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JPS6038646B2 - emissivity measurement method - Google Patents
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JPS6038646B2 - emissivity measurement method - Google Patents

emissivity measurement method

Info

Publication number
JPS6038646B2
JPS6038646B2 JP6949879A JP6949879A JPS6038646B2 JP S6038646 B2 JPS6038646 B2 JP S6038646B2 JP 6949879 A JP6949879 A JP 6949879A JP 6949879 A JP6949879 A JP 6949879A JP S6038646 B2 JPS6038646 B2 JP S6038646B2
Authority
JP
Japan
Prior art keywords
emissivity
measured
temperature
measurement
measurement method
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
JP6949879A
Other languages
Japanese (ja)
Other versions
JPS55162028A (en
Inventor
士郎 木村
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.)
Resonac Holdings Corp
Original Assignee
Showa Denko KK
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 Showa Denko KK filed Critical Showa Denko KK
Priority to JP6949879A priority Critical patent/JPS6038646B2/en
Publication of JPS55162028A publication Critical patent/JPS55162028A/en
Publication of JPS6038646B2 publication Critical patent/JPS6038646B2/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01JMEASUREMENT OF INTENSITY, VELOCITY, SPECTRAL CONTENT, POLARISATION, PHASE OR PULSE CHARACTERISTICS OF INFRARED, VISIBLE OR ULTRAVIOLET LIGHT; COLORIMETRY; RADIATION PYROMETRY
    • G01J5/00Radiation pyrometry, e.g. infrared or optical thermometry
    • G01J5/0003Radiation pyrometry, e.g. infrared or optical thermometry for sensing the radiant heat transfer of samples, e.g. emittance meter

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Spectroscopy & Molecular Physics (AREA)
  • Radiation Pyrometers (AREA)

Description

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

本発明は放射率測定法に関し、より詳細には例えば熱流
東を測定する熱流センサーを用いて被熱流東側定物表面
からの熱流東を測定する場合、該被測定物の放射率が未
知であれば測定誤差を生ずるのでこの被測定物の放射率
を予め知っておかねばならない。 一般的には、データブックその他の文献よりに放射率は
記載されているが、温度変化に対する放射率の研究は数
少ない。この発明は既知の放射率を有する放射率測定用
素子を用いることによって未知の放射率を決定できる放
射率測定法に関するものである。本発明で述べられる既
知の放射率を有する放射率測定用素子としては所定範囲
の放射率を有するように陽極酸化皮膜厚を調節してアル
ミニウム薄板表面に形成した素子を使用でき、この素子
の放射率は温度依存性が小さいことがわかっている。 熱流センサーとは薄膜熱抵抗体の表裏間の温度差を取り
出す検出素子と表面温度測定用検出素子を電気絶縁性薄
膜体間に組み入れた構造のものを意味する。熱流東(ぐ
:Kcal/〆・h)を放出している被測定物に対して
熱流センサ−を使用してその熱流東◇を測定するとき、
原理的には温度差測定用検出素子(差動熱電対群)によ
って熱抵抗体の表裏の温度差△T(00)を直流電圧出
力Vで測定したとき、次式○=VX^/d刀(り=V/
△TmV/℃)但し、入:熱抵抗体の熱伝導率d:熱抵
抗体の厚さ り:差動熱電対群の熱電能 によって熱流東◇を決定しているが、被測定物と熱流セ
ンサーとの放射エネルギーを考えた場合、互いの放射率
が異なると測定誤差を生ずる。 したがって、被測定物の熱流東を正しく測定するために
は、被測定物表面の放射率ごoと熱流センサーの大気側
表面の放射率ごaとにおいてごo=ごaの関係を成立さ
せることが必要である。そこで、被測定物表面の放射率
ごoをあらかじめ知っておかねばならない。その他物体
の表面温度を赤外線放射温度計にて測定する場合にも物
体表面の放射率を知る必要がある。 ところが、各種物質の放射率ごについては文献などに記
述されているが、放射率の温度変化時の値は余り記述さ
れていない。 上記放射率の測定法としては、下記のような測定法が通
常採用されている。 その測定法の原理は次式に従う。 Q=ご。 TS4但し、Q:被測定物面からの放散熱量 。 :ステフアンの定数Ts:被測定物面の温度 〔1〕 被測定物の表面温度Ts(k)を例えば篤霞型
赤外線温度計で測定し、その温度計(測定対象物に応じ
ご=0〜1.0まで補正可能)の放射率補正ッムミの値
を可変させ、温度計の指示が別に接触型の温度計で測定
した温度Tsになるようになし、その時の放射率補正ッ
マミの指示するごが被測定面の放射率ごとなる。
The present invention relates to an emissivity measurement method, and more specifically, when measuring the heat flow east from the surface of a fixed object on the east side of the heat flow using a heat flow sensor that measures the heat flow east, the present invention relates to an emissivity measurement method, and more particularly, when measuring the heat flow east from the surface of a fixed object on the east side of the heat flow, even if the emissivity of the object to be measured is unknown. Since this will cause measurement errors, the emissivity of the object to be measured must be known in advance. Generally, emissivity is described in data books and other documents, but there are only a few studies on emissivity with respect to temperature changes. The present invention relates to an emissivity measurement method in which an unknown emissivity can be determined by using an emissivity measuring element having a known emissivity. As the emissivity measuring element having a known emissivity as described in the present invention, an element formed on the surface of a thin aluminum plate by adjusting the thickness of the anodic oxide film so as to have an emissivity within a predetermined range can be used. The rate has been found to have a small temperature dependence. A heat flow sensor refers to a structure in which a detection element for detecting the temperature difference between the front and back sides of a thin film thermal resistor and a detection element for measuring the surface temperature are incorporated between an electrically insulating thin film body. When measuring the heat flow east ◇ using a heat flow sensor for a measured object that emits heat flow east (g: Kcal/〆・h),
In principle, when the temperature difference △T (00) between the front and back sides of a thermal resistor is measured with a DC voltage output V using a temperature difference measurement detection element (differential thermocouple group), the following formula ○=VX^/d (ri=V/
△TmV/℃) However, input: Thermal conductivity of the thermal resistor d: Thickness of the thermal resistor: The heat flow east ◇ is determined by the thermopower of the differential thermocouple group, but the When considering the radiated energy of the two, if their emissivities differ, measurement errors will occur. Therefore, in order to accurately measure the heat flow east of the object to be measured, it is necessary to establish the relationship between the emissivity o of the surface of the object to be measured and the emissivity a of the atmospheric side surface of the heat flow sensor. is necessary. Therefore, the emissivity o of the surface of the object to be measured must be known in advance. In addition, when measuring the surface temperature of an object using an infrared radiation thermometer, it is necessary to know the emissivity of the object's surface. However, although the emissivity of various materials is described in literature, the value of emissivity when the temperature changes is not often described. As a method for measuring the above-mentioned emissivity, the following measurement method is usually adopted. The principle of the measurement method follows the following formula. Q = Go. TS4 However, Q: Amount of heat dissipated from the surface of the measured object. : Stephan's constant Ts: Temperature of the surface of the object to be measured [1] Measure the surface temperature Ts(k) of the object to be measured with, for example, an Atsuka-type infrared thermometer, The value of the emissivity correction mm (which can be corrected up to 1.0) is varied so that the temperature indicated by the thermometer becomes the temperature Ts measured separately with a contact thermometer, and the value indicated by the emissivity correction mm is adjusted accordingly. is the emissivity of the surface to be measured.

〔0〕 被測定物表面を赤外分光分析にてふく射スペク
トルの強度分布を測定し、それより放射率ごを計算して
求める。 本発明は上記従来の測定対象物の放射率測定法とは観点
を異にした簡便で精度の高い測定法を提供することにあ
る。 以下、本発明の放射率測定法を添附の原理図を参照しな
がら説明する。 放射温度TRにおける放射率どが既知の放射率測定用素
子4個(恥.1〜4)を測定対象物表面に貼着する。 この状態を第1図に示した。図において1は放射率測定
用素子、2は測定対象物を示す。上記放射率測定用素子
1を測定対象物2表面に夫々貼着したのち、それらが定
常状態に達してから、放射温度測定要素として例えば篤
露型赤外線放射温度計によって放射率補正をしない、即
ち放射率ご=1として放射率測定用素子M.1〜4まで
の放射温度TRを測定する。 該測定対象物の表面温度Tsにおける放射率ごと放射率
測定用素子の放射温度TRとの関数関係を求めて第1図
に示すように検量線を描く。次に測定対象物の放射温度
TR。を赤外線放射温度計で測定する。この測定温度T
Roを検量線上にのせることにより、その温度に対する
放射率ごが求められる。実施例 測定対象物としてステンレス鋼(SUS)を用いこのも
のの放射率ごを測定した。 既知の放射率を有する放射率測定用素子としては硫酸ア
ルマイト法による陽極酸化皮膜をアルミニウム基板に形
成したものを用いた。 この素子をSUS板表面に5個等間隔に貼着し、SUS
板が有する温度に放射率測定用素子の温度が平衡状態に
達した後各放射率測定用素子の放射温度TRを赤外線放
射温度計で放射率補正ないこ、ご=1として測定した。
この測定温度TR(K)と放射率素子の既知の放射率ご
との関係は次表のとおりとなる。・次に放射率が未知の
SUS板の放射率を定めた時の精度を論ずるための前段
階として以下の準備をした。 上記の放射率測定対象物の接触型温度計で測定した表面
温度Tsは各素子のTRを測る都度若干変動(第2表中
のTs)したが約120午Cである。 この温度Tsは放射率ごと室温T^がわかれば次式から
も求めることができる。即ち、TS4=(TR4−T^
4)/ご+T^4次に、接触型温度計で測定したTsを
用い下記の関係式から素子および測定対象物の放射率ご
を求めて第2表に掲げた。 ご=(TR4一T^4)/(TS4−T^4)×100
(%)第2表 上表の接触型温度計で測定したTsより計算された放射
率ご(%)は第1表に示される放射率素子の既知の放射
率ご(%)と大体近似しており、既知の値に譲りのない
ことが確認された。 次に、第1表に掲げた測定結果に基づいて検量線を図表
したものを第2図に示した。 同検量線図からSUSの放射温度TRo(℃)=35.
70の放射率ごoを求めるとごo芋10.05%となり
、35.700(TR)の計算値ごo=10.13%と
良く一致した。 本発明の測定法に従えば、2枚以上の既知の放射率を有
する放射率測定用素子を用いて熱流東側定対象物等の物
体表面の放射率を簡便かつ正確に測定することができる
[0] The intensity distribution of the radiation spectrum of the surface of the object to be measured is measured by infrared spectroscopy, and the emissivity is calculated from this. An object of the present invention is to provide a simple and highly accurate measurement method that is different from the conventional emissivity measurement method for a measurement object. Hereinafter, the emissivity measurement method of the present invention will be explained with reference to the attached principle diagram. Four emissivity measuring elements (1 to 4) whose emissivity at the radiation temperature TR is known are attached to the surface of the object to be measured. This state is shown in FIG. In the figure, 1 indicates an emissivity measuring element, and 2 indicates an object to be measured. After each of the emissivity measurement elements 1 is attached to the surface of the measurement object 2, and after they reach a steady state, emissivity correction is not performed using, for example, a dew-type infrared radiation thermometer as a radiation temperature measurement element, i.e. Assuming that each emissivity is 1, the emissivity measuring element M. Measure the radiant temperature TR from 1 to 4. The functional relationship between each emissivity at the surface temperature Ts of the object to be measured and the radiation temperature TR of the emissivity measuring element is determined, and a calibration curve is drawn as shown in FIG. Next, the radiation temperature TR of the object to be measured. is measured with an infrared radiation thermometer. This measured temperature T
By placing Ro on the calibration curve, the emissivity for that temperature can be determined. EXAMPLE Stainless steel (SUS) was used as the object to be measured, and its emissivity was measured. The emissivity measurement element having a known emissivity was an aluminum substrate on which an anodic oxide film was formed using the sulfuric acid alumite method. Five of these elements were pasted at equal intervals on the surface of the SUS plate, and
After the temperature of the emissivity measuring element reached an equilibrium state with the temperature of the plate, the radiation temperature TR of each emissivity measuring element was measured using an infrared radiation thermometer with no emissivity correction.
The relationship between this measured temperature TR (K) and each known emissivity of the emissivity element is as shown in the following table.・Next, I made the following preparations as a preliminary step to discussing the accuracy of determining the emissivity of a SUS plate with unknown emissivity. The surface temperature Ts of the above emissivity measurement object measured with a contact thermometer is approximately 120 pm, although it varies slightly each time the TR of each element is measured (Ts in Table 2). This temperature Ts can also be determined from the following equation if the room temperature T^ is known for each emissivity. That is, TS4=(TR4-T^
4)/Go+T^4 Next, the emissivity of the element and the object to be measured was determined from the following relational expression using Ts measured with a contact thermometer and listed in Table 2. Go=(TR4-T^4)/(TS4-T^4)×100
(%) The emissivity (%) calculated from Ts measured with the contact thermometer shown in the upper table of Table 2 is approximately approximate to the known emissivity (%) of the emissivity element shown in Table 1. It was confirmed that there was no compromise with the known value. Next, FIG. 2 shows a diagram of a calibration curve based on the measurement results listed in Table 1. From the same calibration curve, the radiation temperature of SUS TRo (°C) = 35.
When the emissivity of 70 was calculated, it was 10.05%, which was in good agreement with the calculated value of 35.700 (TR), which was 10.13%. According to the measurement method of the present invention, it is possible to easily and accurately measure the emissivity of the surface of an object such as a target object on the east side of heat flow using two or more emissivity measurement elements having known emissivity.

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

第1図は本発明の測定法の原理を示す説明図、第2図は
SUS(ステンレス鋼)の測定に使用した検量線図であ
る。 第1図 第2図
FIG. 1 is an explanatory diagram showing the principle of the measuring method of the present invention, and FIG. 2 is a calibration curve diagram used for measuring SUS (stainless steel). Figure 1 Figure 2

Claims (1)

【特許請求の範囲】[Claims] 1 既知の放射率εを有する放射率測定用素子を少なく
とも2枚以上、放射率測定対象物の表面に貼着し定常状
態に達したのち放射率測定用素子の放射温度T_Rと前
記測定対象物の放射温度T_Sを放射温度測定要素によ
つてそれぞれ測定し、放射率測定用素子の放射温度T_
Rと放射率εとの関数関係により測定対象物の放射率ε
oを求めることを特徴とする放射率測定法。
1 At least two or more emissivity measurement elements having a known emissivity ε are attached to the surface of the emissivity measurement object, and after reaching a steady state, the radiation temperature T_R of the emissivity measurement element and the measurement object are measured. The radiation temperature T_S of the emissivity measurement element is measured by each radiation temperature measurement element, and the radiation temperature T_S of the emissivity measurement element is measured by the radiation temperature measurement element.
The emissivity ε of the object to be measured is determined by the functional relationship between R and the emissivity ε.
An emissivity measurement method characterized by determining o.
JP6949879A 1979-06-05 1979-06-05 emissivity measurement method Expired JPS6038646B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP6949879A JPS6038646B2 (en) 1979-06-05 1979-06-05 emissivity measurement method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP6949879A JPS6038646B2 (en) 1979-06-05 1979-06-05 emissivity measurement method

Publications (2)

Publication Number Publication Date
JPS55162028A JPS55162028A (en) 1980-12-17
JPS6038646B2 true JPS6038646B2 (en) 1985-09-02

Family

ID=13404435

Family Applications (1)

Application Number Title Priority Date Filing Date
JP6949879A Expired JPS6038646B2 (en) 1979-06-05 1979-06-05 emissivity measurement method

Country Status (1)

Country Link
JP (1) JPS6038646B2 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4989991A (en) * 1987-10-26 1991-02-05 Ag Processing Technologies, Inc. Emissivity calibration apparatus and method
US4881823A (en) * 1988-03-29 1989-11-21 Purdue Research Foundation Radiation thermometry
US5186541A (en) * 1991-10-21 1993-02-16 Gentri Controls, Inc. Non-contact infrared temperature sensing system

Also Published As

Publication number Publication date
JPS55162028A (en) 1980-12-17

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