JPH0572221A - Air velocity sensor - Google Patents

Air velocity sensor

Info

Publication number
JPH0572221A
JPH0572221A JP3262908A JP26290891A JPH0572221A JP H0572221 A JPH0572221 A JP H0572221A JP 3262908 A JP3262908 A JP 3262908A JP 26290891 A JP26290891 A JP 26290891A JP H0572221 A JPH0572221 A JP H0572221A
Authority
JP
Japan
Prior art keywords
temperature
wind speed
heater
sensor
thin
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
Application number
JP3262908A
Other languages
Japanese (ja)
Inventor
Shinichi Osada
田 慎 一 長
Tsugi Tanihiro
広 次 谷
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.)
Murata Manufacturing Co Ltd
Original Assignee
Murata Manufacturing Co Ltd
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 Murata Manufacturing Co Ltd filed Critical Murata Manufacturing Co Ltd
Priority to JP3262908A priority Critical patent/JPH0572221A/en
Publication of JPH0572221A publication Critical patent/JPH0572221A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To obtain an air velocity sensor in an output signal of which an error hardly occurs even when the temperature of air current to be measured changes sharply and which has high responsiveness. CONSTITUTION:This air velocity sensor 10 comprises a base 12, and a thin-film temperature-measuring resistor 14 for a heater and a thin-film temperature- measuring resistor 16 for temperature compensation are formed on the base 12. The thin-film temperature-measuring resistor 14 for the heater and the thin- film temperature-measuring resistor 16 for temperature compensation are formed in the same shape and dimensions and each of them is formed by applying Pt, for instance, on a rectangular alumina base of a thickness 0.15mm, for instance, by laser trimming or etching. On the base 12, moreover, a circuit of fixed temperature method is formed as a is formed as a detecting circuit 18, which is connected to the thin-film temperature-measuring resistor 14 for the heater and the thin-film temperature-measuring resistor 16 for temperature compensation.

Description

【発明の詳細な説明】Detailed Description of the Invention

【0001】[0001]

【産業上の利用分野】この発明は風速センサに関し、特
にたとえば、熱式風速センサなどの風速センサに関す
る。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a wind speed sensor, and more particularly to a wind speed sensor such as a thermal wind speed sensor.

【0002】[0002]

【従来の技術】風速センサとしては、主にPtセンサを
はじめとする測温抵抗体を発熱させ、気流による放熱か
ら風速を求める熱式風速センサがある。熱式風速センサ
の回路方式としては、測温抵抗体に定電流を流す定電流
法と、測温抵抗体の温度が常に一定になるように制御す
る定温度法がよく用いられる。特に、応答速度を速くで
きることや、回路部品数を少なくできるなどの点から、
定温度法がよく用いられる。
2. Description of the Related Art As a wind velocity sensor, there is a thermal type wind velocity sensor such as a Pt sensor, which mainly produces heat from a resistance temperature detector and obtains the wind velocity from the heat radiated by an air flow. As the circuit system of the thermal wind sensor, a constant current method in which a constant current is applied to the resistance temperature detector and a constant temperature method in which the temperature of the resistance temperature detector is controlled to be always constant are often used. In particular, from the viewpoint that the response speed can be increased and the number of circuit parts can be reduced,
The constant temperature method is often used.

【0003】図2は、従来の熱式風速センサの一例を示
す平面図である。この風速センサ1は、2つの温度セン
サ2,3を含む。これらの温度センサ2,3は、プリン
ト基板4の電子回路5に接続される。これらの温度セン
サのうち、一方の温度センサ2には、ヒータ用温度セン
サとしてのヒータ用測温抵抗体が用いられ、一定の温度
に発熱させて気流による放熱の変化をとらえる機能を有
する。他方の温度センサ3には温度補償用センサとして
の温度補償用測温抵抗体が用いられ、気流の温度変化に
よる風速測定値の誤差を補正する機能を有する。
FIG. 2 is a plan view showing an example of a conventional thermal wind speed sensor. The wind speed sensor 1 includes two temperature sensors 2 and 3. These temperature sensors 2 and 3 are connected to the electronic circuit 5 of the printed circuit board 4. Among these temperature sensors, one of the temperature sensors 2 uses a heater resistance temperature detector as a heater temperature sensor, and has a function of generating heat at a constant temperature and catching a change in heat radiation due to an air flow. The other temperature sensor 3 uses a temperature compensating resistance temperature detector as a temperature compensating sensor and has a function of correcting an error in the measured value of the wind speed due to the temperature change of the air flow.

【0004】風速センサ1の電子回路5としては、たと
えば図3に示すような定温度法の回路方式が用いられ
る。温度センサ2,3は、抵抗6,7とともにブリッジ
回路を構成する。そして、温度センサ2,3の出力は、
オペアンプ8に入力される。オペアンプ8の出力側はト
ランジスタ9のベースに接続され、トランジスタ9の出
力はブリッジ回路にフィードバックされる。ヒータ用の
温度センサ2には電流が流され、それによって温度セン
サ2は加熱する。ここに気流が接触すると温度センサ2
の熱が奪われ、温度センサ2の抵抗値変化から風速が測
定される。また、温度補償用の温度センサ3で空気の温
度が測定され、空気の温度の違いによる風速の誤差が補
正される。したがって、風速の変化に対する風速センサ
1の応答速度は、一方の温度センサ2の熱応答性によっ
て決定される。熱応答性をよくするため、温度センサ2
には、非常に薄いたとえば厚さ0.15mmのアルミナ
基板が用いられている。このような風速センサ1では、
風速の変化に対する風速センサ1の応答時間は約0.1
secである。また、他方の温度センサ3は、風速の変
化に対する風速センサ1の応答時間の決定に関与しな
い。そのため、その温度センサ3には、たとえば厚さ
0.6mmのアルミナ基板が従来から用いられている。
As the electronic circuit 5 of the wind speed sensor 1, for example, a constant temperature method circuit system as shown in FIG. 3 is used. The temperature sensors 2 and 3 form a bridge circuit together with the resistors 6 and 7. And the outputs of the temperature sensors 2 and 3 are
It is input to the operational amplifier 8. The output side of the operational amplifier 8 is connected to the base of the transistor 9, and the output of the transistor 9 is fed back to the bridge circuit. An electric current is passed through the temperature sensor 2 for the heater, which causes the temperature sensor 2 to heat. When the airflow contacts here, the temperature sensor 2
Is taken away, and the wind speed is measured from the change in the resistance value of the temperature sensor 2. Further, the temperature sensor 3 for temperature compensation measures the temperature of the air, and the error in the wind speed due to the difference in the temperature of the air is corrected. Therefore, the response speed of the wind speed sensor 1 to the change in the wind speed is determined by the thermal responsiveness of the one temperature sensor 2. Temperature sensor 2 to improve thermal response
Is a very thin alumina substrate having a thickness of 0.15 mm. In such a wind speed sensor 1,
The response time of the wind speed sensor 1 to changes in wind speed is about 0.1.
sec. The other temperature sensor 3 is not involved in determining the response time of the wind speed sensor 1 with respect to changes in the wind speed. Therefore, an alumina substrate having a thickness of 0.6 mm, for example, has been conventionally used for the temperature sensor 3.

【0005】[0005]

【発明が解決しようとする課題】しかしながら、このよ
うな風速センサ1では、測定する気流の温度が急激に変
化した場合、一方の温度センサ2と他方の温度センサ3
との応答時間が大幅に違うため、温度変化が終了して
も、しばらくは、正確な風速信号を出力できない現象が
発生する。すなわち、気流の温度が上昇した場合、ま
ず、一方の温度センサ2によって、奪われる熱量の変化
が測定される。それから、他方の温度センサ3が空気の
温度を測定し、空気の温度の違いによる風速の誤差を補
正する。そのため、この風速センサ1では、気流の変化
がなくても、気流が小さくなったという風速信号を出力
してしまう。したがって、このような風速センサ1で
は、気流の急激な温度変化が無い場合、応答時間は0.
1secと応答性が高いけれども、気流の急激な温度変
化のある場合、非常に大きな誤差を伴って風速信号を出
力する。
However, in such a wind speed sensor 1, when the temperature of the air flow to be measured changes suddenly, one temperature sensor 2 and the other temperature sensor 3 are used.
Since the response time of and is significantly different, even if the temperature change ends, the phenomenon that the accurate wind speed signal cannot be output occurs for a while. That is, when the temperature of the airflow rises, first, the change in the amount of heat taken by one of the temperature sensors 2 is measured. Then, the other temperature sensor 3 measures the temperature of the air and corrects the error in the wind speed due to the difference in the temperature of the air. Therefore, the wind speed sensor 1 outputs a wind speed signal indicating that the air flow has become small even if there is no change in the air flow. Therefore, in such a wind speed sensor 1, when there is no rapid temperature change of the air flow, the response time is 0.
Although the response is as high as 1 sec, when there is a rapid temperature change in the airflow, the wind speed signal is output with a very large error.

【0006】それゆえに、この発明の主たる目的は、測
定する気流の温度が急激に変化しても、出力信号に誤差
が生じにくく、応答性の高い風速センサを提供すること
である。
Therefore, a main object of the present invention is to provide a wind speed sensor having a high responsiveness, in which an error does not easily occur in an output signal even if the temperature of the measured airflow changes rapidly.

【0007】[0007]

【課題を解決するための手段】この発明は、気流によっ
て奪われる熱量を測定するためのヒータ用測温抵抗体
と、気流の温度を測定するための温度補償用測温抵抗体
とを含み、ヒータ用測温抵抗体と温度補償用測温抵抗体
とは、同一の形状および大きさに形成され、かつ、定温
度法によって風速が検出される、風速センサである。
The present invention includes a resistance temperature detector for a heater for measuring the amount of heat taken by an air flow, and a temperature compensation resistance temperature sensor for measuring the temperature of an air flow, The heater resistance temperature detector and the temperature compensation resistance temperature detector are wind speed sensors that are formed in the same shape and size and detect the wind speed by the constant temperature method.

【0008】[0008]

【作用】ヒータ用測温抵抗体と温度補償用測温抵抗体と
は、同一の形状および同一の大きさに形成されるため、
それらの熱容量が同一となる。そのため、ヒータ用測温
抵抗体と温度補償用測温抵抗体との熱応答性が等しくな
る。
Since the resistance temperature detector for the heater and the resistance temperature detector for temperature compensation are formed in the same shape and the same size,
They have the same heat capacity. Therefore, the thermal responsiveness of the resistance temperature detector for heater and that of the resistance temperature detector for temperature compensation become equal.

【0009】[0009]

【発明の効果】この発明によれば、測定する気流の温度
が急激に変化しても、出力信号に誤差が生じにくく、応
答性の高い風速センサが得られる。
According to the present invention, it is possible to obtain a wind speed sensor having high responsiveness in which an error does not easily occur in the output signal even when the temperature of the air flow to be measured changes suddenly.

【0010】この発明の上述の目的,その他の目的,特
徴および利点は、図面を参照して行う以下の実施例の詳
細な説明から一層明らかとなろう。
The above-mentioned objects, other objects, features and advantages of the present invention will become more apparent from the following detailed description of embodiments with reference to the drawings.

【0011】[0011]

【実施例】図1はこの発明の一実施例を示す図解図であ
る。風速センサ10は基板12を含む。基板12の上に
は、ヒータ用温度センサとしてのヒータ用薄膜測温抵抗
体14と、温度補償用温度センサとしての温度補償用薄
膜測温抵抗体16とが形成される。ヒータ用薄膜測温抵
抗体14は、たとえば厚さ0.15mmの矩形のアルミ
ナ基板の上に、たとえばPtをレーザトリミングあるい
はエッチングすることによって形成される。同様にし
て、温度補償用薄膜測温抵抗体16も、厚さ0.15m
mの矩形のアルミナ基板の上に、Ptをレーザトリミン
グあるいはエッチングすることによって形成される。な
お、この場合、ヒータ用薄膜測温抵抗体14の抵抗値と
しては、たとえば10Ωのものが用いられ、温度補償用
薄膜測温抵抗体16としては、たとえば500Ωのもの
が用いられる。この実施例では、特に、従来ヒータ用測
温抵抗体に用いられていた、たとえば厚さ0.15mm
のアルミナ基板が用いられ、ヒータ用薄膜測温抵抗体1
4と温度補償用薄膜測温抵抗体16とは、同一の形状お
よび同一の大きさに形成される。
FIG. 1 is an illustrative view showing one embodiment of the present invention. The wind speed sensor 10 includes a substrate 12. On the substrate 12, a heater thin film resistance temperature detector 14 as a heater temperature sensor and a temperature compensation thin film resistance temperature detector 16 as a temperature compensation temperature sensor are formed. The heater thin film resistance temperature detector 14 is formed, for example, by laser trimming or etching Pt on a rectangular alumina substrate having a thickness of 0.15 mm. Similarly, the thin film resistance temperature detector 16 for temperature compensation also has a thickness of 0.15 m.
It is formed by laser trimming or etching Pt on a rectangular alumina substrate of m. In this case, the resistance value of the heater thin film resistance temperature detector 14 is, for example, 10Ω, and the temperature compensation thin film resistance temperature detector 16 is, for example, 500Ω. In this embodiment, in particular, a thickness of 0.15 mm, which has been conventionally used for a resistance temperature detector for a heater, is used.
Thin film resistance temperature detector for heater 1
4 and the temperature compensating thin film resistance temperature detector 16 are formed in the same shape and the same size.

【0012】さらに、基板12の上には、検出回路18
が形成される。この検出回路18としては、図3に示す
ような定温度法の回路が形成される。そして、ヒータ用
薄膜測温抵抗体14と温度補償用薄膜測温抵抗体16と
が検出回路18に接続される。
Further, a detection circuit 18 is provided on the substrate 12.
Is formed. As the detection circuit 18, a constant temperature circuit as shown in FIG. 3 is formed. Then, the heater thin film resistance temperature detector 14 and the temperature compensation thin film resistance temperature detector 16 are connected to the detection circuit 18.

【0013】この風速センサ10では、ヒータ用薄膜測
温抵抗体14が加熱され、空気の流れが接触することに
よって、その熱が奪われる。この温度変化にともなうヒ
ータ用薄膜測温抵抗体14の抵抗値の変化が検出回路1
8によって検出される。また、温度補償用薄膜測温抵抗
体16によって空気の温度が測定され、空気の温度によ
る風速測定の誤差が補正される。これらのヒータ用薄膜
測温抵抗体14および温度補償用薄膜測温抵抗体16の
信号が検出回路18に入力され、風速に対応する検出信
号が出力される。この検出信号が、引き出しリード20
を介して信号を処理するための外部回路に入力される。
また、この風速センサ10のための電源が、引き出しリ
ード22によって検出回路18に接続される。
In this wind speed sensor 10, the thin film resistance temperature detector 14 for a heater is heated and the heat of the thin film resistance temperature detector 14 for a heater is taken away by contact with the air flow. The change in the resistance value of the heater thin film resistance temperature detector 14 due to this temperature change is detected by the detection circuit 1.
Detected by 8. Further, the temperature of the air is measured by the temperature compensating thin film resistance temperature detector 16, and the error in the wind speed measurement due to the temperature of the air is corrected. The signals from the heater thin film resistance temperature detector 14 and the temperature compensation thin film resistance temperature detector 16 are input to the detection circuit 18, and a detection signal corresponding to the wind speed is output. This detection signal is output by the lead 20.
Is input to an external circuit for processing the signal.
Further, the power supply for the wind speed sensor 10 is connected to the detection circuit 18 by the lead 22.

【0014】この風速センサ10では、特に、ヒータ用
薄膜測温抵抗体14と温度補償用薄膜測温抵抗体16と
が同一の形状および同一の大きさに形成されるため、そ
れらの熱容量が同じになる。そのため、この風速センサ
10では、気流の急激な温度変化に対しても、温度補償
の遅れがなく、風速に対する検出信号の誤差を防止でき
る。したがって、応答性の高い風速センサが得られる。
この実施例の風速センサ10では、その応答速度が0.
1secとなり、従来のものと比べて大幅に応答性を高
めることができる。
In the wind velocity sensor 10, since the thin film resistance temperature detector 14 for heater and the thin film resistance temperature detector 16 for temperature compensation are formed in the same shape and the same size, their heat capacities are the same. become. Therefore, in this wind speed sensor 10, there is no delay in temperature compensation even with a sudden temperature change of the air flow, and an error in the detection signal with respect to the wind speed can be prevented. Therefore, a highly responsive wind speed sensor can be obtained.
In the wind speed sensor 10 of this embodiment, the response speed is 0.
It becomes 1 sec, and the responsiveness can be greatly improved compared to the conventional one.

【0015】なお、ヒータ用薄膜測温抵抗体14および
温度補償用薄膜測温抵抗体16としては、従来温度補償
用薄膜測温抵抗体に用いられていた、たとえば厚さ0.
6mmのアルミナ基板を用いたものでもよい。この場合
でも、ヒータ用薄膜測温抵抗体14と温度補償用薄膜測
温抵抗体16とは、同一の形状および同一の大きさに形
成される。ヒータ用薄膜測温抵抗体14と温度補償用薄
膜測温抵抗体16とに厚いアルミナ基板を用いると、薄
いアルミナ基板を用いたものに比べて熱応答性は劣る
が、これらの熱容量が等しいために熱応答性に差がな
い。したがって、このような風速センサ10でも、気流
の温度が変化しても、風速の検出に対する温度補償の遅
れがなく、風速に対応する検出信号の誤差を防止でき
る。この風速センサ10は、アルミナ基板を薄く形成す
る必要がないために、コストを低くすることができる。
したがって、このような風速センサ10は、それほど応
答性を必要としないローコストタイプとして用いられ
る。
As the thin film resistance temperature detector 14 for heater and the thin film resistance temperature detector 16 for temperature compensation, for example, a thickness of 0.
A 6 mm alumina substrate may be used. Even in this case, the heater thin film resistance temperature detector 14 and the temperature compensation thin film resistance temperature detector 16 are formed to have the same shape and the same size. When a thick alumina substrate is used for the heater thin film resistance temperature detector 14 and the temperature compensation thin film resistance temperature detector 16, the thermal response is inferior to that using a thin alumina substrate, but the heat capacities are equal. There is no difference in thermal response. Therefore, even with such a wind speed sensor 10, even if the temperature of the air flow changes, there is no delay in temperature compensation for the detection of the wind speed, and an error in the detection signal corresponding to the wind speed can be prevented. The wind speed sensor 10 does not require a thin alumina substrate, so that the cost can be reduced.
Therefore, such a wind speed sensor 10 is used as a low-cost type that does not require much responsiveness.

【図面の簡単な説明】[Brief description of drawings]

【図1】この発明の一実施例を示す図解図である。FIG. 1 is an illustrative view showing one embodiment of the present invention.

【図2】従来の風速センサの一例を示す図解図である。FIG. 2 is an illustrative view showing an example of a conventional wind speed sensor.

【図3】図2に示す風速センサの回路図である。FIG. 3 is a circuit diagram of the wind speed sensor shown in FIG.

【符号の説明】[Explanation of symbols]

10 風速センサ 12 基板 14 ヒータ用薄膜測温抵抗体 16 温度補償用薄膜測温抵抗体 18 検出回路 10 Wind speed sensor 12 Substrate 14 Thin film resistance temperature detector for heater 16 Thin film resistance temperature detector for temperature compensation 18 Detection circuit

Claims (1)

【特許請求の範囲】[Claims] 【請求項1】 気流によって奪われる熱量を測定するた
めのヒータ用測温抵抗体、および前記気流の温度を測定
するための温度補償用測温抵抗体を含み、 前記ヒータ用測温抵抗体と前記温度補償用測温抵抗体と
は、同一の形状および大きさに形成され、かつ、定温度
法によって風速が検出される、風速センサ。
1. A resistance temperature detector for a heater for measuring an amount of heat taken by an air flow, and a temperature compensation resistance temperature sensor for measuring a temperature of the air flow, wherein the resistance temperature detector for a heater is: The temperature compensating temperature-measuring resistor is a wind speed sensor that has the same shape and size and detects the wind speed by the constant temperature method.
JP3262908A 1991-09-12 1991-09-12 Air velocity sensor Pending JPH0572221A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3262908A JPH0572221A (en) 1991-09-12 1991-09-12 Air velocity sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3262908A JPH0572221A (en) 1991-09-12 1991-09-12 Air velocity sensor

Publications (1)

Publication Number Publication Date
JPH0572221A true JPH0572221A (en) 1993-03-23

Family

ID=17382281

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3262908A Pending JPH0572221A (en) 1991-09-12 1991-09-12 Air velocity sensor

Country Status (1)

Country Link
JP (1) JPH0572221A (en)

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