow rectifying action. And a second throttle portion provided in a conduit downstream of the rectifier and upstream of the vortex generating column and performing a fluid throttle action, and the dimensional ratio of the inlet and the outlet of the first throttle portion is 1.1 to 1.5: 1 in the direction parallel to the vortex generating column, 1.2 to 1.5: 1 in the direction perpendicular to it
Is what is.
この発明における第1の絞り部は、偏流の流速を中心
流の流速に近づけるとともに、偏流や乱流を矯正して正
常流を増速させるようにする。The first throttle portion in the present invention makes the flow velocity of the non-uniform flow close to the flow velocity of the central flow and corrects the non-uniform flow and the turbulent flow to accelerate the normal flow.
以下、この発明の実施例を図面とともに説明する。第
1図はこの実施例による渦流量計41を内燃機関に搭載
し、エアクリーナ2と吸気管3との間に接続した状態の
断面図である。11bは導管11のハニカム整流器14より上
流側に即ちエアクリーナ2内に突出して設けられた断面
四辺形のファンネル部(第1の絞り部)で、ベルマウス
部(第2の絞り部)11aと同様に導管11の入口全周に設
けられる。渦流量計41の他の構成は、第3図に示す従来
の渦流量計1と同様である。Embodiments of the present invention will be described below with reference to the drawings. FIG. 1 is a sectional view showing a state in which the vortex flowmeter 41 according to this embodiment is mounted on an internal combustion engine and is connected between the air cleaner 2 and the intake pipe 3. Reference numeral 11b denotes a funnel portion (first throttle portion) having a quadrangular cross section, which is provided on the upstream side of the honeycomb rectifier 14 of the conduit 11, that is, protruding into the air cleaner 2, and is similar to the bell mouth portion (second throttle portion) 11a. Is provided all around the inlet of the conduit 11. The other structure of the vortex flowmeter 41 is the same as that of the conventional vortex flowmeter 1 shown in FIG.
上記構成において、流体は従来同様にエアクリーナ2
を流れ、導管11のファンネル部11bに達するが、このう
ち流線F1〜F3に沿った流体はファンネル部11bを通過し
てハニカム整流器14に達し、このハニカム整流器14によ
り流れる方向を矯正され、ベルマウス部11aを通過す
る。この過程で流線F1はファンネル部11bで絞られるた
め、ハニカム整流器14の直前の流速が流線F2の流速に従
来より近づく。又、流線F4は従来では流線F3を押し流し
ていたが、ファンネル部11bの絞り効果により流線F3を
増速する方向に矯正される。この結果、第1の渦発生柱
12の直前の導管11内の流速分布vLは均一になる。このた
め、第2図(a),(b)に示すように、渦糸位置VCと
渦強さVOが時間Tの経過において極めて安定して渦が正
常に発生し、計測精度が向上する。又、ファンネル部11
bは導管11の全周に設けられているため、第1の渦発生
柱12に対し直交する流速分布も均一化され、渦発生がよ
り安定化する。ここで、ファンネル部11bの絞り率即ち
ファンネル部11bの入口と出口の寸法比を、渦発生柱12
と平行方向で1.1〜1.5:1、直角方向で1.2〜1.5:1とする
ことにより、より安定性に優れたものが得られる。In the above configuration, the fluid is the same as in the conventional air cleaner 2.
Flow, but reaches the funnel portion 11b of the conduit 11, the fluid along these streamlines F 1 to F 3 passes through the funnel portion 11b reaches a honeycomb rectifier 14, it is corrected to the direction of flow by the honeycomb rectifier 14 , Passes through the bell mouth portion 11a. In this process, the streamline F 1 is narrowed by the funnel portion 11b, so that the flow velocity immediately before the honeycomb rectifier 14 becomes closer to the flow velocity of the flow line F 2 than before. Further, the streamline F 4 has been swept away from the streamline F 3 in the past, but is corrected in the direction in which the streamline F 3 is accelerated by the throttling effect of the funnel portion 11b. As a result, the first vortex generating column
The flow velocity distribution v L in the conduit 11 just before 12 becomes uniform. Therefore, as shown in FIGS. 2 (a) and 2 (b), the vortex filament position V C and the vortex strength V O are extremely stable and vortices are normally generated over time T, and the measurement accuracy is improved. To do. Also, the funnel section 11
Since b is provided on the entire circumference of the conduit 11, the flow velocity distribution orthogonal to the first vortex generating column 12 is also made uniform, and vortex generation is further stabilized. Here, the reduction ratio of the funnel portion 11b, that is, the dimensional ratio between the inlet and the outlet of the funnel portion 11b, is determined by
By setting 1.1 to 1.5: 1 in the parallel direction and 1.2 to 1.5: 1 in the orthogonal direction, a more stable product can be obtained.
以上のようにこの発明によれば、渦流量計の導管内の
流体流入側に整流器を設け、この整流器の上流側に第1
の絞り部を設けるとともに下流側に第2の絞り部を設
け、第1の絞り部の入口と出口の寸法比を、渦発生柱と
平行方向で1.1〜1.5:1、直角方向で1.2〜1.5:1とするこ
とにより、渦流量計に流入する流体のうちの偏流や乱流
は第1の絞り部により矯正されて流速が増大し、流速分
布が均一化される。このため、流体の流れが安定して渦
が正常に発生し、流量測定精度を向上することができ
る。As described above, according to the present invention, the rectifier is provided on the fluid inflow side of the conduit of the vortex flowmeter, and the first rectifier is provided on the upstream side of the rectifier.
And the second throttle on the downstream side, and the dimensional ratio of the inlet to the outlet of the first throttle is 1.1 to 1.5: 1 in the direction parallel to the vortex generating column and 1.2 to 1.5 in the right angle direction. By setting the ratio to 1 :, the drift or turbulence of the fluid flowing into the vortex flowmeter is corrected by the first throttle portion, the flow velocity is increased, and the flow velocity distribution is made uniform. For this reason, the flow of the fluid is stable and the vortex is normally generated, and the flow rate measurement accuracy can be improved.
第1図はこの発明による渦流量計を内燃機関のエアクリ
ーナに接続した状態の断面図、第2図(a),(b)は
この発明による渦流量計の渦発生状態を示す図、第3図
は従来の渦流量計をエアクリーナに接続した状態の断面
図、第4図は第3図の部分拡大図、第5図(a),
(b)は従来の渦流量計の渦発生状態を示す図である。 2……エアクリーナ、3……吸気管、11……導管、11a
……ベルマウス部、11b……ファンネル部、12,13……渦
発生柱、14……ハイカム整流器、41……渦流量計。 なお、図中同一符号は同一又は相当部分を示す。FIG. 1 is a cross-sectional view of a vortex flowmeter according to the present invention connected to an air cleaner of an internal combustion engine, and FIGS. 2A and 2B are views showing vortex generation states of the vortex flowmeter according to the present invention. The figure is a cross-sectional view of a conventional vortex flowmeter connected to an air cleaner. Fig. 4 is a partially enlarged view of Fig. 3, Fig. 5 (a),
(B) is a figure which shows the vortex generation state of the conventional vortex flowmeter. 2 ... Air cleaner, 3 ... Intake pipe, 11 ... Conduit, 11a
…… Bell mouth part, 11b …… Funnel part, 12,13 …… Vortex generating column, 14 …… High cam rectifier, 41 …… Vortex flow meter. The same reference numerals in the drawings indicate the same or corresponding parts.
Claims (1)
生する渦発生柱を有する渦流量計において、導管の流体
流入側端部に形成され、流体の絞り作用を行う第1の絞
り部と、導管における第1の絞り部の下流に設けられ、
流体の整流作用を行う整流器と、この整流器の下流でか
つ渦発生柱の上流側における上記導管に形成され、流体
の絞り作用を行う第2の絞り部を備え、上記第1の絞り
部の入口と出口の寸法比が、上記渦発生柱と平行方向で
1.1〜1.5:1、直角方向で1.2〜1.5:1であることを特徴と
する渦流量計。1. A vortex flowmeter having a vortex generating column for generating a Karman vortex in a conduit through which a fluid to be measured passes, the first squeezing portion being formed at a fluid inflow end of the conduit and performing a squeezing action of the fluid. And downstream of the first throttle portion of the conduit,
An inlet of the first throttle portion, which includes a rectifier for rectifying the fluid and a second throttle portion formed in the conduit downstream of the rectifier and on the upstream side of the vortex generating column for performing the fluid throttle operation. And the dimension ratio of the outlet is parallel to the vortex generating column above.
A vortex flowmeter characterized by 1.1 to 1.5: 1 and 1.2 to 1.5: 1 in the right angle direction.
Priority Applications (6)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1106656A JPH0823506B2 (en) | 1989-04-25 | 1989-04-25 | Vortex flowmeter |
| DE4013351A DE4013351A1 (en) | 1989-04-25 | 1990-04-23 | Vortex flow meter |
| AU53826/90A AU620980B2 (en) | 1989-04-25 | 1990-04-24 | Vortex flowmeter |
| US07/514,443 US5029465A (en) | 1989-04-25 | 1990-04-25 | Vortex flowmeter |
| KR1019900005829A KR900016737A (en) | 1989-04-25 | 1990-04-25 | Vortex flowmeter |
| KR2019930024454U KR940007792Y1 (en) | 1989-04-25 | 1993-11-19 | Fluid metering device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1106656A JPH0823506B2 (en) | 1989-04-25 | 1989-04-25 | Vortex flowmeter |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH02284026A JPH02284026A (en) | 1990-11-21 |
| JPH0823506B2 true JPH0823506B2 (en) | 1996-03-06 |
Family
ID=14439146
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1106656A Expired - Fee Related JPH0823506B2 (en) | 1989-04-25 | 1989-04-25 | Vortex flowmeter |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0823506B2 (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US10208717B2 (en) | 2016-07-11 | 2019-02-19 | Komatsu Ltd. | Intake apparatus and dump truck |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5540353U (en) * | 1978-09-08 | 1980-03-15 | ||
| JPS5861411A (en) * | 1981-10-08 | 1983-04-12 | Nippon Denso Co Ltd | Measuring device for flow rate of gas |
-
1989
- 1989-04-25 JP JP1106656A patent/JPH0823506B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| JPH02284026A (en) | 1990-11-21 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| LAPS | Cancellation because of no payment of annual fees |