JPH0484739A - Refractive-index measuring apparatus - Google Patents

Refractive-index measuring apparatus

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Publication number
JPH0484739A
JPH0484739A JP20058090A JP20058090A JPH0484739A JP H0484739 A JPH0484739 A JP H0484739A JP 20058090 A JP20058090 A JP 20058090A JP 20058090 A JP20058090 A JP 20058090A JP H0484739 A JPH0484739 A JP H0484739A
Authority
JP
Japan
Prior art keywords
refractive index
light
light source
reflected
interferometer
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
JP20058090A
Other languages
Japanese (ja)
Inventor
Katsuya Ikezawa
克哉 池澤
Katsumi Isozaki
克巳 磯崎
Shinji Komiya
伸二 小宮
Hideo Hirukawa
英男 蛭川
Bunkan Kin
文煥 金
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
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 Yokogawa Electric Corp filed Critical Yokogawa Electric Corp
Priority to JP20058090A priority Critical patent/JPH0484739A/en
Publication of JPH0484739A publication Critical patent/JPH0484739A/en
Pending legal-status Critical Current

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Abstract

PURPOSE:To provide an apparatus for obtaining refractive index readily and highly accurately by using a variable frequency light source, and measuring a vacuum part and an atmospheric part at the same time. CONSTITUTION:The output light from a variable frequency light source 1 is split into two light beams through a beam splitter 2. One light beam is transmitted through the splitter 2, cast into an interferometer 41 and split into two light beams. The light beams are reflected from reflecting surfaces 51a and 51b of an atmospheric part 51 in a reference space part 5, respectively, returned into the interferometer 41 and cast into detector 61. The other light beam is reflected from the beam splitter 2 and a mirror 3, cast into an interferometer 41 and split into two light beams. The light beams are reflected from reflecting surfaces 52a and 52b of a vacuum part 52 in the reference space part 5, respectively, returned into the interferometer 42 and cast into a detector 62. The outputs of the interference signals obtained from the interferometers 41 and 42 are measured in the detectors 61 and 62. The phases are measured with phase measuring devices 71 and 72. The absolute value of the refractive index is obtained in an operator 8 based on the change in phase. Thus, the highly accurate apparatus can be readily obtained.

Description

【発明の詳細な説明】 〈産業上の利用分野〉 本発明は、干渉を利用した屈折率を測定する装置に関し
、特に光源に周波数可変光源を用いた屈折率測定装置に
関する。
DETAILED DESCRIPTION OF THE INVENTION <Industrial Application Field> The present invention relates to an apparatus for measuring a refractive index using interference, and particularly to a refractive index measuring apparatus using a variable frequency light source as a light source.

〈従来の技術〉 このような光源に周波数可変光源を用いた屈折率測定装
置の先行技術として、本願出願人による特願平0f−1
28135号r屈折率測定装置」がある0本発明は、こ
の既出願のr屈折率測定装置」を改善したものであるが
、以下、本発明を説明する前に、この既出願について、
第3図を用いて概略説明する。
<Prior art> As a prior art of a refractive index measuring device using a variable frequency light source as a light source, Japanese Patent Application No. 0f-1 filed by the applicant of the present application
No. 28135 "Refractive Index Measuring Apparatus" The present invention is an improvement of the "Refractive Index Measuring Apparatus" of this previously filed application.Below, before explaining the present invention, regarding this previously filed application,
An outline will be explained using FIG.

第3図において、11は周波数の異なる複数のコヒーレ
ントな光を選択的に発生する周波数可変光源であり、例
えば一定周波数の光源11aと周波数を任意の量だけシ
フトさせる周波数シフタ11bにより構成され、任意の
周波数の光を順次発生するものである0周波数可変光源
11の出力は干渉計12で2つに分岐される。これら2
つの光は基準間隔部13に入射され、基準間隔部13の
反射面13a、13bでそれぞれ反射され、再び干渉計
12に戻り、合波されて検出器14に入射される。この
検出器14の出力が演算器15に入力される。演算器1
5では周波数可変光源11の周波数を変化させた時の検
出器14で検出される干渉次数変化より、屈折率の絶対
値を求めることができる。
In FIG. 3, reference numeral 11 denotes a variable frequency light source that selectively generates a plurality of coherent lights with different frequencies, and is composed of, for example, a light source 11a with a constant frequency and a frequency shifter 11b that shifts the frequency by an arbitrary amount. The output of the 0-frequency variable light source 11, which sequentially generates light having frequencies of , is branched into two by an interferometer 12. These 2
The two lights are incident on the reference spacing section 13, are reflected by the reflecting surfaces 13a and 13b of the reference spacing section 13, return to the interferometer 12 again, are combined, and enter the detector 14. The output of this detector 14 is input to a calculator 15. Arithmetic unit 1
5, the absolute value of the refractive index can be determined from the change in interference order detected by the detector 14 when the frequency of the variable frequency light source 11 is changed.

ここで、周波数可変光源11の光周波数を変化させた時
に検出器14で測定される干渉次数変化mは、 m=2nL (1/λIv−1/λ2v)となり、この
式より n=m/2L ・ (1/ (1/λ1v−1/λ2v
))==AV−m/2L −(m/2L)(Cv /△f )      −・・
■ただし、 n:屈折率 λ1■、λ2v:真空中の変化前後の波長A■:λ1v
とλ2vの合成波長 Cv 二真空中の光速 △f:周波数可変幅 である。
Here, the interference order change m measured by the detector 14 when changing the optical frequency of the variable frequency light source 11 is m=2nL (1/λIv-1/λ2v), and from this formula, n=m/2L・ (1/ (1/λ1v-1/λ2v
))==AV-m/2L-(m/2L)(Cv/△f)-・・
■However, n: refractive index λ1■, λ2v: wavelength A before and after change in vacuum■: λ1v
and λ2v combined wavelength Cv.2 Speed of light in vacuum △f: Frequency variable width.

従って、基準間隔部13の反射面13a、]3bの間隔
りと周波数可変幅Δfを予め設定しておき、干渉次数変
化mを測定することにより、上記0式より屈折率の絶対
値を求めることができる。
Therefore, by setting the spacing between the reflective surfaces 13a, ]3b of the reference spacing section 13 and the frequency variable width Δf in advance, and measuring the interference order change m, the absolute value of the refractive index can be determined from the above formula 0. I can do it.

〈発明が解決しようとする課題〉 しかしながら上記従来捜術に示す屈折率測定装置におい
て、屈折率の絶対値をより高精度に求めるためには、基
準間隔部の反射面の間隔りや周波数可変幅△fや干渉次
数変化の測定fMm全てに高い精度が要求され、屈折率
の絶対値の高精度化を妨げていた。
<Problems to be Solved by the Invention> However, in the refractive index measuring device shown in the conventional search technique described above, in order to obtain the absolute value of the refractive index with higher accuracy, it is necessary to adjust the interval between the reflective surfaces of the reference interval part and the frequency variable width △. High precision is required for all measurements of f and interference order change fMm, which has hindered high precision of the absolute value of the refractive index.

本発明は、この点に着目し、容易に屈折率の絶対値をよ
り高精度に求めることができる周波数可変光源を用いた
屈折率測定装置を提供することを目的としたものである
The present invention has focused on this point and aims to provide a refractive index measuring device using a variable frequency light source that can easily determine the absolute value of the refractive index with higher precision.

く課題を解決するための手段〉 上記課題を解決するための本発明の構成は、周波数可変
光源と、この光源の出力光を2つに分岐する光学部品と
、この光学部品により分岐された2つの光がそれぞれ入
射される2つの干渉計と、反射面が所定の等しい長さ基
準で平行配置されると共に真空状態に密閉された真空部
と大気に解放された大気部で構成され、前記2つの干渉
計からの入射光が前記真空部及び大気部の反射面でそれ
ぞれ反射した後出射するように形成された基準間隔部と
、この基準間隔部から反射された光の光路長差に伴って
前記干渉計により得られる干渉信号の出力を測定する複
数の検出器と、この出力された干渉信号の位相を測定す
る複数の位相測定器と、前記周波数可変光源の周波数を
連続的に掃引した時の干渉信号の位相の変化から屈折率
の絶対値を演算する演算器とを設けた構成としたことを
特徴とするものである。
Means for Solving the Problems> The configuration of the present invention for solving the above problems includes a variable frequency light source, an optical component that splits the output light of the light source into two, and a light beam split into two by the optical component. It is composed of two interferometers into which two beams of light are respectively incident, a vacuum part whose reflecting surfaces are arranged parallel to each other with predetermined equal length standards, and a vacuum part sealed in a vacuum state and an atmospheric part which is opened to the atmosphere. Due to the optical path length difference between the reference interval part formed so that the incident light from the two interferometers is emitted after being reflected on the reflective surfaces of the vacuum part and the atmospheric part, and the light reflected from this reference interval part, a plurality of detectors that measure the output of the interference signal obtained by the interferometer; a plurality of phase measuring devices that measure the phase of the output interference signal; and when the frequency of the frequency variable light source is continuously swept. The present invention is characterized in that it is provided with a computing unit that computes the absolute value of the refractive index from a change in the phase of the interference signal.

〈作用〉 本発明によれば、真空部と大気部とを同時に測定し、又
、屈折率(n−1)を測定するため、基準間隔部の反射
面の間隔や周波数可変幅等に高い精度を必要としなくて
も、屈折率の絶対値をより高精度に求めることができる
<Function> According to the present invention, since the vacuum area and the atmospheric area are measured simultaneously, and the refractive index (n-1) is measured, high accuracy is achieved in the interval between the reflective surfaces of the reference interval part, the frequency variable width, etc. The absolute value of the refractive index can be determined with higher precision even if the refractive index is not required.

〈実施例〉 以下、本発明を図面に基づいて説明する。<Example> Hereinafter, the present invention will be explained based on the drawings.

第1図は本発明の屈折率測定装置の一実施例を示す構成
図である。第1図りこおいて、1は周波数可変光源、2
は周波数可変光源1の出力光を2つに分岐するビームス
プリッタ、3はミラー、41゜42は干渉計、5は同一
のスペーサから形成された基準間隔部であり、反射面5
1aと51b、52aと52bとが等しい長さ基準して
平行配置され、一方は大気に解放された大気部51、他
方は真空状態に密閉された真空部52を形成している。
FIG. 1 is a block diagram showing an embodiment of the refractive index measuring device of the present invention. In the first diagram, 1 is a frequency variable light source, 2
is a beam splitter that splits the output light of the frequency variable light source 1 into two; 3 is a mirror; 41° and 42 are interferometers; 5 is a reference interval formed from the same spacer;
1a and 51b, and 52a and 52b are arranged in parallel on the basis of equal length, and one forms an atmospheric part 51 that is open to the atmosphere, and the other forms a vacuum part 52 that is sealed in a vacuum state.

61.62は基準間隔部5から反射された光の光路長変
化に伴なって、干渉計41.42から得られる干渉信号
の出力を測定する検出器、71.72は検出器61.6
2から出力された干渉信号の位相を測定する位相測定器
、8は位相測定器71゜72から出力された干渉信号の
位相の変化から屈折率の絶対値を演算する演算器である
61.62 is a detector that measures the output of the interference signal obtained from the interferometer 41.42 as the optical path length of the light reflected from the reference interval part 5 changes, and 71.72 is the detector 61.6.
2 is a phase measuring device that measures the phase of the interference signal outputted, and 8 is a computing unit that calculates the absolute value of the refractive index from the change in the phase of the interference signal outputted from the phase measuring devices 71 and 72.

このような構成において、周波数可変光源1の出力光は
ビームスプリッタ2で2つに分岐される。
In such a configuration, the output light of the frequency variable light source 1 is split into two by the beam splitter 2.

一方の光は、ビームスプリッタ2を透過し、干渉計41
に入射される。入射された光は干渉計41にて更に2つ
に分岐され、基準間隔部5の大気部51の反射面51a
、51bでそれぞれ反射され、再び干渉計41に戻り、
検出器61に入射される。
One of the lights passes through the beam splitter 2 and passes through the interferometer 41.
is incident on the The incident light is further split into two by the interferometer 41, and reflected by the reflective surface 51a of the atmospheric part 51 of the reference interval part 5.
, 51b and return to the interferometer 41 again,
The light is incident on the detector 61.

他方の光はビームスプリッタ2、ミラー3で反射され、
干渉計42に入射される。入射された光は、干渉計42
にて更に2つに分岐され、基準間隔部5の真空部52の
反射面52 a、52 bでそれぞれ反射され、再び干
渉計42に戻り、検出器62に入射される。検出器61
.62では、干渉計41.42から得られる干渉信号の
出力が測定され、位相測定器71.72にて、干渉信号
の位相を測定後、演算器8にて干渉信号の位相変化から
屈折率の絶対値が求められる。
The other light is reflected by beam splitter 2 and mirror 3,
The light is incident on the interferometer 42. The incident light passes through an interferometer 42
The light is further branched into two parts, reflected by the reflecting surfaces 52 a and 52 b of the vacuum part 52 of the reference interval part 5 , returns to the interferometer 42 again, and enters the detector 62 . Detector 61
.. At 62, the output of the interference signal obtained from the interferometers 41 and 42 is measured, and after the phase of the interference signal is measured at the phase measuring device 71 and 72, the refractive index is calculated from the phase change of the interference signal at the arithmetic unit 8. Absolute value is required.

ここで、第2図(イ)に示すように、周波数可変光源1
の周波数を連続的に変化(図中、ν。→ν1)させた時
の検出器61と62から得られる干渉信号の出力は、そ
れぞれ第2図(ロ)、(ハ)に示すようになる。この干
渉信号の出力は、θvl= < 2 v o / c 
) L    ・=(1)θv2= (2v + / 
c ) L    ・・・(2)θa1= (2vo 
/ c ) n L   ・・・(3)θa2=(2ν
+/c)nL   −C4)ただし、Cは真空中での光
速である。
Here, as shown in FIG. 2(a), the frequency variable light source 1
The outputs of the interference signals obtained from the detectors 61 and 62 when the frequency of is continuously changed (in the figure, ν → ν1) are shown in Figure 2 (B) and (C), respectively. . The output of this interference signal is θvl=<2 v o / c
) L ・=(1)θv2= (2v + /
c) L...(2) θa1= (2vo
/ c ) n L ... (3) θa2=(2ν
+/c) nL -C4) where C is the speed of light in vacuum.

ここで、シ1−シ0=Δνとすると、上記(1)〜(4
)式は、 (2/c)  ΔJ/L−θv2−θvt    =(
5)(2/c)  ΔvnL=θa2−θa 1   
−(6)となる、この(5) 、 (6)式より、n=
(θa2−θal)/(θv2−θv1)・・・(7)
と表される。この(7)式から求められる屈折率(n)
の精度は、干渉信号の出力θの精度により決定されるも
のであり、一般的には高精度にはならない。
Here, if S1-S0=Δν, the above (1) to (4
) formula is (2/c) ΔJ/L−θv2−θvt =(
5) (2/c) ΔvnL=θa2-θa 1
-(6) From these equations (5) and (6), n=
(θa2-θal)/(θv2-θv1)...(7)
It is expressed as Refractive index (n) obtained from this equation (7)
The accuracy of is determined by the accuracy of the output θ of the interference signal, and is generally not highly accurate.

次に、上記(2)−、(4)式より 2v1 /c  ・ (n   1 )L=θa2−θ
v2=M+α  ・・・(8) ただし、M:は正の整数 α;小数 とする、この(8)式の内、小数αは検出器61,62
の出力θa2.θv2より求められるが、Mは求められ
ない、しかし、前記(7)式より、屈折率nの概算値を
求め・ることができ、又S前記(8)式よりMは正の整
数であるため、Mを誤差なく求めることができる。
Next, from the above equations (2)- and (4), 2v1 /c ・ (n 1 )L=θa2-θ
v2=M+α...(8) However, M: is a positive integer α; it is a decimal number. In this equation (8), the decimal number α is the detector 61, 62
The output θa2. It can be found from θv2, but M cannot be found.However, from the above equation (7), an approximate value of the refractive index n can be found, and from the above equation (8), M is a positive integer. Therefore, M can be determined without error.

したがって、前記(8)式を変形した n−1= (c/2ν+ L)(M+cz)−(9)か
ら、屈折率nを高精度に求めることができる。
Therefore, the refractive index n can be determined with high precision from n-1=(c/2ν+L)(M+cz)-(9), which is a modification of the equation (8).

−檀1四22と1− 以下、具体例を上げて詳細に説明する。-Dan 1422 and 1- Hereinafter, a detailed explanation will be given using a specific example.

周波数可変幅Δν=3TH2、長さ基準L=100am
、位相内挿精度を11500とすると、前記(5)、(
6)式より、(θv2−θv1)、(θa2−θa1)
の概算値は、2X10”程度となる。又、前記(7)式
は、 ldn/nl ;1 d (θa2−θa1)/(θa2−θa1)十
1d(θv2−θv1)/(θv2−θvl) 1−0
0となり、整数部には誤差を生じないため、d(θa2
−θal)l=ld(θv2−θvl)= 11500 、’、 l dn/n l =2x l O’したがっ
て、前記(7)式より求まる屈折率nの精度は、2X1
0’程度である。
Frequency variable width Δν = 3TH2, length reference L = 100am
, when the phase interpolation accuracy is 11500, the above (5), (
From formula 6), (θv2-θv1), (θa2-θa1)
The approximate value of is approximately 2X10''. Also, the above equation (7) is: ldn/nl; 1-0
0, and there is no error in the integer part, so d(θa2
-θal)l=ld(θv2-θvl)=11500,', ldn/nl=2xlO'Therefore, the accuracy of the refractive index n found from the above equation (7) is 2X1
It is about 0'.

次に、I/l =3.8x 10”H2(A+ =78
0nll)n−1+2.7X10−とすると、前記(8
)式より、    M+α″、68 又、〔8)式は、 d(M十α)/(M+α) =ldシ1/シ1 十l d (n−1)/ (n−1) +ldL/Ll      ・・・ODとなる。この0
0式で、 (dシ1/シ1)く104 は容易に得られる。ス、 l  dn/n 1=2x1.o’ を用いて、 d (n−1)/ (n−1) =2xlO’/2.7xlO’=7.4xlO°2とな
る。更に、Lの測定精度を10μmとすると、dL/L
=10’ 、°、ld(M+α)l=0.51<1したがって、整
数部Mを誤差なく求めることができる。
Next, I/l = 3.8x 10”H2 (A+ = 78
0nll)n-1+2.7X10-, the above (8
) From the formula, M + α'', 68 Also, the formula [8] is: d (M + α) / (M + α) = ld shi 1 / shi 1 d (n-1) / (n-1) + ldL / Ll ...It becomes OD.This 0
In the equation 0, (dsi1/shi1)ku104 can be easily obtained. l dn/n 1=2x1. o', d (n-1)/(n-1) = 2xlO'/2.7xlO' = 7.4xlO°2. Furthermore, if the measurement accuracy of L is 10 μm, dL/L
=10',°, ld(M+α)l=0.51<1 Therefore, the integer part M can be determined without error.

前記■)式より、 I d (n−1)/ (n−1> =ldシ1/シ、l+ldL/L 十ld(M+α)/JM十α) =10’+10’十(11500)/68=1.4X1
0’ n−1=2.7X104であるので、 dn/n l =3.8X10’ となり、前記(7)式から求めた屈折率の絶対値より高
精度で求めることができる。
From the above formula (■), I d (n-1)/ (n-1> = ldshi1/shi, l+ldL/L 10'ld(M+α)/JM10') = 10'+10'10(11500)/68 =1.4X1
Since 0' n-1 = 2.7X104, dn/n l =3.8X10', which can be determined with higher precision than the absolute value of the refractive index determined from equation (7) above.

なお、上記実施例において、干渉計として、ダブルパス
干渉計を用いることにより、基準間隔部の大気部と真空
部の長さ基準の一致精度を高めることができるため、よ
り高精度に屈折率の絶対値を求めることができる。
In the above embodiment, by using a double-pass interferometer as the interferometer, it is possible to improve the accuracy of matching the length standards of the atmospheric part and the vacuum part of the reference interval part, so that the absolute refractive index can be determined with higher precision. You can find the value.

又、基準間隔部の大気部を一度真空状態として、2つの
基準間隔の比を校正することにより、基準間隔部の大気
部と真空部の長さ基準の不一致を補償することができる
ため、より高精度に屈折率の絶対値を求めることができ
る。
In addition, by once setting the atmospheric part of the standard interval part in a vacuum state and calibrating the ratio of the two standard intervals, it is possible to compensate for the discrepancy between the length standards of the atmospheric part and the vacuum part of the standard interval part. The absolute value of the refractive index can be determined with high precision.

更に、位相の検出方法としては、ヘテロダイン方式や偏
光干渉方式等を用いても良い。
Further, as a phase detection method, a heterodyne method, a polarization interference method, or the like may be used.

〈発明の効果〉 以上、実施例と共に具体的に説明したように、本発明に
よれば、周波数可変光源を用いて真空部と大気部とを同
時に測定しており、又、屈折率(n−1)を測定するた
め、基準間隔部の反射面の間隔(長さ基準)や周波数可
変幅等に高い精度を要求しなくても、容易に屈折率の絶
対値をより高精度に求めることができる周波数可変光源
を用いた屈折率測定装置を実現することができる。
<Effects of the Invention> As described above in detail with the embodiments, according to the present invention, the vacuum region and the atmospheric region are simultaneously measured using a variable frequency light source, and the refractive index (n- 1), it is possible to easily obtain the absolute value of the refractive index with higher precision without requiring high accuracy in the interval (length standard) of the reflective surfaces in the reference interval section or the frequency variable width. It is possible to realize a refractive index measuring device using a variable frequency light source.

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

第1図は本発明の屈折率測定装置の一実施例を示す構成
図、第2図は第1図装置の周波数可変光源を変化させた
時の検出器出力を示す図、第3図は本発明の屈折率測定
装置の先行例を示す構成図である。 1・・・周波数可変光源、2・・・ビームスプリッタ、
3・・・ミラー 5・・・基準間隔部、8・・・演算器
、41゜42・・・干渉計、51・・・大気部、52・
・・真空部、51a、51b、52a、52b−基準間
隔部の反射面、61.62・・・検出器、71.72・
・・位相測定器。 第1図 第2図 (−gnご
Fig. 1 is a configuration diagram showing an embodiment of the refractive index measuring device of the present invention, Fig. 2 is a diagram showing the detector output when the variable frequency light source of the device shown in Fig. 1 is changed, and Fig. 3 is a diagram showing the main unit. FIG. 1 is a configuration diagram showing a prior example of a refractive index measuring device of the invention. 1... Frequency variable light source, 2... Beam splitter,
3...Mirror 5...Reference interval part, 8...Calculator, 41°42...Interferometer, 51...Atmospheric part, 52...
...Vacuum section, 51a, 51b, 52a, 52b-Reflection surface of reference interval section, 61.62...Detector, 71.72.
...Phase measuring device. Figure 1 Figure 2 (-gn

Claims (1)

【特許請求の範囲】 周波数可変光源と、 この光源の出力光を2つに分岐する光学部品と、この光
学部品により分岐された2つの光がそれぞれ入射される
2つの干渉計と、 反射面が所定の等しい長さ基準で平行配置されると共に
真空状態に密閉された真空部と大気に解放された大気部
で構成され、前記2つの干渉計からの入射光が前記真空
部及び大気部の反射面でそれぞれ反射した後出射するよ
うに形成された基準間隔部と、 この基準間隔部から反射された光の光路長差に伴って前
記干渉計により得られる干渉信号の出力を測定する複数
の検出器と、 この出力された干渉信号の位相を測定する複数の位相測
定器と、 前記周波数可変光源の周波数を連続的に掃引した時の干
渉信号の位相の変化から屈折率の絶対値を演算する演算
器とを設けた構成としたことを特徴とする屈折率測定装
置。
[Claims] A variable frequency light source, an optical component that splits the output light of the light source into two, two interferometers into which the two lights split by the optical component are respectively incident, and a reflecting surface. It consists of a vacuum section that is arranged in parallel with predetermined equal length standards and is sealed in a vacuum state and an atmospheric section that is open to the atmosphere, and the incident light from the two interferometers is reflected from the vacuum section and the atmospheric section. a reference interval portion formed to be emitted after being reflected by a surface; and a plurality of detection units for measuring the output of an interference signal obtained by the interferometer according to the optical path length difference of the light reflected from the reference interval portion. a plurality of phase measuring devices for measuring the phase of the output interference signal; and calculating the absolute value of the refractive index from the change in the phase of the interference signal when the frequency of the variable frequency light source is continuously swept. 1. A refractive index measuring device characterized by having a configuration including a computing unit.
JP20058090A 1990-07-27 1990-07-27 Refractive-index measuring apparatus Pending JPH0484739A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP20058090A JPH0484739A (en) 1990-07-27 1990-07-27 Refractive-index measuring apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP20058090A JPH0484739A (en) 1990-07-27 1990-07-27 Refractive-index measuring apparatus

Publications (1)

Publication Number Publication Date
JPH0484739A true JPH0484739A (en) 1992-03-18

Family

ID=16426704

Family Applications (1)

Application Number Title Priority Date Filing Date
JP20058090A Pending JPH0484739A (en) 1990-07-27 1990-07-27 Refractive-index measuring apparatus

Country Status (1)

Country Link
JP (1) JPH0484739A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012127838A (en) * 2010-12-16 2012-07-05 Canon Inc Apparatus and method for absolute position measurement
CN108318420A (en) * 2017-12-22 2018-07-24 北京航天计量测试技术研究所 A kind of light channel structure for high-precision gas refractometry

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2012127838A (en) * 2010-12-16 2012-07-05 Canon Inc Apparatus and method for absolute position measurement
CN108318420A (en) * 2017-12-22 2018-07-24 北京航天计量测试技术研究所 A kind of light channel structure for high-precision gas refractometry

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