JPH0363686B2 - - Google Patents
Info
- Publication number
- JPH0363686B2 JPH0363686B2 JP2990483A JP2990483A JPH0363686B2 JP H0363686 B2 JPH0363686 B2 JP H0363686B2 JP 2990483 A JP2990483 A JP 2990483A JP 2990483 A JP2990483 A JP 2990483A JP H0363686 B2 JPH0363686 B2 JP H0363686B2
- Authority
- JP
- Japan
- Prior art keywords
- gas flow
- point
- gas
- flow path
- 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
- 238000001514 detection method Methods 0.000 description 7
- 230000033001 locomotion Effects 0.000 description 4
- 238000000691 measurement method Methods 0.000 description 3
- 238000005259 measurement Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 230000010349 pulsation Effects 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
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
- G01F1/704—Measuring the volume flow or mass flow of fluid or fluent solid material wherein the fluid passes through a meter in a continuous flow using marked regions or existing inhomogeneities within the fluid stream, e.g. statistically occurring variations in a fluid parameter
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Measuring Volume Flow (AREA)
Description
【発明の詳細な説明】
本発明は、ガス、特に家庭用ガスの消費量を測
定するガス流量の測定方法に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a gas flow rate measurement method for measuring the consumption of gas, particularly household gas.
従来、各家庭のガスの消費量を測定するガスメ
ータのガス流量の測定方法は、ガスの圧力によつ
て内蔵された運動子、例えば回転子、ますを駆動
し、この運動子の運動数で通過全流量を求めるよ
うになつている。そして、この運動子はますに相
当する計量室を形成しているため、小型化には限
度が有り、小型化のため該運動子により形成され
るますを小さくすること、この運動子は高速運動
することが要求され、大変圧力損失の大きいもの
となつてしまい、その結果実用的小型化がある程
度に限らるという欠点を有している。 Conventionally, the gas flow rate measurement method for gas meters used to measure gas consumption in each household uses gas pressure to drive a built-in motion element, such as a rotor, and the number of motions of this motion element is used to measure the gas flow rate. It is now possible to find the total flow rate. Since this mover forms a measuring chamber equivalent to a square, there is a limit to its miniaturization. This results in a very large pressure loss, which has the disadvantage that practical miniaturization is limited to a certain extent.
本発明は、上記欠点にかんがみなされたもの
で、従来のガス流量をガス圧によつて駆動される
運動子を介して測定するのとは逆に、ガス流自体
に間欠的な衝撃を加え、この衝撃によるガス流の
乱れがガス流路の一定距離を移動したことにより
ガス流量の測定を行なうことで、圧力損失を高め
ることなく測定位置を小型化できるガス流量の測
定方法を提案するものである。 The present invention has been made in view of the above-mentioned drawbacks, and, contrary to the conventional method of measuring the gas flow rate through an agitator driven by gas pressure, the present invention applies intermittent shocks to the gas flow itself. This paper proposes a method for measuring gas flow rate that can reduce the size of the measurement location without increasing pressure loss by measuring the gas flow rate when the gas flow disturbance caused by this impact moves a certain distance in the gas flow path. be.
以下、本発明を添付図面に示す装置例にもとず
いて詳細に説明する。 DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described in detail below based on an example of the apparatus shown in the accompanying drawings.
図中、1がガス流路で一端側(図右側)よりガ
スが流入し、他端側(図左側)に流出するもの
で、具体的には家庭用ガス配管の一部に簡単に設
置することができる。 In the figure, 1 is a gas flow path where gas flows in from one end (right side of the figure) and flows out to the other end (left side of the figure). Specifically, it can be easily installed in a part of household gas piping. be able to.
上記ガス流路1の所定位置A点には、該ガス流
路1内のガス流に定時間間隔で衝撃を加えガス流
に間欠的乱れを生ぜしめる衝撃装置2が配され
る。この衝撃装置2によるガス流の乱れは、ガス
流路内A点を連続的に通過するガス流に間欠的に
圧力差を持たせガス流に脈動を加えるものと、同
じくA点を連続的に通過するガス流に間欠的にう
ず流を発生させるものが有る。具体的には図示の
ごとく、ガス流路1内にガス流と平行な板3を配
し、この板3をガス流の流れ方向と直角方向の軸
を中心として間欠往復回動すると、ガス流路1の
流路面積が間欠的に変動しガス流を脈動すること
ができ、また、図示はしていないが板3に代えオ
リフイスを設けこのオリフイス径を間欠的に変更
してもガス流を脈動させることができる。また、
この板3はガス流中の支障物をともなつているた
め、この板3の下流側にはカルマンうず列が生
じ、このうず流は板3の間欠回動によりそのうず
量を間欠的に変更することができ、また、図示は
していないが、板3に代え該ガス流路1内に間欠
的に出入する棒を配するとうず流部を間欠的に有
したガス流を有することができる。さらにまた、
この衝撃装置2は、A点で気体を間欠的に噴射す
る等、A点で与えられたガス流への影響がB点で
検出できるものであればよい。 At a predetermined point A in the gas flow path 1, an impact device 2 is arranged which applies an impact to the gas flow in the gas flow path 1 at regular time intervals to cause intermittent turbulence in the gas flow. The turbulence of the gas flow caused by this impact device 2 can be caused by intermittently creating a pressure difference in the gas flow that continuously passes through point A in the gas flow path and adding pulsations to the gas flow. Some gas flows intermittently generate eddy flows. Specifically, as shown in the figure, a plate 3 parallel to the gas flow is arranged in the gas flow path 1, and when this plate 3 is intermittently rotated back and forth about an axis perpendicular to the flow direction of the gas flow, the gas flow is The flow area of channel 1 can be varied intermittently to cause the gas flow to pulsate, and although not shown, an orifice is provided in place of plate 3, and even if the orifice diameter is intermittently changed, the gas flow cannot be controlled. It can be made to pulsate. Also,
Since this plate 3 is accompanied by an obstacle in the gas flow, a Karman vortex train is generated on the downstream side of this plate 3, and the amount of vortex is intermittently changed by the intermittent rotation of the plate 3. Although not shown, if a rod that intermittently goes in and out of the gas flow path 1 is placed in place of the plate 3, it is possible to have a gas flow that has intermittently whirlpool portions. . Furthermore,
This impact device 2 may be of any type as long as the influence on the gas flow given at point A can be detected at point B, such as by intermittently injecting gas at point A.
上記ガス流路1のA点より下流側のB点には、
A点よりB点に流れてきたガス流の圧力変動また
はうず流の乱れを検出する検出装置4が配され
る。この検出装置4は圧力変動を検出するものと
しては従来公知な感圧素子5が使用でき、またう
ず流を検出するものとしては感圧素子5を振動や
ねじれにより電気抵抗値を変える歪みゲージに代
えるか、あるいは該感圧素子5をアンテナに代え
うず流の歳差運動による所定巾の周波数を読み取
つてもよい。 At point B on the downstream side of point A in the gas flow path 1,
A detection device 4 is arranged to detect pressure fluctuations in the gas flow flowing from point A to point B or turbulence in the eddy flow. This detection device 4 can use a conventionally known pressure sensing element 5 to detect pressure fluctuations, and can use a strain gauge that changes the electrical resistance value by vibration or twisting to detect eddy flow. Alternatively, the pressure sensitive element 5 may be replaced with an antenna to read frequencies within a predetermined range due to the precession of the eddy current.
上記検出装置4は、A点で衝撃を加えられたガ
ス流部がB点まで流れたことを検出するためのも
のであり、そのため、A点とB点とは衝撃装置2
によるガス流の乱れたガスが流れずに停留してい
ても伝わるおそれがない距離とし、かつ、ガス流
の乱れはガス流の流れにともなつて衰退するので
この衝撃衰退前の距離とすることが望ましい。な
お、この検出装置4は、上記のごときガス流の乱
れを、ある価の範囲内で検出すると後述制御盤6
において一パルスの信号を出力するようになすこ
とにより誤動作を防ぐことができるのは無論であ
る。 The above-mentioned detection device 4 is for detecting that the gas flow portion subjected to impact at point A has flowed to point B. Therefore, point A and point B are connected to the impact device 2.
The distance should be set so that there is no risk of the gas turbulent in the gas flow being transmitted even if the gas is stationary without flowing, and since the turbulence in the gas flow will decline as the gas flow continues, the distance should be set at the distance before this impact decays. is desirable. Note that when this detection device 4 detects the above-mentioned disturbance in the gas flow within a certain value range, it will be activated by a control panel 6, which will be described later.
It goes without saying that malfunctions can be prevented by outputting a single pulse signal.
そして、上記検出装置4でガス流の乱れを検出
すると、制御盤6でガス流がA点B点間の所要時
間を換算するとともにガス流量を演算し表示部7
に表示される。 When the detection device 4 detects disturbance in the gas flow, the control panel 6 converts the time required for the gas flow to travel between points A and B, calculates the gas flow rate, and displays the information on the display 7.
will be displayed.
すなわち、ガス流路1内を流れるガス流は、A
点で乱れを行し、このガス流の乱れ部がガス流と
ガス流路1のA点とB点間の距離分をますとして
その所要時間を測定すれば、ガス流路1の通過全
流量が求められるものである。 That is, the gas flow flowing in the gas flow path 1 is A
If turbulence is caused at a point, and the time required for this turbulent part of the gas flow is calculated by dividing the distance between the gas flow and points A and B in gas flow path 1, then the total flow rate passing through gas flow path 1 can be calculated as follows: is what is required.
本発明ガス流量の測定方法は上記のごときであ
るので、衝撃装置2と検出装置4と制御盤6のみ
でガス流量を測定することができ、かつ、これら
はガス圧に駆動されるものでないから小型化が可
能である。特に、衝撃装置2によるガス流の脈動
化またはうず流発生によつても圧力損失が当然生
ずるか、この圧力損失はガス圧により運動子を駆
動する従来例とは比較にならない程小さいため、
圧力損失を高めることなく装置を小型化できるも
のである。 Since the gas flow rate measurement method of the present invention is as described above, the gas flow rate can be measured only with the impact device 2, the detection device 4, and the control panel 6, and these are not driven by gas pressure. Miniaturization is possible. In particular, pressure loss naturally occurs due to pulsation of the gas flow or generation of eddy flow by the impact device 2, or this pressure loss is much smaller than in the conventional example in which the motion element is driven by gas pressure.
The device can be made smaller without increasing pressure loss.
また、本発明は、ガス流量を電気的信号として
読み取るため、電力消費をともなうが、測定結果
を遠隔表示したり、測定値の集計をオンライン化
することも可能であるため、電力消費をおぎなう
経済的有利性をも有するものである。 Furthermore, since the present invention reads the gas flow rate as an electrical signal, it consumes power, but it is also possible to display the measurement results remotely and aggregate the measured values online, so it is economical to reduce power consumption. It also has certain advantages.
図面は本発明ガス流量の測定方法を用いた装置
例一部断面正面図である。
1〜ガス流路、2〜衝撃装置、3〜板、4〜検
出装置、5〜感圧素子、6〜制御盤。
The drawing is a partially sectional front view of an example of an apparatus using the method for measuring gas flow rate of the present invention. 1 - Gas flow path, 2 - Impact device, 3 - Plate, 4 - Detection device, 5 - Pressure sensitive element, 6 - Control panel.
Claims (1)
ガス流に定時間間隔で衝撃を加えガス流に間欠的
乱れを生ぜしめ、該ガス流路のA点より下流側の
B点で、A点よりB点に流れてきたガス流の乱れ
を検出し、A点よりB点にいたつた所要時間によ
り流速を演算してガス流量を測定するようになし
たことを特徴とするガス流量の測定方法。1. At a predetermined point A in the gas flow path, impact is applied to the gas flow in the gas flow path at regular intervals to cause intermittent turbulence in the gas flow, and at a point B downstream from point A in the gas flow path. The gas flow rate is measured by detecting turbulence in the gas flow flowing from point A to point B, and calculating the flow velocity based on the time required to reach point B from point A. How to measure flow rate.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2990483A JPS59155717A (en) | 1983-02-24 | 1983-02-24 | Measurement of gas flow rate |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2990483A JPS59155717A (en) | 1983-02-24 | 1983-02-24 | Measurement of gas flow rate |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS59155717A JPS59155717A (en) | 1984-09-04 |
JPH0363686B2 true JPH0363686B2 (en) | 1991-10-02 |
Family
ID=12288963
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP2990483A Granted JPS59155717A (en) | 1983-02-24 | 1983-02-24 | Measurement of gas flow rate |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS59155717A (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2507791A (en) * | 2012-11-12 | 2014-05-14 | Rolls Royce Plc | Apparatus and method for measuring gas flow through a gas turbine rotary seal |
-
1983
- 1983-02-24 JP JP2990483A patent/JPS59155717A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
JPS59155717A (en) | 1984-09-04 |
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