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JPS6239941B2 - - Google Patents
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JPS6239941B2 - - Google Patents

Info

Publication number
JPS6239941B2
JPS6239941B2 JP267482A JP267482A JPS6239941B2 JP S6239941 B2 JPS6239941 B2 JP S6239941B2 JP 267482 A JP267482 A JP 267482A JP 267482 A JP267482 A JP 267482A JP S6239941 B2 JPS6239941 B2 JP S6239941B2
Authority
JP
Japan
Prior art keywords
circuit
microphone
output signal
flow velocity
gas flow
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
Application number
JP267482A
Other languages
Japanese (ja)
Other versions
JPS58120169A (en
Inventor
Takeo Murata
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
National Institute of Advanced Industrial Science and Technology AIST
Original Assignee
Agency of Industrial Science and Technology
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Agency of Industrial Science and Technology filed Critical Agency of Industrial Science and Technology
Priority to JP267482A priority Critical patent/JPS58120169A/en
Publication of JPS58120169A publication Critical patent/JPS58120169A/en
Publication of JPS6239941B2 publication Critical patent/JPS6239941B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P7/00Measuring speed by integrating acceleration

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Volume Flow (AREA)

Description

【発明の詳細な説明】 本発明は気体の流速を測定する装置に関する。
従来、気体の流速測定には主として熱式の流速
計、例えば熱線式流速計が用いられている。しか
し、熱式流速計は温度センサを必要とする。ま
た、流速の早い変化を測定するためには、温度セ
ンサの温度に対する応答性を高めなければなら
ず、このためには熱容量の小さい、従つて寸法の
微小な特殊センサーを必要とする。これらの特殊
センサーは一般に入手し難く、製作も困難であ
り、又破損しやすく、高価である。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an apparatus for measuring gas flow velocity.
Conventionally, a thermal current meter, such as a hot wire current meter, has been mainly used to measure the flow velocity of gas. However, thermal anemometers require a temperature sensor. Furthermore, in order to measure rapid changes in flow velocity, the responsiveness of the temperature sensor to temperature must be increased, and this requires a special sensor with a small heat capacity and, therefore, a small size. These specialized sensors are generally difficult to obtain, difficult to manufacture, easily damaged, and expensive.

本発明の第1の目的は温度センサーを必要とし
ない気体流速測定装置を提供することであり、第
2の目的は製作容易で、丈夫で、安価に構成でき
る気体流速測定装置を提供することである。
The first object of the present invention is to provide a gas flow rate measuring device that does not require a temperature sensor, and the second purpose is to provide a gas flow rate measuring device that is easy to manufacture, durable, and inexpensive. be.

以下、図面とともに本発明の詳細について説明
する。本発明は基本的には第1図に示すように、
マイクロホン1、積分回路2、処理回路3から構
成される。マイクロホン1は通常の音声を検出す
るための、マイクロホンの風防を除去したものが
用いられる。積分回路2は上記マイクロホンの出
力信号を積分するための電子回路で、周知の回路
が用いられる。処理回路3は積分回路2の出力信
号のパワーを検出し気体流速に相当する出力信号
を得るように構成された関数発生回路であり、具
体的には通常平方根回路で構成される。
Hereinafter, details of the present invention will be explained with reference to the drawings. The present invention is basically as shown in FIG.
It is composed of a microphone 1, an integrating circuit 2, and a processing circuit 3. The microphone 1 is a microphone with a windshield removed, which is used to detect normal voices. The integrating circuit 2 is an electronic circuit for integrating the output signal of the microphone, and a well-known circuit is used. The processing circuit 3 is a function generating circuit configured to detect the power of the output signal of the integrating circuit 2 and obtain an output signal corresponding to the gas flow velocity, and specifically, is usually configured as a square root circuit.

次に、本発明の動作について説明する。 Next, the operation of the present invention will be explained.

実験によれば、風防を除去したマイクロホンの
受音面に測定しようとする流動気体が当るように
マノクロホンを配置した場合、マイクロホンの出
力信号は流動気体の流速と流動気体の加速度の積
に極めて高い近似で比例することが明かになつ
た。故に、このマイクロホンの出力信号を積分回
路2で積分すると、流動気体の流速の2乗に極め
て高い近似で比例する信号が得られる。この信号
を処理回路3で平方根の処理を施せば、測定しよ
うとする流動気体の流速に極めて高い近似で比例
する信号を得ることができる。
According to experiments, when a manocrophon is placed so that the flowing gas to be measured hits the sound receiving surface of the microphone with the windshield removed, the output signal of the microphone is extremely high as the product of the flow velocity of the flowing gas and the acceleration of the flowing gas. It became clear that they are proportional by approximation. Therefore, when the output signal of this microphone is integrated by the integrating circuit 2, a signal that is proportional to the square of the flow velocity of the flowing gas with a very high approximation is obtained. By subjecting this signal to square root processing in the processing circuit 3, it is possible to obtain a signal that is proportional to a very high approximation to the flow velocity of the flowing gas to be measured.

次に、第2図及び第3図を用いて本発明をより
詳細に説明する。第2図は積分回路2及び処理回
路3の具体例を示しており、積分回路2は演算増
幅器4、入力抵抗5、帰還容量6で構成される。
処理回路3は入力抵抗9をもつ演算増幅器7の帰
還回路に公知の2乗回路8を用いた平方根回路で
ある。
Next, the present invention will be explained in more detail using FIGS. 2 and 3. FIG. 2 shows a specific example of the integrating circuit 2 and the processing circuit 3, and the integrating circuit 2 is composed of an operational amplifier 4, an input resistor 5, and a feedback capacitor 6.
The processing circuit 3 is a square root circuit using a known square circuit 8 as a feedback circuit of an operational amplifier 7 having an input resistor 9.

第3図イは測定しようとする気体の流速変化の
一例を示し、ロはマイクロホン1の出力信号波
形、ハは積分回路2の出力信号波形、ニは処理回
路3の出力信号波形を示す。気体の流速を示す波
形イとマイクロホン1の出力ロの比較から明らか
なように、マイクロホン1の出力信号は、気体の
流速υとそれを微分した波形として考えられる気
体の加速度の積υ・αを表している。又、波形イ
とハの比較から明らかなように積分回路2の出力
信号は、流速の2乗を表し、イ,ニの比較から明
らかなように、積分出力ハを処理回路3でその平
方根をとつて得られた出力は、測定しようとして
いる流速そのものをあらわしている。このような
関係は他の異つた流動状態の気体についてもなり
たつことが実験でたしかめられた。
3A shows an example of a change in the flow velocity of the gas to be measured, B shows the output signal waveform of the microphone 1, C shows the output signal waveform of the integrating circuit 2, and D shows the output signal waveform of the processing circuit 3. As is clear from the comparison of waveform A indicating the gas flow velocity and output B of microphone 1, the output signal of microphone 1 is the product of the gas flow velocity υ and the gas acceleration, which can be considered as a waveform obtained by differentiating it, υ・α. represents. Also, as is clear from the comparison of waveforms A and C, the output signal of the integrating circuit 2 represents the square of the flow velocity, and as is clear from the comparison of waveforms A and D, the integral output C is processed by the processing circuit 3 to calculate its square root. The output obtained represents the flow velocity itself to be measured. Experiments have confirmed that this relationship also holds true for gases in different fluid states.

なお、処理回路3としては一般には平方根回路
が用いられるが、使用するマイクロホンの特性等
の違いにより、入出力特性を平方根特性より若干
シフトさせた方がよいことがある。
Although a square root circuit is generally used as the processing circuit 3, it may be better to shift the input/output characteristic slightly from the square root characteristic depending on the characteristics of the microphones used.

以上述べたように、本発明による気体の流速測
定装置は、マイクロホンと、マイクロホン出力を
積分する積分回路と、積分出力のほぼ平方根を得
る処理回路とから構成することができ、温度セン
サーを必要としない。また、本発明によれば気体
の流れのセンサーとして一般に広く使用されてい
るマイクロホンを用いることができ、測定回路も
積分回路と簡単な処理回路のみで構成できるの
で、製作容易で、丈夫で、安価な気体の流速測定
装置を提供できることは明かである。
As described above, the gas flow rate measuring device according to the present invention can be configured from a microphone, an integrating circuit that integrates the microphone output, and a processing circuit that obtains approximately the square root of the integrated output, and does not require a temperature sensor. do not. Furthermore, according to the present invention, a microphone that is generally widely used as a gas flow sensor can be used, and the measurement circuit can be configured with only an integrating circuit and a simple processing circuit, so it is easy to manufacture, durable, and inexpensive. It is clear that it is possible to provide a gas flow rate measuring device.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明による気体の流速測定装置の基
本構成を示すブロツク図、第2図は、第1図の気
体の流速測定装置の具体的構成例を示す図、第3
図は第2図における各部の信号波形を示す図であ
る。 1…マイクロホン、2…積分回路、3…処理回
路。
FIG. 1 is a block diagram showing the basic configuration of a gas flow rate measuring device according to the present invention, FIG. 2 is a diagram showing a specific configuration example of the gas flow rate measuring device of FIG. 1, and FIG.
The figure is a diagram showing signal waveforms at various parts in FIG. 2. 1...Microphone, 2...Integrator circuit, 3...Processing circuit.

Claims (1)

【特許請求の範囲】[Claims] 1 マイクロホンと、マイクロホンの出力信号を
積分する積分回路と、積分回路の出力信号を処理
する処理回路から構成されることを特徴とする気
体の流速測定装置。
1. A gas flow rate measuring device comprising a microphone, an integrating circuit that integrates the output signal of the microphone, and a processing circuit that processes the output signal of the integrating circuit.
JP267482A 1982-01-13 1982-01-13 Gas flow velocity measuring apparatus Granted JPS58120169A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP267482A JPS58120169A (en) 1982-01-13 1982-01-13 Gas flow velocity measuring apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP267482A JPS58120169A (en) 1982-01-13 1982-01-13 Gas flow velocity measuring apparatus

Publications (2)

Publication Number Publication Date
JPS58120169A JPS58120169A (en) 1983-07-16
JPS6239941B2 true JPS6239941B2 (en) 1987-08-26

Family

ID=11535853

Family Applications (1)

Application Number Title Priority Date Filing Date
JP267482A Granted JPS58120169A (en) 1982-01-13 1982-01-13 Gas flow velocity measuring apparatus

Country Status (1)

Country Link
JP (1) JPS58120169A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6283667A (en) * 1985-10-09 1987-04-17 Sakata Denki Kk Method for measuring flow speed of ground water

Also Published As

Publication number Publication date
JPS58120169A (en) 1983-07-16

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