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JPH0134336B2 - - Google Patents

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Publication number
JPH0134336B2
JPH0134336B2 JP16522782A JP16522782A JPH0134336B2 JP H0134336 B2 JPH0134336 B2 JP H0134336B2 JP 16522782 A JP16522782 A JP 16522782A JP 16522782 A JP16522782 A JP 16522782A JP H0134336 B2 JPH0134336 B2 JP H0134336B2
Authority
JP
Japan
Prior art keywords
gas
infrared
measurement signal
measurement
helmholtz resonator
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
JP16522782A
Other languages
Japanese (ja)
Other versions
JPS5954950A (en
Inventor
Masato Maeda
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.)
Yokogawa Electric Corp
Original Assignee
Yokogawa Electric Corp
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Filing date
Publication date
Application filed by Yokogawa Electric Corp filed Critical Yokogawa Electric Corp
Priority to JP16522782A priority Critical patent/JPS5954950A/en
Publication of JPS5954950A publication Critical patent/JPS5954950A/en
Publication of JPH0134336B2 publication Critical patent/JPH0134336B2/ja
Granted legal-status Critical Current

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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N21/00Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
    • G01N21/17Systems in which incident light is modified in accordance with the properties of the material investigated
    • G01N21/25Colour; Spectral properties, i.e. comparison of effect of material on the light at two or more different wavelengths or wavelength bands
    • G01N21/31Investigating relative effect of material at wavelengths characteristic of specific elements or molecules, e.g. atomic absorption spectrometry
    • G01N21/35Investigating relative effect of material at wavelengths characteristic of specific elements or molecules, e.g. atomic absorption spectrometry using infrared light
    • G01N21/37Investigating relative effect of material at wavelengths characteristic of specific elements or molecules, e.g. atomic absorption spectrometry using infrared light using pneumatic detection
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01NINVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
    • G01N21/00Investigating or analysing materials by the use of optical means, i.e. using sub-millimetre waves, infrared, visible or ultraviolet light
    • G01N21/17Systems in which incident light is modified in accordance with the properties of the material investigated
    • G01N21/59Transmissivity
    • G01N21/61Non-dispersive gas analysers

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  • Physics & Mathematics (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Health & Medical Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Chemical & Material Sciences (AREA)
  • Analytical Chemistry (AREA)
  • Biochemistry (AREA)
  • General Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Immunology (AREA)
  • Pathology (AREA)
  • Investigating Or Analysing Materials By Optical Means (AREA)

Description

【発明の詳細な説明】[Detailed description of the invention]

本発明は、非分散形赤外線ガス分析計の検出器
として用いられ、ドツプラー効果を利用してヘル
ムホルツ共鳴の速度振幅を測定することにより、
入射する赤外線のエネルギーを検出する赤外線検
出器に関する。 一般に、非分散形赤外線ガス分析計に用いられ
る検出器としては、従来からコンデンサマイクロ
フオンとマイクロフローセンサーが知られてい
る。該コンデンサマイクロフオンは、測定ガスお
よび基準ガスによつて夫々吸収された赤外線エネ
ルギーの差をマイクロフオンの変位として検出す
ることにより、上記測定ガス中の被測定成分濃度
を検出するものであり、マイクロフローセンサー
は、測定ガスおよび基準ガスによつて夫々吸収さ
れた赤外線エネルギーを所定のガスが充填された
検出部で受け該検出部内に装設された検出端によ
つて上記所定のガスの微小な流速変化を検出する
ことにより、上記測定ガス中の被測定成分濃度を
検出するものである。 然し乍ら、上記コンデンサマイクロフオンの場
合も上記マイクロフローセンサの場合も、コンデ
ンサ膜の変位を捕えたり所定のガスの流速変化を
捕えたりするような構成であるため、上記コンデ
ンサマイクロフオンや所定のガス中に供給される
赤外線エネルギーが数Hz程度の周波数であること
と相まち、検出される信号が非常に微弱であつて
上記被測定成分濃度の高感度測定が困難であると
いう欠点があつた。 本発明は、かかる欠点に鑑みてなされたもので
あり、その目的は、非分散形赤外線ガス分析計の
検出器として用いられ測定ガス中の被測定成分濃
度を高感度に測定できる赤外線検出器を提供する
ことにある。 本発明の特徴は、非分散形赤外線ガス分析計の
検出器として用いられ測定ガス中の被測定成分濃
度を測定する赤外線検出器において、ドツプラー
効果を利用してヘルムホルツ共鳴の速度振幅を測
定することにより、上記測定ガス等を透過して入
射する赤外線のエネルギーを高感度に検出するよ
うにしたことにある。 以下、本発明について図を用いて詳細に説明す
る。第1図は、本発明の理解を容易にするため示
すヘルムホルツ共鳴器の原理説明図であり、図
中、1は内容積Vを有する気密な円筒状の第1容
器、2は第1容器1の一側所部分に一体的に固着
され内部空間の断面積Sと長さlを有する円柱状
の第2容器である。また、第1容器1と第2容器
2は通常同一部材で一体的に形成され、夫々の内
部空間も一体的に連なつている。このようなヘル
ムホルツ共鳴器の内部空間に気体が満たされる
と、第2容器2内の気体が振動質量となり、第1
容器1内の気体がばねの役割を行なうようにな
る。従つて、第1容器1内の気体が断熱変化する
場合、第1および第2の容器1,2の内部空間で
形成される系内の気体の固有振動数fn〔c/s〕
は下式(1)のようになる。 但し、 P:気体の圧力〔Kg/cm2〕、 γ:断熱指数(通常は1.4〜1.7) ρ:気体の密度〔Kg・s2/cm4〕 C:気体中の音速〔cm/s〕、
The present invention is used as a detector for a non-dispersive infrared gas analyzer, and by measuring the velocity amplitude of Helmholtz resonance using the Doppler effect,
The present invention relates to an infrared detector that detects incident infrared energy. In general, condenser microphones and microflow sensors are conventionally known as detectors used in non-dispersive infrared gas analyzers. The condenser microphone detects the concentration of the component to be measured in the measurement gas by detecting the difference in infrared energy absorbed by the measurement gas and the reference gas as the displacement of the microphone. A flow sensor receives infrared energy absorbed by a measurement gas and a reference gas, respectively, in a detection section filled with a predetermined gas, and detects minute amounts of the predetermined gas by a detection end installed in the detection section. By detecting changes in flow velocity, the concentration of the component to be measured in the measurement gas is detected. However, in the case of the above-mentioned condenser microphone and the above-mentioned microflow sensor, since they are configured to capture the displacement of the capacitor membrane or the change in the flow velocity of a predetermined gas, Coupled with the fact that the infrared energy supplied to the sensor has a frequency of about several Hz, the detected signal is extremely weak, making it difficult to measure the concentration of the component to be measured with high sensitivity. The present invention has been made in view of these drawbacks, and its purpose is to provide an infrared detector that can be used as a detector in a non-dispersive infrared gas analyzer and can measure the concentration of a component to be measured in a measurement gas with high sensitivity. It is about providing. A feature of the present invention is that the velocity amplitude of Helmholtz resonance is measured using the Doppler effect in an infrared detector used as a detector of a non-dispersive infrared gas analyzer to measure the concentration of a component to be measured in a measurement gas. Accordingly, the energy of the infrared rays passing through the measurement gas and the like is detected with high sensitivity. Hereinafter, the present invention will be explained in detail using figures. FIG. 1 is a diagram explaining the principle of a Helmholtz resonator shown to facilitate understanding of the present invention. In the figure, 1 is an airtight cylindrical first container having an internal volume V; 2 is a first container 1 This is a cylindrical second container which is integrally fixed to one side of the container and has an internal space having a cross-sectional area S and a length l. Further, the first container 1 and the second container 2 are usually integrally formed from the same member, and their respective internal spaces are also integrally connected. When the internal space of such a Helmholtz resonator is filled with gas, the gas in the second container 2 becomes a vibrating mass, and the first
The gas inside the container 1 comes to play the role of a spring. Therefore, when the gas in the first container 1 changes adiabatically, the natural frequency fn [c/s] of the gas in the system formed by the internal spaces of the first and second containers 1 and 2
is as shown in equation (1) below. However, P: Pressure of gas [Kg/cm 2 ], γ: Adiabatic index (usually 1.4 to 1.7) ρ: Density of gas [Kg・s 2 /cm 4 ] C: Speed of sound in gas [cm/s] ,

【式】 因みに、V=2〔cm3〕、l=2〔cm〕、S=0.2
〔cm2〕、C=340x102〔cm/s〕の場合について、上
式(1)から上記固有振動数fnを求めると、fn=
1.21x103〔c/s〕=1.21〔kHz〕となる。従つて、
この1.21kHzで上記系内にエネルギーを注ぐと、
上記系はそのエネルギーを吸収して発振するよう
になる。また、上記系が発振状態になると系内の
気体の振動振幅が増大するが、気体の粘性などに
よる減衰のため次第に定常状態に移行し、この時
の速度倍率μv(即ち、第1図の容器1,2内の気
体に、外部から供給される赤外線エネルギーなど
によつて一定の力が働くときに、該気体の熱膨張
などによつて生じる気体の流れの速度Aと、その
力がトリガーとなつて容器1,2内の気体が振動
する場合における振動速度の最大値Bとの比A/
B)は下式(2)のように与えられる。 但し、 Vmax:気体が振動する速度の最大値 Vs:一定のエネルギーが供給されているとき気
体の膨脹によつて生ずるその気体の流速 u:振動数比(即ち2πfと共振振動数ωnとの比
2πf/ωn) ζ:減衰比(0<ζ<1であつて、減衰振動にお
いて減衰の比率を示す。換言するならば、全振
動と非振動の間の振動らしさを示す係数という
こともできる) また、第2図は本発明実施例の使用例説明図で
あり、図中、3は導入口3aから測定ガスが導び
かれて内部を流れ導出口3bから外部へ送出され
る測定セル、4は基準ガスが充填されてなる基準
セル、5a,5bは例えば赤外線ランプである光
源、6を光源5a,5bから発せられた光線を
夫々断続光となすセクタ、7はセクタ6を所定の
周期で回転させるモータ、8は内部に所定の気体
(例えば測定成分ガスと同一気体)が充填される
と共に第1図のヘルムホルツ共鳴器が2個結合さ
れてなるヘルムホルツ共鳴器、9aは該共鳴器8
内の一側所定部分に固着され超音波信号を発する
超音波発振器、9bは上記共鳴器8内の他側所定
部分(超音波発信器9aが固着されている位置と
対向する位置)に固着され上記超音波信号を受け
る超音波受信器である。また、ヘルムホルツ共鳴
器8、超音波発信器9a、および超音波受信器9
bによつて本発明実施例の赤外線検出器が構成さ
れると共に、超音波受信器9bの出力が所定の信
号処理回路(図示せず)でもつて信号処理され上
記測定ガス中の被測定成分濃度を示す値に変換さ
れて表示器等(図示せず)に濃度表示されるよう
になつている。尚、上記ヘルムホルツ共鳴器8は
第1図のヘルムホルツ共鳴器が2個結合されたも
のであるが、第1図の場合と同じように上記(1)式
や(2)式が成立する。更に、第3図は上記セクタ6
を構成する部品の平面構成図であり、図中、10
は中心に上記モータ7の回転軸が固着可能な中央
部、10a1〜10aoは所定の幅を有し該幅と等し
い間隔を互いに保ちながら中央部10に一側が一
体的固着されてなる複数個の羽根である。また、
上記セクタ6は第3図に示す部品が2個組み合わ
されて構成され、そのうちの一方は固定されて動
かず他方は上記モータ7の回転軸に上記中央部1
0が固着されて回転させられるようになつてい
る。因みに、上記羽根10a1〜10aoの数が200
個である場合には、上記モータ7が360r.p.m.で
回転すると、光源5a,5bから発せられた光線
は1.2kHzで断続されるようになる。これは、従来
の赤外線ガス分析計で使用されているセクタに比
して数百倍を速くチヨツピングを行なつているこ
とに相当する。また、上記断続光の周波数とヘル
ムホルツ共鳴器8の共振振動数ωnをほぼ等しく
することにより、前記(2)式で2πf≒ωn即ちu≒1
が成立し、μv≒1/2となる。従つて、ζが小さい 程μvが大きくなり、上記気体の大きな速度振幅
が得られるようになる 以下、上記構成からなる本発明実施例の動作に
ついて、第2図を用いて詳細に説明する。第2図
において、被測定成分を含む測定ガスは矢印で示
す如く導入口3aから測定セル3内へ導入され導
出口3bから外部へ送出されると共に、基準セル
4内には所定の基準ガスが充填されている。ま
た、超音波発振器9aから発せられた超音波信号
は、ヘルムホルツ共鳴器8内の気体中を伝播し超
音波受信器9bに達して受信されている。更に、
光源5a,5bから発せられセクタ6によつて断
続光とされた測定光および基準光は、夫々測定セ
ル3内の測定ガスおよび基準セル4内の基準ガス
を透過してヘルムホルツ共鳴器8内に到達する。
従つて、上記測定ガス内に被測定成分が存在しな
い測定ガスが流されている場合(以下「基準状
態」という)には、上記測定光および基準光が
夫々測定ガスおよび基準ガスによるエネルギー吸
収を受けずにヘルムホルツ共鳴器8内に到達する
が、上記測定ガス内に被測定成分が存在する測定
ガスが流されている場合(以下「測定状態」とい
う)には、上記測定光のみが測定ガスによるエネ
ルギー吸収を受け減衰してヘルムホルツ共鳴器8
内に到達する。従つて、該ヘルムホルツ共鳴器8
内では、上記基準状態と測定状態の場合で前記(2)
式のVs値が変化する。このような変化を検出す
るのに、従来の赤外線検出器であるコンデンサマ
イクロホンの場合は、回転するチヨツパーを用い
チヨツピングの一周期毎に信号を取出すようにな
つていた。 これに対し、本発明の実施例の場合は、その変
化する値が小さくても共鳴状態になつている。こ
のため、エネルギーが取込まれて速度倍率μvの
変化する値は大きくなり、究極的にヘルムホルツ
共鳴器8内の気体の速度振幅が大きく変化するよ
うになる。 従つて、超音波発信器9aから周波数fsの超音
波信号が発せられると、該超音波信号はドツプラ
ー効果による「うなり」の周波数Δfsを伴なつて
超音波受信器9bに受信される。ここに、ドツプ
ラー効果による「うなり」の周波数Δfsとは、上
記気体のプラス方向とマイナス方向(第2図の超
音波発信器9aと超音波受信器9bを結ぶ軸方向
において一方の方向をプラス方向とし反対の方向
をマイナス方向と呼ぶものとする)の最大流速の
差に比例するものであり、零からΔfsまでヘルム
ホルツ共鳴の周波数fnで周期的に変化するように
なつている。 従つて、超音波受信器9bの出力信号はいわゆ
るドツプラー効果による周波数の差として取出さ
れ、上記信号処理回路で信号処理され最終的に上
記表示器などに上記被測定成分濃度が示されるよ
うになる。尚、上記ドツプラー周波数Δfsは上記
ヘルムホルツ共鳴器8の固有振動数fnと等しく0
〜Δfsの間で周期的に変化するため、Δfsの最大
値が検出されて上記信号処理回路で信号処理され
るようになつている。 以上詳しく説明したような本発明の実施例によ
れば、ヘルムホルツ共鳴器8にとり込まれた赤外
線のエネルギーが蓄積された状態で超音波信号に
よつて測定されるような構成であるため、前記従
来例に比して測定ガス等を透過して入射する赤外
線のエネルギーを高感度に検出することができる
という利点がある。また、前記従来例のコンデン
サマイクロフオン等の場合に比し、可動部が少な
く故障しにくいという利点もある。尚、上記実施
例においてはヘルムホルツ共鳴器8内にとり込ま
れた赤外線のエネルギーを超音波信号で測定する
場合について詳述したが、本発明はこれに限定さ
れるものではなく例えば該エネルギーをレーザ光
で測定するようにしてもよく、又単にマイクロフ
オンにより共鳴音の音圧を測定するようにしても
よい。
[Formula] Incidentally, V = 2 [cm 3 ], l = 2 [cm], S = 0.2
[cm 2 ], C=340x10 2 [cm/s], and find the above natural frequency fn from the above formula (1), fn=
1.21x10 3 [c/s] = 1.21 [kHz]. Therefore,
When energy is poured into the above system at this 1.21kHz,
The above system absorbs that energy and begins to oscillate. Furthermore, when the above system enters an oscillation state, the vibration amplitude of the gas in the system increases, but due to attenuation due to the viscosity of the gas, it gradually shifts to a steady state. When a certain force is applied to the gas in 1 and 2 by infrared energy etc. supplied from the outside, the speed A of the gas flow caused by thermal expansion of the gas and that force are the trigger. The ratio A/ to the maximum value B of the vibration speed when the gas in the containers 1 and 2 vibrates
B) is given as shown in equation (2) below. However, Vmax: Maximum value of the speed at which the gas vibrates Vs : Flow velocity of the gas caused by expansion of the gas when constant energy is supplied U: Frequency ratio (i.e., the ratio between 2πf and the resonance frequency ωn) ratio
2πf/ωn) ζ: Damping ratio (0 < ζ < 1, which indicates the ratio of damping in damped vibration. In other words, it can also be said to be a coefficient that indicates the likelihood of vibration between full vibration and non-vibration) Further, FIG. 2 is an explanatory view of an example of use of the embodiment of the present invention, and in the figure, reference numeral 3 denotes a measurement cell into which a measurement gas is introduced from an inlet 3a, flows inside, and is sent out from an outlet 3b; 5 is a reference cell filled with a reference gas; 5a and 5b are light sources such as infrared lamps; 6 is a sector in which the light beams emitted from the light sources 5a and 5b are intermittent light; A rotating motor 8 is a Helmholtz resonator whose interior is filled with a predetermined gas (for example, the same gas as the measurement component gas) and two Helmholtz resonators shown in FIG. 1 are connected; 9a is a Helmholtz resonator 8;
An ultrasonic oscillator 9b, which is fixed to a predetermined part on one side of the resonator 8 and emits an ultrasonic signal, is fixed to a predetermined part on the other side of the resonator 8 (a position opposite to the position where the ultrasonic transmitter 9a is fixed). This is an ultrasonic receiver that receives the ultrasonic signal. Also, a Helmholtz resonator 8, an ultrasonic transmitter 9a, and an ultrasonic receiver 9
b constitutes the infrared detector of the embodiment of the present invention, and the output of the ultrasonic receiver 9b is signal-processed by a predetermined signal processing circuit (not shown) to determine the concentration of the component to be measured in the measurement gas. The concentration is then displayed on a display (not shown). The Helmholtz resonator 8 is a combination of two Helmholtz resonators shown in FIG. 1, and the above equations (1) and (2) hold true as in the case of FIG. Furthermore, FIG. 3 shows the above sector 6.
10 is a plan configuration diagram of parts constituting the
10a 1 to 10a o are plural parts having a predetermined width and having one side fixed to the central part 10 while maintaining a distance equal to the width. It is a single feather. Also,
The sector 6 is constructed by combining two parts shown in FIG. 3, one of which is fixed and does not move.
0 is fixed and can be rotated. By the way, the number of the blades 10a 1 to 10a o is 200.
When the motor 7 rotates at 360 rpm, the light beams emitted from the light sources 5a and 5b are interrupted at 1.2 kHz. This corresponds to chopping several hundred times faster than sectors used in conventional infrared gas analyzers. Furthermore, by making the frequency of the intermittent light and the resonant frequency ωn of the Helmholtz resonator 8 approximately equal, 2πf≒ωn, that is, u≒1
is established, and μv≒1/2. Therefore, the smaller ζ is, the larger μv becomes, and a larger velocity amplitude of the gas can be obtained.Hereinafter, the operation of the embodiment of the present invention having the above configuration will be explained in detail using FIG. 2. In FIG. 2, a measurement gas containing a component to be measured is introduced into the measurement cell 3 from an inlet 3a as shown by an arrow and is sent out from an outlet 3b, while a predetermined reference gas is contained in a reference cell 4. Filled. Further, the ultrasonic signal emitted from the ultrasonic oscillator 9a propagates through the gas within the Helmholtz resonator 8, reaches the ultrasonic receiver 9b, and is received. Furthermore,
The measurement light and the reference light emitted from the light sources 5a and 5b and made into intermittent light by the sector 6 pass through the measurement gas in the measurement cell 3 and the reference gas in the reference cell 4, respectively, and enter the Helmholtz resonator 8. reach.
Therefore, when the measurement gas in which no component to be measured is present is flowing (hereinafter referred to as the "reference state"), the measurement light and the reference light absorb energy by the measurement gas and the reference gas, respectively. However, when the measurement gas in which the component to be measured is present in the measurement gas is flowing (hereinafter referred to as the "measurement state"), only the measurement light reaches the measurement gas. The Helmholtz resonator 8 is attenuated due to energy absorption by
reach within. Therefore, the Helmholtz resonator 8
(2) above for the reference state and measurement state.
The V s value in Eq. changes. In order to detect such changes, in the case of a condenser microphone, which is a conventional infrared detector, a rotating chopper is used to extract a signal every cycle of chopping. On the other hand, in the case of the embodiment of the present invention, the resonance state is achieved even if the changing value is small. Therefore, energy is taken in and the value of the velocity multiplier μv increases, and ultimately the velocity amplitude of the gas within the Helmholtz resonator 8 changes greatly. Therefore, when an ultrasonic signal with a frequency fs is emitted from the ultrasonic transmitter 9a, the ultrasonic signal is received by the ultrasonic receiver 9b with a "beat" frequency Δfs due to the Doppler effect. Here, the "beat" frequency Δfs due to the Doppler effect refers to the positive and negative directions of the gas (in the axial direction connecting the ultrasonic transmitter 9a and the ultrasonic receiver 9b in Fig. 2, one direction is the positive direction). and the opposite direction is called the negative direction), and changes periodically from zero to Δfs at the Helmholtz resonance frequency fn. Therefore, the output signal of the ultrasonic receiver 9b is extracted as a frequency difference due to the so-called Doppler effect, is processed by the signal processing circuit, and finally the concentration of the component to be measured is displayed on the display or the like. . Note that the Doppler frequency Δfs is equal to the natural frequency fn of the Helmholtz resonator 8, which is 0.
Since the maximum value of Δfs changes periodically between Δfs and Δfs, the maximum value of Δfs is detected and processed by the signal processing circuit. According to the embodiment of the present invention as described in detail above, the infrared energy taken into the Helmholtz resonator 8 is stored and measured by the ultrasonic signal. Compared to the example, this method has an advantage in that the energy of infrared rays passing through the measurement gas and the like can be detected with high sensitivity. Further, compared to the conventional condenser microphone, etc., there is an advantage that there are fewer moving parts and less chance of failure. In the above embodiment, the case where the infrared energy taken into the Helmholtz resonator 8 is measured using an ultrasonic signal has been described in detail, but the present invention is not limited to this, and for example, the energy can be measured using a laser beam. Alternatively, the sound pressure of the resonance sound may be simply measured using a microphone.

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

第1図はヘルムホルツ共鳴器の原理説明図、第
2図は本発明実施例の使用例説明図、第3図はセ
クタの構成部品の平面構成図である。 1,2……容器、3……測定セル、3a,3b
……導出入口、4……基準セル、5a,5b……
光源、6……セクタ、7……モータ、8……ヘル
ムホルツ共鳴器、9a,9b……超音波発受信
器、10……中央部、10a1〜10ao……羽根。
FIG. 1 is an explanatory diagram of the principle of a Helmholtz resonator, FIG. 2 is an explanatory diagram of an example of use of an embodiment of the present invention, and FIG. 3 is a plan configuration diagram of the constituent parts of a sector. 1, 2... Container, 3... Measurement cell, 3a, 3b
...Derivation/exit entrance, 4...Reference cell, 5a, 5b...
Light source, 6... Sector, 7... Motor, 8... Helmholtz resonator, 9a, 9b... Ultrasonic transmitter/receiver, 10... Central part, 10a 1 to 10a o ... Vane.

Claims (1)

【特許請求の範囲】 1 光源から発せられた赤外光を短冊状の羽根が
複数個設けられたセクタを用いて高速チヨツピン
グすることにより、基準ガスが封入された基準セ
ルと被測定ガスが供給される測定セルに交互かつ
高速に赤外線を照射し、該測定セルで吸収された
赤外線を検出して前記被測定ガス中の測定成分ガ
ス濃度を分析する非分散型赤外線ガス分析計の検
出器として用いられ入射する赤外線のエネルギー
を検出する赤外線検出器において、前記基準セル
を透過した赤外線が入射する第1容器部分、前記
測定セルを透過した赤外線が入射する第2容器部
分、及びこれら2つの容器部分を連通させる連通
部分からなり測定成分ガスを含む所定の気体が充
填されてなるヘルムホルツ共鳴器と、前記第1及
び第2の容器部分の壁面であつて前記連通部分を
挾んで対向する位置にそれぞれ固着された測定信
号発信器及び測定信号受信器とを具備し、前記ヘ
ルムホルツ共鳴器内へ入射される前記赤外線エネ
ルギーの変化を該ヘルムホルツ共鳴器内の気体膨
脹による振動エネルギーに変換してヘルムホルツ
共鳴を起させると共に、前記ヘルムホルツ共鳴器
内の前記気体の速度振幅を前記測定信号発信器か
ら発せられる測定信号のドツプラー効果による周
波数の差として検出し前記測定信号受信器から出
力することを特徴とする赤外線検出器。 2 前記測定信号発信器、測定信号受信器、及び
測定信号が、それぞれ超音波発信器、超音波受信
器、及び超音波信号でなる特許請求範囲第1項記
載の赤外線検出器。 3 前記測定信号発信器、測定信号受信器、及び
測定信号が、それぞれレーザ発信器、レーザ受信
器、及びレーザ光信号でなる特許請求範囲第1項
記載の赤外線検出器。
[Claims] 1. A reference cell filled with a reference gas and a gas to be measured are supplied by high-speed chopping of infrared light emitted from a light source using a sector provided with a plurality of strip-shaped blades. As a detector for a non-dispersive infrared gas analyzer that irradiates infrared rays alternately and at high speed onto a measuring cell, detects the infrared rays absorbed by the measuring cell, and analyzes the concentration of the gas component to be measured in the gas to be measured. In an infrared detector used to detect the energy of incident infrared rays, a first container part into which the infrared rays that have passed through the reference cell enters, a second container part into which the infrared rays which have passed through the measurement cell enter, and these two containers. A Helmholtz resonator comprising a communication part that communicates the parts and filled with a predetermined gas containing the measurement component gas, and a Helmholtz resonator located on the wall surfaces of the first and second container parts at positions facing each other with the communication part in between. A measuring signal transmitter and a measuring signal receiver are respectively fixed, and the change in the infrared energy incident into the Helmholtz resonator is converted into vibration energy due to gas expansion in the Helmholtz resonator to generate Helmholtz resonance. and detecting the velocity amplitude of the gas in the Helmholtz resonator as a frequency difference due to the Doppler effect of the measurement signal emitted from the measurement signal transmitter, and outputting it from the measurement signal receiver. Infrared detector. 2. The infrared detector according to claim 1, wherein the measurement signal transmitter, measurement signal receiver, and measurement signal are respectively an ultrasonic transmitter, an ultrasonic receiver, and an ultrasonic signal. 3. The infrared detector according to claim 1, wherein the measurement signal transmitter, measurement signal receiver, and measurement signal are respectively a laser transmitter, a laser receiver, and a laser light signal.
JP16522782A 1982-09-22 1982-09-22 infrared detector Granted JPS5954950A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16522782A JPS5954950A (en) 1982-09-22 1982-09-22 infrared detector

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16522782A JPS5954950A (en) 1982-09-22 1982-09-22 infrared detector

Publications (2)

Publication Number Publication Date
JPS5954950A JPS5954950A (en) 1984-03-29
JPH0134336B2 true JPH0134336B2 (en) 1989-07-19

Family

ID=15808268

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16522782A Granted JPS5954950A (en) 1982-09-22 1982-09-22 infrared detector

Country Status (1)

Country Link
JP (1) JPS5954950A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12411116B2 (en) 2022-02-02 2025-09-09 Asahi Kasei Microdevices Corporation Apparatus with gas detection function

Also Published As

Publication number Publication date
JPS5954950A (en) 1984-03-29

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